# AC 36-1H: Noise Levels for U.S. Certificated and Foreign Aircraft - Type: Advisory circular (guidance, not mandatory unless a rule or AD requires it) - Status: Current - Approved: May 25, 2012 - Last reviewed: May 25, 2012 - This change: Change 1 incorporated - Family: AC 36-1 - 14 CFR parts: 36 - Pages: 364 - PDF: https://openairdocs.org/files/sha256/3e/5d/3e5d35c0b2608271673826a7cdd11ebd6de21fc38b1d7d22d82a1ebadb99c38c - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID177453994220220125131310.0001 - DRS record last changed: November 21, 2025 - Page: https://openairdocs.org/ac/36-1 ## Versions - [AC 36-1H](https://openairdocs.org/ac/36-1) (Current), approved May 25, 2012, 364 pages. Change 1 incorporated - [AC 36-1G](https://openairdocs.org/ac/36-1G) (Historical), approved Aug 27, 1997, 179 pages ## Text Each page's text from the PDF; open the PDF at a page with #page=N. ### Page 1 U.S. Department of Transportation Federal Aviation Administration Advisory Circular SUBJECT: Noise Levels for U.S. Certificated and Foreign Aircraft Date: 05/25/2012 Initiated by: AEE-100 AC No: 36-1H Change 1 1. Purpose. a. This Advisory Circular (AC) publishes needed changes to the existing AC material as a result of additions of certificated aircraft noise levels submitted since the AC was published. b. This change revises Appendix 1, U.S Certificated Turbojet Powered Airplanes and Appendix 8, U.S. Certificated Propeller Driven Small Airplanes (14 CFR Part 16, Appendix G), and Appendix 8 Notes. c. The change number and the date of the changed material are shown at the top of each page in Appendix 1, Appendix 8, and Appendix 8 Notes.. 2. Principal Changes. Appendix 1, Appendix 8, and Appendix 8 Notes. 3. Website Availability. To access this AC electronically, go to http://www.faa.gov/regulations_policies/advisory_circulars/ **PAGE CONTROL CHART** Remove Pages Dated Insert Pages Dated Appendix 1 1 thru 53 Appendix 8 1 and 4 11/15/01 11/15/01 Appendix 1 1 thru 186 Appendix 8 1 thru 7 4/24/2012 4/24/2012 ### Page 2 ~~ Advisory u.s. Department of Transportation Circular Federal Aviation Administration Subject: Date: 11/15/01 Initiated by: AEE-100 AC No: 36-1H Change: **NOISE LEVELS FOR U.S. CERTIFICATED** **AND FOREIGN AIRCRAFT** 1. PURPOSE. This circular provides noise level data for aircraft certificated under 14 CFR part 36. Noise level data for foreign aircraft certificated to ICAO Annex 16 standards are also provided in a separate appendix for informational purposes. Other appendices list selected configurations of U.S. certificated aircraft and provide listings of noise levels ranked in descending order. 2. CANCELLATION. Advisory Circular 36-1G, Noise Levels for U.S. Certificated and Foreign Aircraft, dated August 27, 1997, is canceled. 3. BACKGROUND. The agency's regulatory program for aircraft noise requires the quantification of aircraft noise levels. Progress in the control and abatement of aircraft noise continues to be made to achieve further relief and protection to the public. This updated Advisory Circular, containing certificated aircraft noise· levels, will provide both private and public exposure to this progress, as well as offering a common noise level reference for potential future reductions. 4. NOISE LEVELS. Noise levels measured during type certification under 14 CFR part 36 and ICAO Annex 16 are presented in Appendices 1 through 11. Formulas for calculating the appropriate 14 CFR part 36 noise level requirements, as contained in sections C36.5, F36.301, G36.301, H36.305, and 136.305 follow the applicable appendix. Appendix 1 provides noise levels of turbojet powered airplanes, measured during type certification under 14 CFR part 36, Appendix C. This appendix includes tabulations of engine model, maximum takeoff weights, landing weights, flap settings, the "Stage" with which the airplane complies, and the measured noise in Effective Perceived Noise Level (EPNdB). Data are not presented for all of the maximum certificated takeoff weights for each airplane type. Rather, the data presented generally represent the highest and lowest maximum certificated takeoff weight. Airplane noise levels are shown as complying with either Stage 2 or Stage 3. A "Stage 2 airplane" means an airplane that has been shown under 14 CFR part 36 to comply with the Stage 2 noise levels prescribed in section C36.5 of Appendix C (including use of the applicable tradeoff provisions) and that does not comply with the requirements for a Stage 3 airplane. A "Stage 3 airplane" means an airplane that has been shown under 14 CFR part 36 to comply with Stage 3 noise levels prescribed in section C36.5 of Appendix C (including use of the applicable tradeoff provisions). FAA Form 1320-15 (4-82) Supersedes WA Form 1320-2 ### Page 3 As required by Part 36, certification noise levels for approach are those which are most critical from a noise standpoint, for the airplane configurations used to show compliance with the landing requirements in the airworthiness regulations constituting the type certification basis of the airplane. Takeoff certification noise levels are presented for takeoff with thrust cutback unless there is an asterisk (*) in the "NOTES" column, in which case full takeoff thrust certification noise levels are presented. It should be noted that the sideline noise levels are generally presented for the current 450-meter distance. However, some four-engine airplane configurations were certificated to the earlier 650-meter standard; these configurations are denoted with a double asterisk (**) in the "NOTES" column. Since the original measurement locations and noise test conditions cited in 14 CFR part 36, on November 18, 1969, have been amended through the years, the noise levels contained herein are for the measurement locations and noise test conditions applicable at the time of certification. In each case, the measured data have been corrected to sea level, 77 OF, 70% relative humidity conditions using the procedures outlined in 14 CFR part 36. Specific information providing more detail on either the measurement locations or noise test conditions, if available, are indicated by the notes accompanying each listing. Blank spaces or lack of notes in the report indicate the data were not available. Appendix 2 provides noise levels of foreign turbojet powered airplanes certificated to ICAO Annex 16, Chapters 2 and 3. These noise levels are provided for informational purposes. Airplanes certificated to both 14 CFR part 36 and ICAO Annex 16 are only listed in Appendix l. Appendix 3 provides a listing of U.S. certificated Stage 3 turbojet powered airplanes. These airplanes are also included in Appendix 1. Appendix 4 and 5 represent selected listings of noise levels for turbojet powered airplanes certificated under 14 CFR part 36, Appendix C. Appendices 4 and 5 provide listings of takeoff and approach noise levels in EPNdB, respectively, in descending order. Representative models of each airplane are listed, using the maximum takeoff weight available. These listings are presented as a convenience in locating noise level data on specific airplane models. For a more detailed listing on variations of a representative model, see Appendix 1. Appendix 6 contains noise levels of propeller-driven transport category airplanes. Noise levels measured during type certification were obtained under 14 CFR part 36, Appendix C. This appendix includes tabulations of maximum takeoff weights, landing weights, engine type, horsepower, propeller­ type, propeller diameter, and flap settings. The "Stage" with which the airplane complies is also provided, as well as the Effective Perceived Noise Level (EPNdB). Appendix 7 lists the certificated airplane noise levels for propeller-driven small airplanes certificated under 14 CFR part 36, Appendix F. This appendix includes a tabulation of maximum takeoffweights, landing weights, engine type, horsepower, propeller type, and propeller diameter. The measured A-weighted sound levels (dBA) for flyovers have been corrected to sea level 77 OF, 70% relative humidity conditions where required by 14 CFR part 36, Appendix F. ### Page 4 . Burleson 11115/01 AC 36-1H Appendix 8 lists the certificated airplane noise levels for propeller-driven small airplanes and commuter category airplanes certificated under 14 CFR part 36, Appendix G. This appendix includes a tabulation of maximum takeoff weights, landing weights, engine type, horsepower, propeller type and propeller diameter, and the noise level in dB(A). Note that the 14 CFR part 36, Appendix G noise certification requirements for propeller-driven small airplanes and commuter category airplanes superseded those of 14 CFR part 36, Appendix F for noise certification tests conducted on or after December 22, 1988. Appendix 9 contains noise levels for propeller-driven small airplanes certificated under ICAO Annex 16, Chapter 6. These noise levels are listed for informational purposes. Appendix 10 lists the certificated noise levels for helicopters certificated under 14 CFR part 36, Appendix H. Helicopter noise levels are classified as either Stage 1 or Stage 2. A II Stage 2" helicopter means a helicopter that has been shown under 14 CFR part 36 to comply with the Stage 2 noise levels prescribed in section H36.305 of Appendix H (including use of applicable tradeoff provisions). Appendix 11 lists the certificated noise levels for helicopters certificated under 14 CFR part 36, Appendix J. Appendix J prescribes alternative (to 14 CFR part 36 Appendix H) noise certification requirements for helicopters in the primary, normal, transport, and restricted categories having maximum certificated takeoff weight of not more than 6,000 pounds. Appendix 12 defines the abbreviations that are used in this Advisory Circular. 5. Distribution. Requests for additional copies of this Advisory Circular should be sent to: u.s. Department of Transportation Subsequent Distribution Office Ardmore East Business Center 3341 Q 75th Avenue Landover, MD 20785 Requests to be placed on the mailing list to receive future revisions of this Advisory Circular should be sent to: u.S. Department of Transportation Distribution Requirements Section SVC-121.21 Washington, DC 20590. 6. REVISIONS. This Advisory Circular will be revised and updated periodically . 'irector, of Environment and Energy Page 3 ### Page 5 LIST OF APPENDICES Appendix 1 Appendix 2 Appendix 3 Appendix 4 Appendix 5 Appendix 6 Appendix 7 Appendix 8 Appendix 9 Appendix 10 Appendix 11 Appendix 12 Aircraft Noise Data for United States Certificated Turbojet Powered Airplanes Aircraft Noise Data for Foreign Certificated Turbojet Powered Airplanes Stage 3 Turbojet Powered Airplanes Aircraft Noise Certification Levels in Descending EPNdB for US. Certificated Turbojet Powered Airplanes - Takeoff Aircraft Noise Certification Levels in Descending EPNdB for US. Certificated Turbojet Powered Airplanes - Approach Aircraft Noise Data for Propeller Driven Airplanes Certificated in the Transport Category Aircraft Noise Data for US. Certificated Propeller Driven Small Airplanes (14 CFRPart 36, Appendix F) Aircraft Noise Data for US. Certificated Propeller Driven Small Airplanes and Commuter Category Airplanes (14 CFR part 36, Appendix G) ; Aircraft Noise Data for Foreign Certificated Propeller Driven Small Airplanes Aircraft Noise Data for US. Certificated Helicopters (14 CFR part 36, Appendix H) Aircraft Noise Data for US. Certificated Helicopters (14 CFR part 36, Appendix J) Abbreviations Page 4 ### Page 6 04/24/2012 **MANUFACTURER** AEROSPATIALE MODEL SN601 CORVETTE 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **13.90 12.40 JT15D-4 2 2.50 2.68 TO AP FLAPS 15 35 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 80.4 85.4 89.5 3 * AEROSPATIALE SN601 CORVETTE 14.60 13.20 JT15D-4 2 2.50 2.68 15 35 74.0 81.0 90.0 3 AIRBUS A300 B4-605R 330.40 290.00 CF6-80C2A5F 2 61.50 5.00 0 40 87.4 98.8 99.5 3 AIRBUS A300 B4-605R 385.46 319.38 CF6-80C2A5F 2 61.50 5.00 0 40 91.5 98.5 100.0 3 AIRBUS A300B2-1C 291.00 268.00 CF6-50C2-R 2 50.40 4.40 0 25 89.9 97.5 102.9 3 AIRBUS A300B2-1C 313.00 286.60 CF6-50C2-R 2 50.40 4.40 0 25 91.8 97.4 103.1 3 Page 1 ### Page 7 04/24/2012 MANUFACTURER AIRBUS MODEL A300B2-203 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **313.10 286.60 CF6-50-C2 2 51.80 4.30 TO AP FLAPS 16 25 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 91.1 97.9 103.1 3 AIRBUS A300B4-103 347.20 295.40 CF6-50-C2 2 51.80 4.30 16 25 93.6 97.7 103.0 3 AIRBUS A300B4-203 313.05 286.60 CF6-50C2 2 51.80 4.30 0 25 90.5 97.3 102.4 3 31 AIRBUS A300B4-203 363.70 299.83 CF6-50-C2 2 51.80 4.30 0 25 94.0 96.9 102.4 3 31 AIRBUS A300B4-622R 330.00 275.00 PW-4158 2 58.00 4.85 0 40 88.0 98.3 101.3 3 AIRBUS A300B4-622R 385.00 304.50 PW-4158 2 58.00 4.85 0 40 93.1 97.9 101.9 3 Page 2 ### Page 8 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES AIRBUS A310-221 305.60 267.90 JT9D-7R4D1 2 48.00 4.50 15 40 90.5 94.8 100.6 3 AIRBUS A310-304 275.58 261.25 CF6-80C2A2 2 53.50 5.00 0 40 85.7 96.5 98.5 3 AIRBUS A310-304 352.74 286.60 CF6-80C2A2 2 53.50 5.00 0 40 92.9 96.1 98.8 3 AIRBUS A310-324 330.69 271.16 PW-4152 2 52.00 4.85 15 40 90.6 97.2 100.2 3 AIRBUS A318-111 123.46 123.46 CFM56-5B8/P 2 21.60 6.00 10 40 79.1 91.1 93.8 3 AIRBUS A318-111 149.91 126.77 CFM56-5B8/P 2 21.60 6.00 10 40 84.1 90.4 93.9 3 Page 3 ### Page 9 **APPENDIX 1, CHANGE 1** MANUFACTURER AIRBUS MODEL A318-112 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **130.07 123.46 CFM56-5B9/P 2 23.30 5.90 TO AP FLAPS 10 40** TO SL AP NOISE LEVEL (EPNdB) 79.4 92.3 93.8 STAGE 3 NOTES AIRBUS A318-112 149.91 126.77 CFM56-5B9/P 2 23.30 5.90 10 40 83.0 91.9 93.9 3 AIRBUS A319-111 136.69 134.48 CFM56-5B/P w/ Mod No. 2 22.00 5.90 10 40 80.5 91.1 93.2 3 27772 and w/ or w/o Mod No. 38770 (HPC upgrade Kit) or CFM56-5B5/3 (Mod No. 37147) w/ Mod No. 27772 AIRBUS A319-111 136.69 134.48 CFM56-5B5 2 22.00 5.90 10 40 81.0 91.5 92.4 4 AIRBUS A319-111 136.69 134.48 CFM56-5B5/P Mod No. 2 22.00 5.90 10 40 81.2 91.8 93.4 4 25800 w or w/o Mod No. 38770 or CFM56-5B5/3 (Mod No. 37147) AIRBUS A319-111 168.65 137.79 CFM56-5B/P w/ Mod No. 2 22.00 5.90 10 40 87.8 90.0 93.5 4 27772 and w/ or w/o Mod No. 38770 (HPC upgrade Kit) or CFM56-5B5/3 (Mod No. 37147) w/ Mod No. 27772 Page 4 ### Page 10 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** MANUFACTURER AIRBUS MODEL A319-111 1000# MTOW 168.65 1000# MLW 137.79 **ENGINE MODEL CFM56-5B5 NO.** 2 THRUST 1000# **22.00 BPR** **5.90 TO AP FLAPS 10 40** TO SL AP NOISE LEVEL (EPNdB) 88.2 90.5 92.6 STAGE 4 NOTES AIRBUS A319-111 168.65 137.79 CFM56-5B5/P Mod No. 2 22.00 5.90 10 40 88.7 90.6 93.6 4 25800 w or w/o Mod No. 38770 or CFM56-5B5/3 (Mod No. 37147) AIRBUS A319-112 123.45 121.25 CFM56-5B6/P 2 23.50 6.00 10 40 78.5 93.2 93.7 3 AIRBUS A319-112 136.69 134.48 CFM56-5B6 2 23.50 6.00 10 40 80.4 92.4 92.4 4 AIRBUS A319-112 136.69 134.48 CFM56-5B6/2P w/ Mod No. 2 23.50 6.00 10 40 81.5 93.3 94.2 4 25800 & 25530 AIRBUS A319-112 136.69 134.48 CFM56-5B6/2P w/ Mod No. 2 23.50 6.00 10 40 80.8 92.4 93.9 4 26610 and w/ or w/o Mod No. 27772 Page 5 ### Page 11 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** MANUFACTURER AIRBUS AIRBUS MODEL A319-112 A319-112 1000# MTOW 136.69 136.69 1000# MLW 134.48 134.48 ENGINE MODEL CFM56-5B6/P Mod No. 27772 and/or CFM56-5B6/3 Mod No. 37147 w/ Mod No. 27772, w or w/o Mod No. 28342 CFM56-5B6/P w or w/o Mod No. 38770 or CFM56- 5B6/3 (Mod No. 37147) NO. 2 2 THRUST 1000# 23.50 **23.50 BPR** 6.00 **6.00 TO AP FLAPS 10 40 10 40** TO SL AP NOISE LEVEL (EPNdB) 80.4 92.2 93.5 81.0 92.9 93.4 STAGE 4 4 NOTES AIRBUS A319-112 168.65 137.79 CFM56-5B6 2 23.50 6.00 10 40 87.0 91.8 92.6 4 AIRBUS A319-112 168.65 137.79 CFM56-5B6/2P w/ Mod No. 25800 & 25530 2 23.50 6.00 10 40 87.8 92.6 94.5 4 AIRBUS A319-112 168.65 137.79 CFM56-5B6/2P w/ Mod No. 26610 and w/ or w/o Mod No. 27772 2 23.50 6.00 10 40 87.0 91.7 94.0 4 AIRBUS A319-112 168.65 137.79 CFM56-5B6/P Mod No. 27772 and/or CFM56-5B6/3 Mod No. 37147 w/ Mod No. 27772, w or w/o Mod No. 28342 2 23.50 6.00 10 40 86.9 91.4 93.7 4 Page 6 ### Page 12 **APPENDIX 1, CHANGE 1** MANUFACTURER AIRBUS MODEL A319-112 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** 168.65 137.79 CFM56-5B6/P w or w/o Mod No. 38770 or CFM56- 5B6/3 (Mod No. 37147) 2 23.50 6.00 TO AP FLAPS 10 40 TO SL AP NOISE LEVEL (EPNdB) 87.7 92.2 93.6 STAGE 4 NOTES AIRBUS A319-112 166.44 149.91 CFM56-5B6/P 2 23.50 6.00 10 40 86.3 92.0 94.4 3 AIRBUS A319-113 123.46 121.25 CFM56-5A4 2 22.00 6.00 10 40 80.1 93.9 94.0 3 AIRBUS A319-113 136.69 134.48 CFM56-5A4 w/ Mod No. 22495 2 22.00 6.00 10 40 81.6 93.1 94.5 4 AIRBUS A319-113 168.65 137.79 CFM56-5A4 w/ Mod No. 22495 2 22.00 6.00 10 40 89.0 91.9 94.6 4 AIRBUS A319-113 158.73 149.91 CFM56-5A4 2 22.00 6.00 10 40 87.5 93.1 94.8 3 Page 7 ### Page 13 **APPENDIX 1, CHANGE 1** MANUFACTURER AIRBUS MODEL A319-114 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **123.45 121.25 CFM56-5A5 2 23.50 6.00 TO AP FLAPS 10 40** TO SL AP NOISE LEVEL (EPNdB) 79.5 94.9 94.0 STAGE 3 NOTES AIRBUS A319-114 136.69 134.48 CFM56-5A5 w/ Mod No. 22495 2 23.50 6.00 10 40 80.9 94.2 94.5 4 AIRBUS A319-114 168.65 137.79 CFM56-5A5 w/ Mod No. 22495 2 23.50 6.00 10 40 87.4 93.5 94.6 4 AIRBUS A319-114 163.14 149.91 CFM56-5A5 2 23.50 6.00 10 40 86.8 94.2 94.8 3 AIRBUS A319-115 136.69 134.48 CFM56-5B7 and/or CFM56- 5B7/P and/or CFM56-5B7/3, w or w/o Mod No. 28342 2 27.00 10 40 78.8 95.0 93.5 4 AIRBUS A319-115 168.65 137.79 CFM56-5B7 and/or CFM56- 5B7/P and/or CFM56-5B7/3, w or w/o Mod No. 28342 2 27.00 10 40 85.1 94.2 93.7 4 Page 8 ### Page 14 MANUFACTURER 04/24/2012 AIRBUS MODEL A319-131 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **123.46 121.25 V2522-A5 2 22.00 4.90 TO AP FLAPS 10 40** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) AC 36-1H APPENDIX 1, CHANGE 1 79.2 92.5 94.0 3 AIRBUS A319-131 136.69 134.48 IAE V2522-A5 w or w/o Mod No. 37868 2 22.00 4.90 10 40 80.2 91.5 94.2 4 AIRBUS A319-131 168.65 137.79 IAE V2522-A5 w or w/o Mod No. 37868 2 22.00 4.90 10 40 86.6 90.5 94.3 4 AIRBUS A319-131 158.73 149.91 V2522-A5 2 22.00 4.90 10 40 85.3 91.4 94.5 3 AIRBUS A319-132 123.45 121.25 V2524-A5 2 23.50 4.90 10 40 78.5 93.0 94.0 3 AIRBUS A319-132 136.69 134.48 IAE V2524-A5 w or w/o Mod No. 28342 2 23.50 4.80 10 40 79.5 92.2 94.3 4 Page 9 ### Page 15 MANUFACTURER 04/24/2012 AIRBUS MODEL A319-132 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** 168.65 137.79 IAE V2524-A5 w or w/o Mod No. 28342 2 23.50 4.80 TO AP FLAPS 10 40 TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) AC 36-1H APPENDIX 1, CHANGE 1 85.5 91.3 94.4 4 AIRBUS A319-132 166.40 149.91 V2524-A5 2 23.50 4.90 10 40 85.9 91.9 94.5 3 AIRBUS A319-133 136.69 134.48 IAE V2527-A5 w or w/o Mod No. 28342 2 26.50 10 40 78.9 93.0 94.3 4 AIRBUS A319-133 168.65 137.79 IAE V2527-A5 w or w/o Mod No. 28342 2 26.50 10 40 84.6 92.5 94.4 4 AIRBUS A320-211 162.00 142.20 CFM56-5A1 2 25.00 6.00 10 35 87.8 94.3 96.4 3 AIRBUS A320-211 149.90 142.20 CFM56-5A1 2 25.00 6.00 10 35 85.3 94.4 96.4 3 Page 10 ### Page 16 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES AIRBUS A320-214 132.16 127.80 CFM56-5B4/P 2 27.00 5.90 10 35 78.8 95.2 95.5 3 AIRBUS A320-214 182.80 150.00 CFM56-5B4/P 2 27.00 5.90 10 35 88.0 93.7 95.8 3 AIRBUS A320-231 149.90 142.20 V2500.A1 2 25.00 6.00 10 40 84.0 93.0 96.6 3 AIRBUS A320-231 162.00 142.20 V2500.A1 2 25.00 6.00 10 40 86.6 92.8 96.6 3 AIRBUS A320-232/233 145.51 142.20 (A320-232 Mod No. 34041) 2 26.50 4.80 10 40 80.2 91.7 94.3 4 IAE V2527-A5 w or w/o Mod No. 37868 and (A320- 233 Mod No. 34041) IAE V2527E-A5 w or w/o Mod No. 37868 AIRBUS A320-232/233 145.51 142.20 (A320-232) IAE V2527-A5 2 26.50 4.80 10 40 80.2 91.7 94.3 4 w or w/o Mod No. 37868 and (A320-233) IAE V2527E-A5 w or w/o Mod No. 37868 Page 11 ### Page 17 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** MTOW MLW MANUFACTURER MODEL 1000# 1000# ENGINE MODEL AIRBUS A320-232/233 171.96 145.51 (A320-232 Mod No. 34041) IAE V2527-A5 w or w/o Mod No. 37868 and (A320- 233 Mod No. 34041) IAE V2527E-A5 w or w/o Mod No. 37868 AIRBUS A320-232/233 171.96 145.51 (A320-232) IAE V2527-A5 w or w/o Mod No. 37868 and (A320-233) IAE V2527E-A5 w or w/o Mod No. 37868 AIRBUS A321-111 171.96 162.04 CFM56-5B1/2P DAC II C w/ Mod. No. 25800 and 26610, w or w/o Mod No. 27772 NO. 2 THRUST 1000# **26.50 BPR** **4.80 TO AP FLAPS 10 40** TO SL AP NOISE LEVEL (EPNdB) 84.9 91.3 94.4 STAGE 4 NOTES 2 26.50 4.80 10 40 84.9 91.3 94.4 4 2 30.00 5.70 10 25 84.8 96.1 96.8 4 AIRBUS A321-111 171.96 162.04 CFM56-5B1/P and/or 5B1/3 2 30.00 5.70 10 25 83.8 94.4 96.1 4 w/ basic NIP (Mod No. 32871, 33987) AIRBUS A321-111 171.96 162.04 CFM56-5B1/P w/ Mod No. 2 30.00 5.70 10 25 84.3 96.1 96.5 4 27772 (w/ or w/o Mod No. 38770 (HPC Upgrade Kit)) or CFM56-5B1/3 (Mod No. 37147) w/ Mod No. 27772 AIRBUS A321-111 171.96 162.04 CFM56-5B1/P w/ or w/o 2 30.00 5.70 10 25 84.9 96.7 96.6 4 Mod No. 38770 (HPC Upgrade Kit)) or CFM56- 5B1/3 (Mod No. 37147) Page 12 ### Page 18 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** MANUFACTURER AIRBUS AIRBUS MODEL A321-111 A321-111 1000# MTOW 196.21 196.21 1000# MLW 166.45 166.45 ENGINE MODEL CFM56-5B1/2P DAC II C w/ Mod. No. 25800 and 26610, w or w/o Mod No. 27772 CFM56-5B1/P and/or 5B1/3 w/ basic NIP (Mod No. 32871, 33987) NO. 2 2 THRUST 1000# 30.00 **30.00 BPR** 5.70 **5.70 TO AP FLAPS 10 25 10 25** TO SL AP NOISE LEVEL (EPNdB) 89.1 95.6 96.9 **87.8 93.9 96.3 STAGE 4 4 NOTES AIRBUS AIRBUS AIRBUS A321-111 A321-111 A321-112** 196.21 196.21 171.96 166.45 166.45 162.04 CFM56-5B1/P w/ Mod No. 27772 (w/ or w/o Mod No. 38770 (HPC Upgrade Kit)) or CFM56-5B1/3 (Mod No. 37147) w/ Mod No. 27772 CFM56-5B1/P w/ or w/o Mod No. 38770 (HPC Upgrade Kit)) or CFM56- 5B1/3 (Mod No. 37147) CFM56-5B2 2 2 2 30.00 30.00 31.00 5.70 5.70 5.60 10 10 10 25 25 25 88.8 89.5 84.3 95.6 96.2 95.8 96.6 96.8 95.7 4 3 4 AIRBUS A321-112 171.96 162.04 CFM56-5B2/P w/ Mod No. 27772 (w/ or w/o Mod No. 38770 (HPC Upgrade Kit)) or CFM56-5B2/3 (Mod No. 37147) w/ Mod No. 27772 2 31.00 5.60 10 25 84.1 96.7 96.5 4 Page 13 ### Page 19 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** MANUFACTURER AIRBUS AIRBUS MODEL A321-112 A321-112 1000# MTOW 171.96 196.21 1000# MLW 162.04 166.45 ENGINE MODEL CFM56-5B2/P w/ or w/o Mod No. 38770 (HPC Upgrade Kit)) or CFM56- 5B2/3 (Mod No. 37147) CFM56-5B2 NO. 2 2 THRUST 1000# 31.00 **31.00 BPR** 5.60 **5.60 TO AP FLAPS 10 25 10 25** TO SL AP NOISE LEVEL (EPNdB) 84.7 97.3 96.6 **88.6 95.4 95.9 STAGE 3 4 NOTES AIRBUS AIRBUS AIRBUS A321-112 A321-112 A321-211** 196.21 196.21 165.34 166.45 166.45 143.29 CFM56-5B2/P w/ Mod No. 27772 (w/ or w/o Mod No. 38770 (HPC Upgrade Kit)) or CFM56-5B2/3 (Mod No. 37147) w/ Mod No. 27772 CFM56-5B2/P w/ or w/o Mod No. 38770 (HPC Upgrade Kit)) or CFM56- 5B2/3 (Mod No. 37147) CFM56-5B3/P; Mod. No. 27772 2 2 2 31.00 31.00 32.00 5.60 5.60 5.60 10 10 25 25 25 88.4 89.2 82.9 96.2 96.8 97.9 96.6 96.8 95.6 4 3 3 AIRBUS A321-211 205.02 171.51 CFM56-5B3/P; Mod. No. 27772 2 32.00 5.60 25 89.8 97.5 96.6 3 Page 14 ### Page 20 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** MANUFACTURER AIRBUS MODEL A321-212 1000# MTOW 171.96 1000# MLW 162.04 ENGINE MODEL CFM56-5B1/2P DAC II C w/ Mod. No. 25800 and 26610, w or w/o Mod No. 27772 NO. 2 THRUST 1000# **30.00 BPR** **5.60 TO AP FLAPS 10 25** TO SL AP NOISE LEVEL (EPNdB) 84.8 96.1 96.8 STAGE 4 NOTES AIRBUS A321-212 171.96 162.04 CFM56-5B1/P and/or 5B1/3 w/ basic NIP (Mod No. **32871, 33987) 2 30.00 5.60 10 25 83.8 94.4 96.1 4 AIRBUS AIRBUS A321-212 A321-212** 171.96 171.96 162.04 162.04 CFM56-5B1/P w/ Mod No. 27772 (w/ or w/o Mod No. 38770 (HPC Upgrade Kit)) or CFM56-5B1/3 (Mod No. 37147) w/ Mod No. 27772 CFM56-5B1/P w/ or w/o Mod No. 38770 (HPC Upgrade Kit)) or CFM56- 5B1/3 (Mod No. 37147) 2 2 30.00 30.00 5.60 5.60 10 10 25 25 84.3 84.9 96.1 96.7 96.5 96.6 4 4 AIRBUS A321-212 206.13 171.52 CFM56-5B1/2P DAC II C w/ Mod. No. 25800 and 26610, w or w/o Mod No. 27772 2 30.00 5.60 10 25 91.1 95.1 97.0 3 AIRBUS A321-212 206.13 171.52 CFM56-5B1/P and/or 5B1/3 w/ basic NIP (Mod No. 32871, 33987) 2 30.00 5.60 10 25 89.5 93.4 96.6 4 Page 15 ### Page 21 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** MANUFACTURER MODEL 1000# MTOW 1000# MLW ENGINE MODEL NO. THRUST 1000# BPR TO AP FLAPS TO SL AP NOISE LEVEL (EPNdB) STAGE NOTES AIRBUS A321-212 206.13 171.52 CFM56-5B1/P w/ Mod No. 27772 (w/ or w/o Mod No. 38770 (HPC Upgrade Kit)) or CFM56-5B1/3 (Mod No. 37147) w/ Mod No. 27772 2 30.00 5.60 10 25 90.9 95.1 96.8 3 AIRBUS A321-212 206.13 171.52 CFM56-5B1/P w/ or w/o Mod No. 38770 (HPC Upgrade Kit)) or CFM56- 5B1/3 (Mod No. 37147) 2 30.00 5.60 10 25 91.6 91.8 97.0 3 AIRBUS A321-213 171.96 162.04 CFM56-5B2/P w/ Mod No. 2 31.00 5.60 10 25 84.1 96.7 96.5 4 27772 (w/ or w/o Mod No. 38770 (HPC Upgrade Kit)) or CFM56-5B2/3 (Mod No. 37147) w/ Mod No. 27772 AIRBUS A321-213 171.96 162.04 CFM56-5B2/P w/ or w/o 2 31.00 5.60 10 25 84.7 97.3 96.6 3 Mod No. 38770 (HPC Upgrade Kit)) or CFM56- 5B2/3 (Mod No. 37147) AIRBUS A321-213 206.13 171.52 CFM56-5B2/P w/ Mod No. 2 31.00 5.60 10 25 90.3 96.1 96.8 3 27772 (w/ or w/o Mod No. 38770 (HPC Upgrade Kit)) or CFM56-5B2/3 (Mod No. 37147) w/ Mod No. 27772 AIRBUS A321-213 206.13 171.52 CFM56-5B2/P w/ or w/o 2 31.00 5.60 10 25 91.0 96.7 97.0 3 Mod No. 38770 (HPC Upgrade Kit)) or CFM56- 5B2/3 (Mod No. 37147) Page 16 ### Page 22 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES AIRBUS A321-231 165.34 143.29 V2533A5 2 33.00 4.46 25 81.8 95.6 95.1 3 AIRBUS A321-231 205.02 171.51 V2533A5 2 33.00 4.46 25 88.2 95.2 95.8 3 AIRBUS A330-301 396.83 361.56 CF6-80E1A2 2 65.80 5.05 14 32 87.0 97.9 98.5 3 AIRBUS A330-301 507.06 418.88 CF6-80E1A2 2 65.80 5.05 14 32 94.2 97.2 98.7 3 AIRBUS A330-321 396.83 330.69 PW4164 2 64.00 4.85 8 32 88.5 98.0 97.3 3 AIRBUS A330-321 507.06 418.88 PW4164 2 64.00 4.85 8 32 95.6 97.5 98.0 3 Page 17 ### Page 23 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES AIRBUS A330-322 396.83 330.69 PW4168 2 68.00 4.85 8 32 87.6 98.6 97.3 3 AIRBUS A330-322 507.06 418.88 PW4168 2 68.00 4.85 8 32 94.3 98.3 98.0 3 AIRBUS A340-212 485.01 363.76 CFM56-5C3 4 32.50 6.60 17 32 88.1 95.8 97.3 3 AIRBUS A340-212 595.25 440.92 CFM56-5C3 4 32.50 6.60 17 32 96.1 95.4 97.2 3 AIRBUS A340-312 485.02 363.76 CFM56-5C3 4 32.50 6.60 17 32 88.0 95.8 97.3 3 AIRBUS A340-312 595.24 440.92 CFM56-5C3 4 32.50 6.60 17 32 96.2 95.3 97.2 3 Page 18 ### Page 24 MANUFACTURER 04/24/2012 AIRBUS MODEL A340-541 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **672.41 485.02 RR TRENT 553 4 55.78 7.70 TO AP FLAPS 17 34** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) AC 36-1H APPENDIX 1, CHANGE 1 88.9 95.7 99.3 3 AIRBUS A340-541 870.83 595.25 RR TRENT 553 4 55.78 7.70 17 34 96.9 94.9 99.5 3 AIRBUS A380-841 1254.43 862.01 RR TRENT 970 4 78.30 8.70 8 23 94.8 95.2 98.0 4 AIRBUS A380-841 1254.40 862.01 RR TRENT 970 w/ Post TC Mod No. 65283 4 78.30 8.70 8 23 95.6 94.2 98.0 4 AIRBUS A380-841 1124.36 868.62 RR TRENT 970 4 78.30 8.70 8 23 91.2 95.2 98.0 4 AIRBUS A380-841 1124.40 868.62 RR TRENT 970 w/ Post TC Mod No. 65283 4 78.30 8.70 8 23 91.9 94.6 98.1 4 Page 19 ### Page 25 MANUFACTURER 04/24/2012 AIRBUS MODEL A380-842 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW 1254.43 862.01 RR TRENT 972 4 80.21 8.60 TO AP FLAPS 8 23** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) AC 36-1H APPENDIX 1, CHANGE 1 94.3 95.3 98.0 4 AIRBUS A380-842 1254.40 862.01 RR TRENT 972 w/ Post TC Mod No. 65283 4 80.21 8.60 8 23 95.1 94.6 98.0 4 AIRBUS A380-842 1124.36 868.62 RR TRENT 972 4 80.21 8.60 8 23 90.9 95.6 98.0 4 AIRBUS A380-842 1124.40 868.62 RR TRENT 972 w/ Post TC Mod No. 65283 4 80.21 8.60 8 23 91.5 94.9 98.1 4 AIRBUS UK 1-11 200 80.00 71.00 SPEY 506-14 2 10.40 1.00 3 45 93.3 99.1 97.8 2 12 AIRBUS UK 1-11 400 87.00 77.20 SPEY511-14/14W 2 11.40 0.70 0 45 94.8 103.4 99.7 2 12 Page 20 ### Page 26 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES AIRBUS UK 1-11 400 89.50 79.00 SPEY511-14/14W 2 11.40 0.70 0 45 95.7 103.3 99.9 2 12 AIRBUS UK 1-11 400 (QTV STC: ST02167AT) 81.90 78.00 SPEY511-14/14W 2 11.40 0.70 26 90.0 96.2 93.8 3 BAE SYSTEMS (AVRO) 146-RJ 100 95.00 83.00 LF 507-1F 4 7.00 5.10 18 33 83.8 88.3 97.2 3 BAE SYSTEMS (AVRO) 146-RJ 100 101.50 88.50 LF 507-1F 4 7.00 5.10 18 33 86.1 88.1 97.6 3 BAE SYSTEMS (AVRO) 146-RJ 70 84.00 83.50 LF 507-1F 4 6.13 5.10 18 33 81.9 87.2 97.5 3 BAE SYSTEMS (AVRO) 146-RJ 70 95.00 83.50 LF 507-1F 4 7.00 5.10 18 33 83.6 88.6 97.5 3 4 Page 21 ### Page 27 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BAE SYSTEMS (AVRO) 146-RJ 70 84.00 83.50 LF 507-1F 4 7.00 5.10 18 33 80.2 89.1 97.5 3 4 BAE SYSTEMS (AVRO) 146-RJ 70 90.00 83.50 LF 507-1F 4 6.13 5.10 18 33 84.1 86.9 97.5 3 BAE SYSTEMS (AVRO) 146-RJ 85 89.50 77.50 LF 507-1F 4 7.00 5.10 18 33 81.9 88.7 96.9 3 BAE SYSTEMS (AVRO) 146-RJ 85 97.00 85.00 LF 507-1F 4 7.00 5.10 18 33 84.3 88.4 97.3 3 BAE SYSTEMS (BAe) 146-100A 76.00 72.35 ALF502R-3 4 6.70 5.90 18 33 80.7 87.2 95.1 3 BAE SYSTEMS (BAe) 146-100A 76.00 72.35 ALF502R-3A 4 6.70 5.90 18 33 79.0 88.0 94.9 3 Page 22 ### Page 28 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BAE SYSTEMS (BAe) 146-100A 82.25 73.35 ALF502R-3A 4 6.70 5.90 18 33 82.3 87.6 95.2 3 BAE SYSTEMS (BAe) 146-100A 82.25 73.35 ALF502R-5 4 6.97 5.70 18 33 82.3 87.6 95.2 3 BAE SYSTEMS (BAe) 146-100A 84.00 77.50 ALF502R-5 4 6.97 5.70 18 33 81.8 87.7 95.6 3 BAE SYSTEMS (BAe) 146-200A 89.50 77.50 ALF502R-3 4 6.97 5.90 18 33 85.9 86.6 95.6 3 BAE SYSTEMS (BAe) 146-200A 89.50 77.50 ALF502R-3A 4 6.70 5.90 18 33 84.9 87.3 95.6 3 BAE SYSTEMS (BAe) 146-200A 89.50 77.50 ALF502R-5 4 6.97 5.70 18 33 84.9 87.3 95.6 3 Page 23 ### Page 29 04/24/2012 MANUFACTURER BAE SYSTEMS (BAe) MODEL 146-200A 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **93.00 81.00 ALF502R-5 4 6.97 5.70 TO AP FLAPS 18 33 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 85.2 87.3 95.8 3 BAE SYSTEMS (BAe) 146-300 95.00 83.00 LF 507-1H/-1F 4 7.00 5.10 18 33 84.0 87.9 97.2 3 BAE SYSTEMS (BAe) 146-300 101.50 88.50 LF 507-1H/-1F 4 7.00 5.10 18 33 86.3 87.6 97.6 3 BAE SYSTEMS (BAe) 146-300A 95.00 83.00 ALF 502R-5 4 6.97 5.70 18 33 86.0 87.0 96.0 3 BAE SYSTEMS (BAe) 146-300A 97.50 84.50 ALF502R-5 4 6.97 5.70 18 33 86.5 86.7 95.6 3 BEECH BEECHJET 400 15.78 14.22 JT15D-5 2 2.90 2.10 10 30 88.6 93.7 91.4 3 * Page 24 ### Page 30 **APPENDIX 1, CHANGE 1** MANUFACTURER BOEING MODEL 727-100RE (RHOR STC SA4363NM) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **174.50 142.50 JT8D-217C/JT8D-7 3 TO AP FLAPS 5 30** TO SL AP NOISE LEVEL (EPNdB) **88.4 98.0 95.5 STAGE 3 NOTES BOEING 727-100RE (RHOR STC SA4363NM)** 169.50 142.50 JT8D-217C/JT8D-7 3 5 30 87.4 98.0 95.5 3 BOEING 727-100RE (RHOR STC SA4363NM) 169.50 142.50 JT8D-217C/JT8D-9 3 5 30 87.3 98.1 95.5 3 BOEING 727-100RE (RHOR STC SA4363NM) 174.50 142.50 JT8D-217C/JT8D-9 3 5 30 88.3 98.0 95.5 3 BOEING 727-100RE (RHOR STC SA4363NM) 174.50 142.50 JT8D-219/JT8D-7 3 5 30 87.7 98.9 95.5 3 BOEING B-707-100B (BAC II STC: ST00956LA) 200.00 160.00 JT3D-1 4 17.00 1.40 20 30 95.5 99.5 101.1 3 12 Page 25 ### Page 31 04/24/2012 MANUFACTURER BOEING MODEL B-707-100B (QNC) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **241.30 190.00 JT3D-1 4 TO AP FLAPS 30 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 103.4 102.8 102.8 2 6,** BOEING B-707-100B (QNC) 258.00 190.00 JT3D-3B 4 18.00 1.40 30 103.8 102.7 102.8 2 6,** BOEING B-707-120B (SHANNON) 258.00 190.00 JT3D-1 4 30 103.5 97.6 105.3 2 21,** BOEING B-707-138B (SHANNON) 258.00 190.00 JT3D-1 4 30 103.2 97.6 105.3 2 21,** BOEING B-707-300B ADV/C ( SHN) 322.30 247.00 JT3D-1-3B(IC) 4 14 25 105.5 99.3 105.7 2 6,21,** BOEING B-707-300B ADV/C (QNC) 335.00 247.50 JT3D-3B 4 18.00 1.40 25 104.4 98.9 107.9 2 6,** Page 26 ### Page 32 04/24/2012 MANUFACTURER BOEING MODEL B-707-300B ADV/C (SHN) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **330.00 201.00 JT3D-7 4 19.00 1.40 TO AP FLAPS 25 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 104.7 99.6 108.3 2 6,** BOEING B-707-300B ADV/C (SHN) 321.00 240.00 JT3D-3B 4 18.00 1.40 25 104.5 99.2 108.2 2 6,** BOEING B-707-300B/C (QSI STC: ST00702LA) 215.00 190.00 JT3D-3B 4 18.00 1.40 14 25 96.2 99.6 101.4 3 12 BOEING B-707-300B/C (QSI STC: ST00702LA) 336.00 247.00 JT3D-3B 4 18.00 1.40 14 25 99.5 98.2 102.9 3 12 BOEING B-707-300B/C (QSI STC: ST00702LA) 336.00 247.00 JT3D-7 4 19.00 1.40 14 25 98.5 99.3 102.7 3 12 BOEING B-717-200 104.50 98.00 BR700-715A1-30 2 18.50 4.66 5 40 79.6 89.2 91.3 3 48 Page 27 ### Page 33 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-717-200 104.50 98.00 BR700-715A1-30 (MP) 2 18.50 4.66 5 40 80.1 89.2 91.3 3 49 BOEING B-717-200 104.50 98.00 BR700-715C1-30 2 21.00 4.66 5 40 78.1 91.7 91.3 3 48 BOEING B-717-200 104.50 98.00 BR700-715C1-30 (MP) 2 21.00 4.66 5 40 78.7 91.7 91.3 3 49 BOEING B-717-200 121.00 110.00 BR700-715A1-30 2 18.00 4.66 5 40 84.0 89.0 91.6 3 48 BOEING B-717-200 121.00 110.00 BR700-715A1-30 (MP) 2 18.50 4.66 5 40 84.1 89.0 92.1 3 49 BOEING B-717-200 121.00 110.00 BR700-715C1-30 2 21.00 4.66 5 40 82.1 91.5 91.6 3 48 Page 28 ### Page 34 MANUFACTURER 04/24/2012 BOEING MODEL B-717-200 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **121.00 110.00 BR700-715C1-30 (MP) 2 21.00 4.66 TO AP FLAPS 5 40** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) AC 36-1H APPENDIX 1, CHANGE 1 82.2 91.5 92.1 3 49 BOEING B-720B (QNC) 234.00 175.00 JT3D-1 4 30 102.3 102.9 101.6 2 6,** BOEING B-720B (QNC) 234.00 175.00 JT3D-3B 4 18.00 1.40 30 99.3 103.2 101.6 2 6,** BOEING B-720B (SHANNON) 234.00 175.00 JT3D-1 4 30 98.9 98.0 104.7 2 6,** BOEING B-720B (SHANNON) 234.00 175.00 JT3D-3B 4 18.00 1.40 30 97.3 99.5 104.7 2 6,** BOEING B-727-100 152.50 135.00 JT8D-7FCD 3 14.00 1.40 5 40 94.4 100.3 104.1 2 3,16 Page 29 ### Page 35 MANUFACTURER 04/24/2012 BOEING MODEL B-727-100 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **169.50 137.50 JT8D-1FCD 3 14.00 1.10 TO AP FLAPS 5 40** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) AC 36-1H APPENDIX 1, CHANGE 1 98.5 99.1 104.3 2 3 BOEING B-727-100 160.50 137.50 JT8D-1FCD 3 14.00 1.10 5 40 96.6 99.2 104.3 2 3 BOEING B-727-100 169.50 137.50 JT8D-7FCD 3 14.00 1.40 5 40 97.9 100.0 104.3 2 3,16 BOEING B-727-100 160.50 137.50 JT8D-9FCD 3 14.50 1.03 5 40 96.1 100.2 105.8 2 3,17 BOEING B-727-100 169.50 137.50 JT8D-9FCD 3 14.50 1.03 5 40 98.3 100.0 105.8 2 3,17 BOEING B-727-100 (Dee Howard) 169.50 137.50 TAY 651-54 3 15.40 5 40 92.1 92.3 98.4 3 Page 30 ### Page 36 04/24/2012 MANUFACTURER BOEING MODEL B-727-100 (Dee Howard) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **169.50 142.50 TAY 651-54 3 15.40 TO AP FLAPS 5 30 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 92.1 92.3 95.3 3 BOEING B727-100 (DUGAN AIR STC) 160.50 142.50 JT8D-7 3 14.00 1.40 4 26 93.5 98.6 97.2 3 BOEING B727-100 (DUGAN AIR STC) 174.50 142.50 JT8D-7 3 14.00 1.40 4 26 95.9 99.0 97.2 3 BOEING B727-100 (FED EX; STC SA3993NM) 160.50 137.50 JT8D-7 w/BOEING INLET+CHIN CSD 3 14.00 1.40 5 30 92.5 96.6 97.8 3 35 BOEING B727-100 (FED EX; STC SA3993NM) 163.50 137.50 JT8D-7 w/BOEING INLET+FAN CSD 3 14.00 1.40 5 30 93.2 97.4 97.8 3 35 BOEING B727-100 (FED EX; STC SA3993NM) 169.50 137.50 JT8D-9 w/BOEING INLET+CHIN CSD 3 14.50 1.03 5 30 93.9 97.5 98.1 3 35 Page 31 ### Page 37 **APPENDIX 1, CHANGE 1** MANUFACTURER BOEING MODEL B727-100 (FED EX; STC SA3993NM) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** 169.50 142.50 JT8D-7 w/BOEING INLET+FAN CSD 3 14.00 1.40 TO AP FLAPS 5 30 TO SL AP NOISE LEVEL (EPNdB) 94.5 97.2 98.0 STAGE 3 NOTES 35 BOEING B727-100 (FED EX; STC SA3993NM) 169.50 142.50 JT8D-7 w/BURBANK INLET+ FAN CSD 3 14.00 1.40 5 30 94.1 97.2 98.2 3 35 BOEING B727-100 (FED EX; STC SA3993NM) 169.50 142.50 JT8D-7 w/BURBANK INLET+CHIN CSD 3 14.00 1.40 5 30 94.1 96.6 98.2 3 35 BOEING B727-100 (FED EX; STC SA3993NM) 174.50 142.50 JT8D-9 w/BOEING INLET+CHIN CSD 3 14.50 1.03 5 30 94.1 97.2 98.9 3 35 BOEING B727-100 (FED EX; STC SA3993NM) 169.50 142.50 JT8D-9 w/BOEING INLET+FAN CSD 3 14.50 1.03 5 30 93.9 98.0 98.4 3 35 BOEING B727-100 (FED EX; STC SA3993NM) 174.50 142.50 JT8D-9 w/BURBANK INLET+CHIN CSD 3 14.50 1.03 5 30 94.9 97.1 98.8 3 35 Page 32 ### Page 38 **APPENDIX 1, CHANGE 1** MANUFACTURER BOEING MODEL B727-100 (FED EX; STC SA3993NM) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** 160.50 142.50 JT8D-9 w/BURBANK INLET+CHIN CSD 3 14.50 1.03 TO AP FLAPS 5 30 TO SL AP NOISE LEVEL (EPNdB) 91.7 97.6 98.8 STAGE 3 NOTES 35 BOEING B727-100 (FED EX; STC SA3993NM) 175.50 154.50 JT8D-7 w/BOEING INLET+CHIN CSD 3 14.00 1.40 5 30 96.6 96.9 99.1 3 35 BOEING B727-100 (FED EX; STC SA3993NM) 175.50 154.50 JT8D-7 w/BURBANK INLET+CHIN CSD 3 14.00 1.40 5 30 96.3 96.0 99.1 3 35 BOEING B727-100 (RAISBECK STC ST00448SE) 172.60 142.50 JT8D-7 3 14.00 1.40 5 25 96.6 98.2 97.2 3 16,43 BOEING B727-100 RE (ROHR STC SA4363NM) 174.50 142.50 JT8D-217C/JT8D-9 3 5 30 89.4 98.0 95.4 3 23 BOEING B727-100 RE (ROHR STC SA4363NM) 160.50 142.50 JT8D-217C/JT8D-9 3 5 30 87.0 98.2 95.4 3 23 Page 33 ### Page 39 **APPENDIX 1, CHANGE 1** MANUFACTURER BOEING MODEL B727-100 RE (ROHR STC SA4363NM) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **169.50 142.50 JT8D-219/JT8D-7B 3 TO AP FLAPS 5 30** TO SL AP NOISE LEVEL (EPNdB) **88.1 98.8 95.4 STAGE 3 NOTES 23 BOEING B727-100 RE (ROHR STC SA4363NM)** 174.50 142.50 JT8D-219/JT8D-7B 3 5 30 89.0 98.8 95.4 3 23 BOEING B727-100 RE (ROHR STC SA4363NM) 169.50 142.50 JT8D-219/JT8D-9 3 5 30 88.0 98.9 95.4 3 23 BOEING B727-100 RE (ROHR STC SA4363NM) 174.50 142.50 JT8D-219/JT8D-9 3 5 30 88.8 98.8 95.4 3 23 BOEING B-727-200 184.20 142.50 JT8D-15QN 3 15.50 1.03 5 40 98.8 102.2 103.2 2 2,18 BOEING B-727-200 190.50 142.50 JT8D-15QN 3 15.50 1.03 5 40 100.0 102.2 103.2 2 2,18 Page 34 ### Page 40 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-727-200 190.50 142.50 JT8D-17QN 3 16.00 1.01 5 40 99.6 103.7 103.2 2 2,19 BOEING B-727-200 190.50 142.50 JT8D-17RQN 3 17.40 0.97 5 40 98.9 104.7 103.2 2 2,20 BOEING B-727-200 208.00 142.50 JT8D-17RQN 3 17.40 0.97 5 40 102.4 104.2 103.2 2 2,20 BOEING B-727-200 177.60 142.50 JT8D-7FCD 3 14.00 1.40 5 40 99.8 99.8 106.3 2 3,16 BOEING B-727-200 172.50 142.50 JT8D-7FCD 3 14.00 1.40 15 40 100.0 100.4 106.3 2 3,16 BOEING B-727-200 172.50 142.50 JT8D-7QN 3 14.00 1.40 15 40 100.0 100.4 104.9 2 2,16 Page 35 ### Page 41 04/24/2012 MANUFACTURER BOEING MODEL B-727-200 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **172.50 142.50 JT8D-9QN 3 14.50 1.03 TO AP FLAPS 15 40 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 99.0 100.4 103.2 2 2,17 BOEING B-727-200 184.80 142.50 JT8D-9QN 3 14.50 1.03 15 40 101.5 100.2 103.2 2 2,17 BOEING B-727-200 178.00 150.00 JT8D-9FCD 3 14.50 1.03 5 30 100.7 99.8 105.8 2 3,17 BOEING B-727-200 203.10 158.00 JT8D-17QN 3 16.00 1.01 5 40 102.0 103.5 104.5 2 2,19 BOEING B727-200 (DUGAN AIR STC) 209.41 164.00 JT8D-15 3 15.50 1.03 4 26 97.0 99.5 97.0 3 BOEING B727-200 (DUGAN AIR STC) 190.50 164.00 JT8D-15 3 15.50 1.03 4 26 94.9 99.2 97.0 3 Page 36 ### Page 42 **APPENDIX 1, CHANGE 1** MANUFACTURER BOEING MODEL B727-200 (DUGAN AIR STC) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **190.50 164.00 JT8D-9 3 14.50 1.03 TO AP FLAPS 4 26** TO SL AP NOISE LEVEL (EPNdB) 95.0 98.3 97.0 STAGE 3 NOTES BOEING B727-200 (FED EX; STC SA4833NM) 172.50 148.00 JT8D-9 w/BURBANK INLET+CHIN CSD 3 14.50 1.03 5 30 94.6 97.2 100.1 3 35 BOEING B727-200 (FED EX; STC SA4833NM) 172.50 150.00 JT8D-7 w/BOEING INLET+CHIN CSD 3 14.00 1.40 5 30 95.9 96.3 99.0 3 35 BOEING B727-200 (FED EX; STC SA4833NM) 172.50 150.00 JT8D-7 w/BOEING INLET+FAN CSD 3 14.00 1.40 5 30 95.9 97.0 99.0 3 35 BOEING B727-200 (FED EX; STC SA4833NM) 172.50 150.00 JT8D-7 w/BURBANK INLET+ FAN CSD 3 14.00 1.40 5 30 95.6 96.5 98.9 3 35 BOEING B727-200 (FED EX; STC SA4833NM) 172.50 150.00 JT8D-7 w/BURBANK INLET+CHIN CSD 3 14.00 1.40 5 30 95.6 95.8 98.9 3 35 Page 37 ### Page 43 **APPENDIX 1, CHANGE 1** MANUFACTURER BOEING MODEL B727-200 (FED EX; STC SA4833NM) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** 169.50 150.00 JT8D-9 w/BURBANK INLET+ FAN CSD 3 14.50 1.03 TO AP FLAPS 5 30 TO SL AP NOISE LEVEL (EPNdB) 94.1 97.8 100.2 STAGE 3 NOTES 35 BOEING B727-200 (FED EX; STC SA4833NM) 177.60 154.50 JT8D-7 w/BOEING INLET+CHIN CSD 3 14.00 1.40 5 30 95.2 97.3 99.0 3 35 BOEING B727-200 (FED EX; STC SA4833NM) 177.60 154.50 JT8D-7 w/BOEING INLET+FAN CSD 3 14.00 1.40 5 30 95.2 97.9 99.0 3 35 BOEING B727-200 (FED EX; STC SA4833NM) 178.42 154.50 JT8D-7 w/BURBANK INLET+CHIN CSD 3 14.00 1.40 5 30 97.0 96.0 99.1 3 35 BOEING B727-200 (FED EX; STC SA4833NM) 177.60 154.50 JT8D-9 w/BOEING INLET+CHIN CSD 3 14.50 1.03 5 30 94.7 97.7 99.7 3 35 BOEING B727-200 (FED EX; STC SA4833NM) 171.44 154.50 JT8D-9 w/BOEING INLET+CHIN CSD 3 14.50 1.03 5 30 94.9 97.6 99.9 3 35 Page 38 ### Page 44 **APPENDIX 1, CHANGE 1** MANUFACTURER BOEING MODEL B727-200 (FED EX; STC SA4833NM) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** 165.60 154.50 JT8D-9 w/BOEING INLET+FAN CSD 3 14.50 1.03 TO AP FLAPS 5 30 TO SL AP NOISE LEVEL (EPNdB) 93.7 98.4 99.9 STAGE 3 NOTES 35 BOEING B727-200 (FED EX; STC SA4833NM) 177.60 154.50 JT8D-9 w/BOEING INLET+FAN CSD 3 14.50 1.03 5 30 94.7 98.2 99.7 3 35 BOEING B727-200 (FED EX; STC SA4833NM) 177.60 154.50 JT8D-9 w/BURBANK INLET+ FAN CSD 3 14.50 1.03 5 30 94.1 98.0 100.3 3 35 BOEING B727-200 (FED EX; STC SA4833NM) 177.60 154.50 JT8D-9 w/BURBANK INLET+CHIN CSD 3 14.50 1.03 5 30 94.1 97.5 100.3 3 35 BOEING B727-200 (FED EX; STC SA4833NM) 178.00 161.00 JT8D-7 w/BURBANK INLET+ FAN CSD 3 14.00 1.40 5 30 96.9 96.6 99.4 3 35 BOEING B727-200 (FED EX; STC SA5839NM) 155.00 150.00 JT8D-9 w/BOEING INLET+CHIN CSD 3 14.50 1.03 5 30 89.2 97.9 97.4 3 27 Page 39 ### Page 45 **APPENDIX 1, CHANGE 1** MANUFACTURER BOEING MODEL B727-200 (FED EX; STC SA5839NM) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** 155.00 150.00 JT8D-9 w/BOEING INLET+FAN CSD 3 14.50 1.03 TO AP FLAPS 5 30 TO SL AP NOISE LEVEL (EPNdB) 89.2 98.4 97.4 STAGE 3 NOTES 27 BOEING B727-200 (FED EX; STC SA5839NM) 155.00 150.00 JT8D-9 w/BURBANK INLET+ FAN CSD 3 14.50 1.03 5 30 88.5 98.1 98.0 3 27 BOEING B727-200 (FED EX; STC SA5839NM) 155.00 150.00 JT8D-9 w/BURBANK INLET+CHIN CSD 3 14.50 1.03 5 30 88.5 97.6 98.0 3 27 BOEING B727-200 (FED EX; STC SA5839NM) 160.00 154.50 JT8D-15 w/BOEING INLET+CHIN CSD 3 15.50 1.03 5 30 92.2 98.0 97.6 3 27 BOEING B727-200 (FED EX; STC SA5839NM) 160.00 154.50 JT8D-15 w/BOEING INLET+FAN CSD 3 15.50 1.03 5 30 92.2 98.2 97.6 3 27 BOEING B727-200 (FED EX; STC SA5839NM) 178.90 154.50 JT8D-15 w/BURBANK INLET+ FAN CSD 3 15.50 1.03 5 30 94.3 97.3 98.2 3 27 Page 40 ### Page 46 **APPENDIX 1, CHANGE 1** MANUFACTURER BOEING MODEL B727-200 (FED EX; STC SA5839NM) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** 184.20 154.50 JT8D-17 w/BOEING INLET+CHIN OR FAN CSD 3 16.00 1.01 TO AP FLAPS 5 30 TO SL AP NOISE LEVEL (EPNdB) 95.3 98.8 97.6 STAGE 3 NOTES 27 BOEING B727-200 (FED EX; STC SA5839NM) 184.20 154.50 JT8D-17 w/BURBANK INLET+CHIN OR FAN CSD 3 16.00 1.01 5 30 94.8 98.6 98.2 3 27 BOEING B727-200 (FED EX; STC SA5839NM) 197.00 154.50 JT8D-17R w/BOEING INLET+CHIN OR FAN CSD 3 17.40 0.97 5 30 96.0 99.4 97.6 3 27 BOEING B727-200 (FED EX; STC SA5839NM) 190.50 154.50 JT8D-17R w/BOEING INLET+CHIN OR FAN CSD 3 17.40 0.97 5 30 96.4 99.2 97.6 3 27 BOEING B727-200 (FED EX; STC SA5839NM) 184.50 154.50 JT8D-17R w/BURBANK INLET+CHIN OR FAN CSD 3 17.40 0.97 5 30 94.8 99.1 98.2 3 27 BOEING B727-200 (FED EX; STC SA5839NM) 204.50 159.00 JT8D-17 w/BURBANK INLET+CHIN OR FAN CSD 3 16.00 1.01 5 30 97.7 98.6 98.4 3 27 Page 41 ### Page 47 **APPENDIX 1, CHANGE 1** MANUFACTURER BOEING MODEL B727-200 (FED EX; STC SA5839NM) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** 191.20 160.00 JT8D-9 w/BURBANK INLET+ FAN CSD 3 14.50 1.03 TO AP FLAPS 5 30 TO SL AP NOISE LEVEL (EPNdB) 97.4 96.3 98.5 STAGE 3 NOTES 27 BOEING B727-200 (FED EX; STC SA5839NM) 191.20 160.00 JT8D-9 w/BURBANK INLET+CHIN CSD 3 14.50 1.03 5 30 97.4 95.7 98.5 3 27 BOEING B727-200 (FED EX; STC SA5839NM) 197.50 161.00 JT8D-17R w/BURBANK INLET+CHIN OR FAN CSD 3 17.40 0.97 5 30 96.9 98.8 98.4 3 27 BOEING B727-200 (FED EX; STC SA5839NM) 199.05 166.00 JT8D-15 w/BOEING INLET+CHIN CSD 3 15.50 1.03 5 30 97.6 98.0 98.1 3 27 BOEING B727-200 (FED EX; STC SA5839NM) 199.05 166.00 JT8D-15 w/BOEING INLET+FAN CSD 3 15.50 1.03 5 30 97.6 98.2 98.1 3 27 BOEING B727-200 (FED EX; STC SA5839NM) 201.00 166.00 JT8D-15 w/BURBANK INLET+ FAN CSD 3 15.50 1.03 5 30 97.7 97.6 98.6 3 27 Page 42 ### Page 48 **APPENDIX 1, CHANGE 1** MANUFACTURER BOEING MODEL B727-200 (FED EX; STC SA5839NM) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** 203.10 166.00 JT8D-17 w/BOEING INLET+CHIN OR FAN CSD 3 16.00 1.01 TO AP FLAPS 5 30 TO SL AP NOISE LEVEL (EPNdB) 96.8 99.1 98.0 STAGE 3 NOTES 27 BOEING B727-200 (FED EX; STC SA5839NM) 196.00 166.00 JT8D-9 w/BOEING INLET+CHIN CSD 3 14.50 1.03 5 30 97.5 96.1 98.0 3 27 BOEING B727-200 (FED EX; STC SA5839NM) 196.00 166.00 JT8D-9 w/BOEING INLET+FAN CSD 3 14.50 1.03 5 30 97.5 96.6 98.0 3 27 BOEING B727-200 (RAISBECK STC ST00399SE) 166.40 153.30 JT8D-9 3 14.50 1.03 5 25 96.5 97.9 97.6 3 17,34,43 BOEING B727-200 (RAISBECK STC ST00555SE) 179.70 166.00 JT8D-9 3 14.50 1.03 5 30 97.0 97.6 97.2 3 34,44 BOEING B727-200 (RAISBECK STC ST00685SE) 193.00 161.00 JT8D-15 3 15.50 1.03 5 30 97.4 96.5 99.9 3 45 Page 43 ### Page 49 **APPENDIX 1, CHANGE 1** MANUFACTURER BOEING MODEL B-727-200 RE (ROHR STC SA4363NM) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **190.50 152.50 JT8D-219/JT8D-9 3 TO AP FLAPS 5 30** TO SL AP NOISE LEVEL (EPNdB) **90.9 99.2 98.8 STAGE 3 NOTES 23,60 BOEING B-727-200 RE (ROHR STC SA4363NM)** 184.00 156.00 JT8D-217C/JT8D-15 3 5 30 89.8 99.2 98.9 3 23,61 BOEING B-727-200 RE (ROHR STC SA4363NM) 184.00 156.00 JT8D-217C/JT8D-9 3 5 30 90.2 98.4 98.9 3 23,60 BOEING B-727-200 RE (ROHR STC SA4363NM) 190.50 159.00 JT8D-217C/JT8D-17 3 5 30 91.2 99.3 99.0 3 23,62 BOEING B-727-200 RE (ROHR STC SA4363NM) 197.00 159.00 JT8D-219/JT8D-15 3 5 30 92.8 99.5 99.0 3 7,23,64 BOEING B-727-200 RE (ROHR STC SA4363NM) 209.50 162.00 JT8D-217C/JT8D-17 3 5 30 95.2 99.2 99.0 3 23,62 Page 44 ### Page 50 **APPENDIX 1, CHANGE 1** MANUFACTURER BOEING MODEL B-727-200 RE (ROHR STC SA4363NM) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **198.50 162.00 JT8D-217C/JT8D-9 3 TO AP FLAPS 5 30** TO SL AP NOISE LEVEL (EPNdB) **93.7 98.2 99.0 STAGE 3 NOTES 23,60 BOEING B-727-200 RE (ROHR STC SA4363NM)** 198.70 162.00 JT8D-219/JT8D-15 3 5 30 92.7 99.4 99.0 3 7,23,64 BOEING B-727-200 RE (ROHR STC SA4363NM) 198.70 162.00 JT8D-219/JT8D-17 3 5 30 92.8 99.5 98.9 3 23 BOEING B-727-200 RE (ROHR STC SA4363NM) 198.70 162.00 JT8D-219/JT8D-9 3 5 30 93.0 99.1 99.0 3 23,60 BOEING B-727-200 RE (ROHR STC SA4363NM) 198.70 162.00 JT8D-219/JT8D-9 3 5 30 92.7 99.5 99.0 3 7,23,63 BOEING B-727-200 RE (ROHR STC SA4363NM) 209.42 164.00 JT8D-217C/JT8D-15 3 5 30 95.3 98.8 99.1 3 23,61 Page 45 ### Page 51 **APPENDIX 1, CHANGE 1** MANUFACTURER BOEING MODEL B-727-200 RE (ROHR STC SA4363NM) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **203.10 164.00 JT8D-217C/JT8D-17A 3 TO AP FLAPS 5 30** TO SL AP NOISE LEVEL (EPNdB) 93.4 99.6 99.3 STAGE 3 NOTES 23 BOEING B-737-200 (AVAERO;STC ST223CH) 128.10 88.00 JT8D-17 2 16.00 1.01 1 40 91.4 97.5 96.7 3 27 BOEING B-737-200 (AVAERO;STC ST223CH) 117.00 90.00 JT8D-15 2 15.50 1.03 1 40 89.7 96.7 98.1 3 35,42 BOEING B-737-200 (AVAERO;STC ST223CH) 128.10 93.00 JT8D-15 2 15.50 1.03 1 40 92.1 96.5 97.1 3 27,42 BOEING B-737-200 (AVAERO;STC ST223CH) 100.80 95.00 JT8D-15 2 15.50 1.03 1 40 83.7 96.8 97.2 3 27,42 BOEING B-737-200 (AVAERO;STC ST223CH) 100.80 95.00 JT8D-9 2 14.50 1.03 1 40 85.2 95.5 97.2 3 27,41 Page 46 ### Page 52 **APPENDIX 1, CHANGE 1** MANUFACTURER BOEING MODEL B-737-200 (AVAERO;STC ST223CH) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **100.50 98.00 JT8D-15 2 15.50 1.03 TO AP FLAPS 1 40** TO SL AP NOISE LEVEL (EPNdB) 84.9 96.9 98.6 STAGE 3 NOTES 35,42 BOEING B-737-200 (AVAERO;STC ST223CH) 100.50 98.00 JT8D-9 2 14.50 1.03 1 40 86.3 95.7 98.6 3 35,41 BOEING B-737-200 (AVAERO;STC ST223CH) 121.50 107.00 JT8D-15 2 15.50 1.03 1 30 91.3 96.9 96.3 3 35,42 BOEING B-737-200 (AVAERO;STC ST223CH) 128.10 107.00 JT8D-15 2 15.50 1.03 1 30 92.1 96.5 94.8 3 27,42 BOEING B-737-200 (AVAERO;STC ST223CH) 115.00 107.00 JT8D-17 2 16.00 1.01 1 40 87.6 97.5 98.0 3 27 BOEING B-737-200 (AVAERO;STC ST223CH) 128.10 107.00 JT8D-17 2 16.00 1.01 1 30 91.4 97.5 94.8 3 27 Page 47 ### Page 53 **APPENDIX 1, CHANGE 1** MANUFACTURER BOEING MODEL B-737-200 (AVAERO;STC ST223CH) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **118.50 107.00 JT8D-9 2 14.50 1.03 TO AP FLAPS 1 30** TO SL AP NOISE LEVEL (EPNdB) 91.5 94.9 96.3 STAGE 3 NOTES 35,41 BOEING B-737-200 (AVAERO;STC ST223CH) 121.50 107.00 JT8D-9 2 14.50 1.03 1 40 91.5 94.8 98.0 3 27,41 BOEING B-737-200 (NORDAM;STC ST00131SE) 103.50 98.00 JT8D-15 w/LGW HUSHKIT 2 15.50 1.03 1 30 86.4 97.1 95.9 3 37 BOEING B-737-200 (NORDAM;STC ST00131SE) 103.50 98.00 JT8D-15 w/LGW-L HUSHKIT 2 15.50 1.03 1 30 85.7 97.1 95.7 3 37 BOEING B-737-200 (NORDAM;STC ST00131SE) 119.50 103.00 JT8D-15 w/LGW HUSHKIT 2 15.50 1.03 1 30 91.1 97.0 95.8 3 37 BOEING B-737-200 (NORDAM;STC ST00131SE) 119.50 103.00 JT8D-15 w/LGW-L HUSHKIT 2 15.50 1.03 1 30 90.2 96.8 95.8 3 37 Page 48 ### Page 54 **APPENDIX 1, CHANGE 1** MANUFACTURER BOEING MODEL B-737-200 ADV (NORDAM; STC SA5730NM) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **110.20 98.00 JT8D-9 2 14.50 1.03 TO AP FLAPS 1 40** TO SL AP NOISE LEVEL (EPNdB) 87.3 94.7 98.2 STAGE 3 NOTES 27,41 BOEING B-737-200 ADV (NORDAM; **STC SA5730NM)** 105.60 103.00 JT8D-15 2 15.50 1.03 1 40 84.6 96.3 98.4 3 27,42 BOEING B-737-200 ADV (NORDAM; **STC SA5730NM)** 115.50 103.00 JT8D-17 2 16.00 1.01 1 40 86.8 97.0 98.4 3 27 BOEING B-737-200 ADV (NORDAM; **STC SA5730NM)** 126.70 107.00 JT8D-15 2 15.50 1.03 1 40 91.0 96.0 98.6 3 27,42 BOEING B-737-200 ADV (NORDAM; **STC SA5730NM)** 126.50 107.00 JT8D-17 2 16.00 1.01 1 40 90.0 96.9 98.6 3 27 BOEING B-737-200 ADV (NORDAM; **STC SA5730NM)** 124.50 107.00 JT8D-9 2 14.50 1.03 1 40 91.9 94.4 98.6 3 27,41 Page 49 ### Page 55 **APPENDIX 1, CHANGE 1** MANUFACTURER BOEING MODEL B-737-200 ADV (NORDAM; STC ST00131SE) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** 100.50 95.00 JT8D-9 w/LGW HUSHKIT 2 14.50 1.03 TO AP FLAPS 1 30 TO SL AP NOISE LEVEL (EPNdB) 86.1 96.7 96.2 STAGE 3 NOTES 36 BOEING B-737-200 ADV (NORDAM; **STC ST00131SE)** 103.50 98.00 JT8D-15 w/LGW HUSHKIT 2 15.50 1.03 1 30 86.4 97.1 96.0 3 37 BOEING B-737-200 ADV (NORDAM; **STC ST00131SE)** 103.50 98.00 JT8D-15 w/LGW-L HUSHKIT 2 15.50 1.03 1 30 85.7 97.1 95.8 3 37 BOEING B-737-200 ADV (NORDAM; **STC ST00131SE)** 115.50 98.00 JT8D-17/-17A w/LGW HUSHKIT 2 16.00 1.01 1 30 89.7 97.5 96.0 3 BOEING B-737-200 ADV (NORDAM; **STC ST00131SE)** 109.00 98.00 JT8D-7 w/LGW-N HUSHKIT 2 14.00 1.40 1 30 89.2 96.3 96.2 3 40 BOEING B-737-200 ADV (NORDAM; **STC ST00131SE)** 100.50 98.00 JT8D-9 w/LGW-N HUSHKIT 2 14.50 1.03 1 30 86.1 96.9 96.2 3 36 Page 50 ### Page 56 **APPENDIX 1, CHANGE 1** MANUFACTURER BOEING MODEL B-737-200 ADV (NORDAM; STC ST00131SE) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** 100.50 99.00 JT8D-9 w/LGW-L HUSHKIT 2 14.50 1.03 TO AP FLAPS 1 30 TO SL AP NOISE LEVEL (EPNdB) 86.9 96.5 95.8 STAGE 3 NOTES 36 BOEING B-737-200 ADV (NORDAM; **STC ST00131SE)** 121.60 107.00 JT8D-15 w/LGW HUSHKIT 2 15.50 1.03 1 30 91.7 96.7 95.9 3 37 BOEING B-737-200 ADV (NORDAM; **STC ST00131SE)** 125.90 107.00 JT8D-15 w/LGW-L HUSHKIT 2 15.50 1.03 1 30 91.8 97.0 95.9 3 37 BOEING B-737-200 ADV (NORDAM; **STC ST00131SE)** 120.50 107.00 JT8D-17/-17A w/LGW HUSHKIT 2 16.00 1.01 1 30 90.8 97.6 95.9 3 BOEING B-737-200 ADV (NORDAM; **STC ST00131SE)** 117.00 107.00 JT8D-7 w/LGW-N HUSHKIT 2 14.00 1.40 1 30 91.6 95.9 96.2 3 40 BOEING B-737-200 ADV (NORDAM; **STC ST00131SE)** 118.70 107.00 JT8D-9 w/LGW HUSHKIT 2 14.50 1.03 1 30 91.6 96.1 95.9 3 36 Page 51 ### Page 57 **APPENDIX 1, CHANGE 1** MANUFACTURER BOEING MODEL B-737-200 ADV (NORDAM; STC ST00131SE) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** 122.90 107.00 JT8D-9 w/LGW-L HUSHKIT 2 14.50 1.03 TO AP FLAPS 1 30 TO SL AP NOISE LEVEL (EPNdB) 91.8 96.0 95.9 STAGE 3 NOTES 36 BOEING B-737-200 ADV (NORDAM; **STC ST00131SE)** 118.50 107.00 JT8D-9 w/LGW-N HUSHKIT 2 14.50 1.03 1 30 91.6 96.5 96.2 3 36 BOEING B-737-200 ADV(AVAERO;STC ST223CH) 119.50 88.00 JT8D-15 2 15.50 1.03 1 40 90.3 96.8 97.7 3 35,42 BOEING B-737-200 ADV(AVAERO;STC ST223CH) 100.80 95.00 JT8D-15 2 15.50 1.03 1 40 83.7 96.9 96.9 3 27,42 BOEING B-737-200 ADV(AVAERO;STC ST223CH) 119.50 95.00 JT8D-9 2 14.50 1.03 1 40 91.7 95.0 98.1 3 35,41 BOEING B-737-200 ADV(AVAERO;STC ST223CH) 100.80 95.00 JT8D-9 2 14.50 1.03 1 40 85.3 95.7 96.9 3 27,41 Page 52 ### Page 58 **APPENDIX 1, CHANGE 1** MANUFACTURER BOEING MODEL B-737-200 ADV(AVAERO;STC ST223CH) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **100.50 98.00 JT8D-15 2 15.50 1.03 TO AP FLAPS 1 40** TO SL AP NOISE LEVEL (EPNdB) 85.0 97.0 98.3 STAGE 3 NOTES 35,42 BOEING B-737-200 ADV(AVAERO;STC ST223CH) 128.10 98.00 JT8D-15 2 15.50 1.03 1 40 92.1 96.5 97.1 3 27,42 BOEING B-737-200 ADV(AVAERO;STC ST223CH) 100.50 98.00 JT8D-9 2 14.50 1.03 1 40 86.4 95.8 98.3 3 35,41 BOEING B-737-200 ADV(AVAERO;STC ST223CH) 124.50 107.00 JT8D-15 2 15.50 1.03 1 30 91.8 96.7 96.3 3 35,42 BOEING B-737-200 ADV(AVAERO;STC ST223CH) 128.10 107.00 JT8D-15 2 15.50 1.03 1 30 92.1 96.5 94.8 3 27,42 BOEING B-737-200 ADV(AVAERO;STC ST223CH) 115.00 107.00 JT8D-17 2 16.00 1.01 1 40 87.5 97.5 97.7 3 27 Page 53 ### Page 59 **APPENDIX 1, CHANGE 1** MANUFACTURER BOEING MODEL B-737-200 ADV(AVAERO;STC ST223CH) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **128.10 107.00 JT8D-17 2 16.00 1.01 TO AP FLAPS 1 30** TO SL AP NOISE LEVEL (EPNdB) 91.2 97.7 94.8 STAGE 3 NOTES 27 BOEING B-737-200 ADV(AVAERO;STC ST223CH) 125.00 107.00 JT8D-17 2 16.00 1.01 1 40 90.2 97.5 97.7 3 27 BOEING B-737-200 ADV(AVAERO;STC ST223CH) 121.50 107.00 JT8D-9 2 14.50 1.03 1 40 91.5 95.0 97.7 3 27,41 BOEING B-737-200 ADV(AVAERO;STC ST223CH) 119.50 107.00 JT8D-9 2 14.50 1.03 1 30 91.7 95.0 96.3 3 35,41 BOEING B-737-200 ADV. 128.10 79.10 JT8D-17QN 2 16.00 1.01 1 40 97.0 104.1 102.8 2 2,19 BOEING B-737-200 ADV. 128.10 88.00 JT8D-15QN 2 15.50 1.03 1 40 97.7 102.4 103.8 2 2,18 Page 54 ### Page 60 04/24/2012 **MANUFACTURER BOEING MODEL B-737-200 ADV.** 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **115.50 95.30 JT8D-17QN 2 16.00 1.01 TO AP FLAPS 1 40 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 93.6 104.4 104.5 2 2,19 BOEING B-737-200 ADV. 115.50 101.00 JT8D-15QN 2 15.50 1.03 1 40 94.4 103.1 105.0 2 2,18 BOEING B-737-200 ADV. 115.50 103.00 JT8D-9QN 2 14.50 1.03 1 40 95.3 100.6 105.1 2 2,17 BOEING B-737-200 ADV. 122.50 105.00 JT8D-9QN 2 14.50 1.03 1 40 96.9 99.9 105.3 2 2,17 BOEING B-737-200 NON-ADV. 100.50 95.00 JT8D-7QN 2 14.00 1.40 1 40 92.1 101.7 102.1 2 2,16 BOEING B-737-200 NON-ADV. 109.00 95.00 JT8D-9QN 2 14.50 1.03 1 40 93.2 100.7 104.8 2 2,17 Page 55 ### Page 61 04/24/2012 **MANUFACTURER BOEING MODEL B-737-200 NON-ADV.** 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **109.00 98.00 JT8D-7QN 2 14.00 1.40 TO AP FLAPS 1 40 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 94.7 101.3 102.1 2 2,16 BOEING B-737-200 NON-ADV. 117.00 101.70 JT8D-9QN 2 14.50 1.03 1 40 95.5 100.3 105.3 2 2,17 BOEING B-737-300 124.50 110.00 CFM56-3 w/HWFAP 2 20.00 5.00 1 40 82.4 89.7 98.5 3 BOEING B-737-300 124.50 110.00 CFM56-3 w/HWFAP 2 20.00 5.00 1 40 82.4 89.7 97.4 3 38 BOEING B-737-300 124.50 110.00 CFM56-3 w/HWFAP 2 22.00 5.00 1 40 81.6 91.2 98.5 3 BOEING B-737-300 124.50 110.00 CFM56-3 w/HWFAP 2 22.00 5.00 1 40 81.6 91.2 97.4 3 38 Page 56 ### Page 62 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-737-300 124.50 110.00 CFM56-3-B1 2 20.00 5.00 1 40 84.4 90.4 99.6 3 BOEING B-737-300 124.50 110.00 CFM56-3B-2 2 22.00 4.90 1 40 82.8 92.2 99.6 3 BOEING B-737-300 139.50 121.00 CFM56-3 w/HWFAP 2 20.00 5.00 1 40 85.2 89.2 98.6 3 BOEING B-737-300 139.50 121.00 CFM56-3 w/HWFAP 2 22.00 5.00 1 40 83.9 90.9 97.6 3 38 BOEING B-737-300 139.50 121.00 CFM56-3 w/HWFAP 2 20.00 5.00 1 40 85.2 89.2 97.6 3 38 BOEING B-737-300 139.50 121.00 CFM56-3 w/HWFAP 2 22.00 5.00 1 40 83.9 90.9 98.6 3 Page 57 ### Page 63 **APPENDIX 1, CHANGE 1** MANUFACTURER BOEING MODEL B-737-300 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **139.50 121.00 CFM56-3-B1 2 20.00 5.00 TO AP FLAPS 1 40** TO SL AP NOISE LEVEL (EPNdB) 87.5 89.9 100.1 STAGE 3 NOTES BOEING B-737-300 139.50 121.00 CFM56-3B-2 2 22.00 4.90 1 40 85.7 91.9 100.1 3 BOEING B737-300 124.50 110.00 CFM56-3B2,-3C1 HWFAP @ -3B2 THRUST RATING 2 0.00 0.00 0 40 81.6 91.6 97.2 4 38,52 BOEING B737-300 139.50 121.00 CFM56-3B1,-3B2,-3C1 HWFAP @ -3B1 THRUST RATING 2 0.00 0.00 0 40 86.0 89.5 97.6 4 38,52 BOEING B737-300 138.50 121.00 CFM56-3B1,-3B2,-3C1 HWFAP @ -3B1 THRUST RATING 2 0.00 0.00 0 40 85.7 89.6 97.6 4 38,52 BOEING B737-300 139.50 121.00 CFM56-3B2,-3C1 HWFAP @ -3B2 THRUST RATING 2 0.00 0.00 0 40 84.4 91.1 97.6 4 38,52 Page 58 ### Page 64 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-737-400 130.00 121.00 CFM56-3 w/HWFAP 2 22.00 5.00 5 40 82.8 91.2 98.6 3 BOEING B-737-400 130.00 121.00 CFM56-3 w/HWFAP 2 20.00 5.00 5 40 83.8 89.8 97.7 3 38 BOEING B-737-400 130.00 121.00 CFM56-3 w/HWFAP 2 20.00 5.00 5 40 83.8 89.8 98.6 3 BOEING B-737-400 130.00 121.00 CFM56-3 w/HWFAP 2 22.00 5.00 5 40 82.8 91.2 97.7 3 38 BOEING B-737-400 130.00 121.00 CFM56-3 w/HWFAP 2 23.50 5.00 5 40 82.4 92.1 97.7 3 38 BOEING B-737-400 130.00 121.00 CFM56-3 w/HWFAP 2 23.50 5.00 5 40 82.4 92.1 98.6 3 Page 59 ### Page 65 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-737-400 138.50 121.00 CFM56-3-B1 2 20.00 5.00 5 40 87.2 90.0 100.2 3 BOEING B-737-400 142.50 121.00 CFM56-3-B1 2 20.00 5.00 5 40 88.9 89.6 100.2 3 BOEING B-737-400 138.50 121.00 CFM56-3B-2 2 22.00 4.90 5 40 85.7 92.1 100.2 3 BOEING B-737-400 138.50 121.00 CFM56-3C-1 2 23.50 5.00 5 40 85.0 93.2 100.2 3 BOEING B-737-400 142.50 124.00 CFM56-3 w/HWFAP 2 20.00 5.00 5 40 86.9 88.9 97.7 3 38 BOEING B-737-400 150.00 124.00 CFM56-3 w/HWFAP 2 22.00 5.00 5 40 86.3 90.7 97.7 3 38 Page 60 ### Page 66 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-737-400 150.00 124.00 CFM56-3 w/HWFAP 2 22.00 5.00 5 40 86.3 90.7 98.6 3 BOEING B-737-400 150.00 124.00 CFM56-3 w/HWFAP 2 23.50 5.00 5 40 85.9 91.8 97.7 3 38 BOEING B-737-400 142.50 124.00 CFM56-3 w/HWFAP 2 20.00 5.00 5 40 86.9 88.9 98.6 3 BOEING B-737-400 150.00 124.00 CFM56-3 w/HWFAP 2 23.50 5.00 5 40 85.9 91.8 98.6 3 BOEING B-737-400 150.00 124.00 CFM56-3B-2 2 22.00 4.90 5 40 87.7 91.7 100.2 3 BOEING B-737-400 150.00 124.00 CFM56-3C-1 2 23.50 4.90 5 40 87.1 93.1 100.2 3 Page 61 ### Page 67 **APPENDIX 1, CHANGE 1** MANUFACTURER BOEING MODEL B737-400 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** 125.50 121.00 CFM56-3B2,-3C1 HWFAP @ -3B2 THRUST RATING 2 0.00 0.00 TO AP FLAPS 0 40 TO SL AP NOISE LEVEL (EPNdB) 83.1 91.8 97.8 STAGE 4 NOTES 38 BOEING B737-400 125.50 121.00 CFM56-3C1 HWFAP @ - 3C1 THRUST RATING 2 0.00 0.00 0 40 82.5 93.1 97.8 4 38 BOEING B737-400 150.00 124.00 CFM56-3B2,-3C1 HWFAP @ -3B2 THRUST RATING 2 0.00 0.00 0 40 88.0 90.7 97.9 4 38 BOEING B737-400 150.00 124.00 CFM56-3C1 HWFAP @ - 3C1 THRUST RATING 2 0.00 0.00 0 40 87.1 92.4 97.9 4 38 BOEING B-737-500 108.00 105.00 CFM56-3 w/HWFAP 2 20.00 5.00 5 40 80.4 90.2 97.2 3 38 BOEING B-737-500 108.00 105.00 CFM56-3 w/HWFAP 2 18.50 5.00 5 40 81.0 89.3 98.4 3 Page 62 ### Page 68 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-737-500 108.00 105.00 CFM56-3 w/HWFAP 2 18.50 5.00 5 40 81.0 89.3 97.2 3 38 BOEING B-737-500 108.00 105.00 CFM56-3 w/HWFAP 2 20.00 5.00 5 40 80.4 90.2 98.4 3 BOEING B-737-500 115.50 105.00 CFM56-3-B1 2 20.00 5.00 5 40 82.7 90.8 99.4 3 BOEING B-737-500 115.50 105.00 CFM56-3-B1(R) 2 18.50 5.00 5 40 83.6 89.9 99.4 3 BOEING B-737-500 132.80 114.00 CFM56-3 w/HWFAP 2 18.50 5.00 5 40 85.4 88.2 97.6 3 38 BOEING B-737-500 139.00 114.00 CFM56-3 w/HWFAP 2 20.00 5.00 5 40 85.4 89.2 97.6 3 38 Page 63 ### Page 69 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-737-500 139.00 114.00 CFM56-3 w/HWFAP 2 20.00 5.00 5 40 85.4 89.2 98.7 3 BOEING B-737-500 132.80 114.00 CFM56-3 w/HWFAP 2 20.00 5.00 5 40 85.4 88.2 98.7 3 BOEING B-737-500 139.00 114.00 CFM56-3-B1 2 20.00 5.00 5 40 87.3 90.0 100.0 3 BOEING B-737-500 132.80 114.00 CFM56-3-B1(R) 2 18.50 5.00 5 40 87.7 88.9 100.0 3 BOEING B737-500 108.00 105.00 CFM56-3B1,-3B2,-3C1 2 0.00 0.00 0 40 80.6 89.6 96.9 4 38,52 HWFAP @ 18,500 SLST BOEING B737-500 108.00 105.00 CFM56-3B1,-3B2,-3C1 2 0.00 0.00 0 40 80.6 97.1 90.6 4 38 HWFAP @ -3B1 THRUST RATING Page 64 ### Page 70 **APPENDIX 1, CHANGE 1** MANUFACTURER BOEING MODEL B737-500 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** 132.80 114.00 CFM56-3B1,-3B2,-3C1 HWFAP @ 18,500 SLST 2 0.00 0.00 TO AP FLAPS 0 40 TO SL AP NOISE LEVEL (EPNdB) 86.0 88.6 97.3 STAGE 4 NOTES 38,52 BOEING B737-500 139.00 114.00 CFM56-3B1,-3B2,-3C1 HWFAP @ -3B1 THRUST RATING 2 0.00 0.00 0 40 87.3 89.2 97.5 4 38 BOEING B-737-600 143.50 120.50 CFM56-7B/2 DAC (B18 derate) 2 19.50 5.60 1 40 85.2 88.7 95.8 3 50 BOEING B-737-600 124.00 120.50 CFM56-7B/2 DAC (B18 derate) 2 19.50 5.60 1 40 82.0 89.7 95.8 3 50 BOEING B-737-600 124.00 120.50 CFM56-7B18 2 19.50 5.60 1 40 82.6 90.3 95.5 3 BOEING B-737-600 143.50 120.50 CFM56-7B18 2 19.50 5.60 1 40 85.7 89.3 95.5 3 Page 65 ### Page 71 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-737-600 143.50 120.50 CFM56-7B20 2 20.60 5.60 1 40 85.4 90.7 95.5 3 BOEING B-737-600 124.00 120.50 CFM56-7B20 2 20.60 5.60 1 40 81.9 91.3 95.5 3 BOEING B-737-600 124.00 120.50 CFM56-7B20/2 DAC 2 20.60 5.60 1 40 81.3 90.7 95.8 3 50 BOEING B-737-600 143.50 120.50 CFM56-7B20/2 DAC 2 20.60 5.60 1 40 84.9 90.0 95.8 3 50 BOEING B-737-600 143.50 120.50 CFM56-7B22 2 22.70 5.40 1 40 84.4 92.3 95.5 3 BOEING B-737-600 124.00 120.50 CFM56-7B22 2 22.70 5.40 1 40 80.9 92.9 95.5 3 Page 66 ### Page 72 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-737-600 143.50 120.50 CFM56-7B22/2 DAC 2 22.70 5.40 1 40 83.7 91.6 95.8 3 50 BOEING B-737-600 124.00 120.50 CFM56-7B22/2 DAC 2 22.70 5.40 1 40 80.2 92.2 95.8 3 50 BOEING B-737-700 133.00 128.00 CFM56-7B20 2 20.60 5.60 1 40 83.8 90.9 95.8 3 BOEING B-737-700 133.00 128.00 CFM56-7B20/2 DAC 2 20.60 5.60 1 40 83.0 90.3 96.1 3 50 BOEING B-737-700 133.00 128.00 CFM56-7B22 2 22.70 5.40 1 40 82.6 92.5 95.8 3 BOEING B-737-700 133.00 128.00 CFM56-7B22/2 DAC 2 22.70 5.40 1 40 81.8 91.8 96.1 3 50 Page 67 ### Page 73 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-737-700 133.00 128.00 CFM56-7B24 2 24.20 5.30 1 40 82.1 93.6 95.8 3 BOEING B-737-700 133.00 128.00 CFM56-7B24/2 DAC 2 24.20 5.30 1 40 81.1 93.0 96.1 3 50 BOEING B-737-700 133.00 128.00 CFM56-7B26 2 26.30 5.10 1 40 81.4 95.4 95.8 3 BOEING B-737-700 133.00 128.00 CFM56-7B26/2 DAC 2 26.30 5.10 1 40 80.3 94.7 96.1 3 50 BOEING B-737-700 154.50 129.20 CFM56-7B20 2 20.60 5.60 1 40 87.1 89.8 95.9 3 BOEING B-737-700 154.50 129.20 CFM56-7B20/2 DAC 2 20.60 5.60 1 40 86.4 89.2 96.2 3 50 Page 68 ### Page 74 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-737-700 154.50 129.20 CFM56-7B22 2 22.70 5.40 1 40 86.3 91.9 95.9 3 BOEING B-737-700 154.50 129.20 CFM56-7B22/2 DAC 2 22.70 5.40 1 40 85.6 91.2 96.2 3 50 BOEING B-737-700 154.50 129.20 CFM56-7B24 2 24.20 5.30 1 40 85.9 93.0 95.9 3 BOEING B-737-700 154.50 129.20 CFM56-7B24/2 DAC 2 24.20 5.30 1 40 84.7 92.3 96.2 3 50 BOEING B-737-700 154.50 129.20 CFM56-7B26 2 26.30 5.10 1 40 84.6 94.7 95.9 3 BOEING B-737-700 154.50 129.20 CFM56-7B26/2 DAC 2 26.30 5.10 1 40 83.8 94.0 96.2 3 50 Page 69 ### Page 75 MANUFACTURER 04/24/2012 BOEING MODEL B-737-700 IGW/-700C 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **159.00 134.00 CFM56-7B24 2 24.20 5.30 TO AP FLAPS 1 40** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) AC 36-1H APPENDIX 1, CHANGE 1 86.6 92.9 96.1 3 51 BOEING B-737-700 IGW/-700C 171.00 134.00 CFM56-7B24 2 24.20 5.30 1 40 88.6 92.5 96.1 3 51 BOEING B-737-700 IGW/-700C/BBJ 159.00 134.00 CFM56-7B26; -7B26/B1 2 26.30 5.10 1 40 85.2 94.6 96.1 3 51 BOEING B-737-700 IGW/-700C/BBJ 171.00 134.00 CFM56-7B26; -7B26/B1 2 26.30 5.10 1 40 87.1 94.3 96.1 3 51 BOEING B-737-700 IGW/BBJ 159.00 134.00 CFM56-7B27/B3 2 27.30 5.10 1 40 84.8 95.5 96.1 3 51 BOEING B-737-700 IGW/BBJ 171.00 134.00 CFM56-7B27/B3 2 27.30 5.10 1 40 86.6 95.2 96.1 3 51 Page 70 ### Page 76 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-737-800 155.50 144.00 CFM56-7B24 2 24.20 5.30 1 40 85.5 92.5 96.4 3 BOEING B-737-800 155.50 144.00 CFM56-7B24/2 DAC 2 24.20 5.30 1 40 84.7 91.8 96.7 3 50 BOEING B-737-800 155.50 144.00 CFM56-7B26/2 DAC 2 26.30 5.10 1 40 83.7 93.5 96.7 3 50 BOEING B-737-800 155.50 144.00 CFM56-7B27/2 DAC 2 27.30 5.10 1 40 83.2 94.4 96.7 3 50 BOEING B-737-800 155.50 144.00 CFM56-7B27/2B1 DAC 2 27.30 5.10 1 40 83.1 94.7 96.7 3 50 BOEING B-737-800 174.20 146.30 CFM56-7B24 2 24.20 5.30 1 40 88.6 92.1 96.5 3 Page 71 ### Page 77 04/24/2012 MANUFACTURER BOEING MODEL B-737-800 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **174.20 146.30 CFM56-7B24/2 DAC 2 24.20 5.30 TO AP FLAPS 1 40 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 87.8 91.4 96.8 3 50 BOEING B-737-800 174.20 146.30 CFM56-7B26/2 DAC 2 26.30 5.10 1 40 86.7 93.1 96.8 3 50 BOEING B-737-800 174.20 146.30 CFM56-7B27/2 DAC 2 27.30 5.10 1 40 86.1 93.9 96.8 3 50 BOEING B-737-800 174.20 146.30 CFM56-7B27/2B1 DAC 2 27.30 5.10 1 40 85.9 94.3 96.8 3 50 BOEING B-737-800/BBJ 2 155.50 144.00 CFM56-7B26; -7B26/B1 2 26.30 5.10 1 40 84.4 94.2 96.4 3 BOEING B-737-800/BBJ 2 155.50 144.00 CFM56-7B27/B1; -7B27/B2 2 27.30 5.10 1 40 84.0 95.5 96.4 3 Page 72 ### Page 78 04/24/2012 MANUFACTURER BOEING MODEL B-737-800/BBJ 2 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** 155.50 144.00 CFM56-7B27; -7B27/B3 2 27.30 5.10 TO AP FLAPS 1 40 AC 36-1H TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 84.1 95.2 96.4 3 BOEING B-737-800/BBJ 2 174.20 146.30 CFM56-7B26; -7B26/B1 2 26.30 5.10 1 40 87.4 93.8 96.5 3 BOEING B-737-800/BBJ 2 174.20 146.30 CFM56-7B27/B1; -7B27/B2 2 27.30 5.10 1 40 86.8 95.0 96.5 3 BOEING B-737-800/BBJ 2 174.20 146.30 CFM56-7B27; -7B27/B3 2 27.30 5.10 1 40 87.0 94.7 96.5 3 BOEING B-737-800W 155.50 144.00 CFM56-7B24 2 24.20 5.30 1 40 84.5 92.5 96.3 3 52 BOEING B-737-800W 155.50 144.00 CFM56-7B24/2 DAC 2 24.20 5.30 1 40 83.8 91.8 96.5 3 50,52 Page 73 ### Page 79 04/24/2012 MANUFACTURER BOEING MODEL B-737-800W 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **155.50 144.00 CFM56-7B26/2 DAC 2 26.30 5.10 TO AP FLAPS 1 40 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 82.7 93.5 96.5 3 50,52 BOEING B-737-800W 155.50 144.00 CFM56-7B27/2 DAC 2 27.30 5.10 1 40 82.3 94.4 96.5 3 50,52 BOEING B-737-800W 155.50 144.00 CFM56-7B27/2B1 DAC 2 27.30 5.10 1 40 82.2 94.7 96.5 3 50,52 BOEING B-737-800W 174.20 146.30 CFM56-7B24 2 24.20 5.30 1 40 87.5 92.1 96.3 3 52 BOEING B-737-800W 174.20 146.30 CFM56-7B24/2 DAC 2 24.20 5.30 1 40 86.9 91.4 96.6 3 50,52 BOEING B-737-800W 174.20 146.30 CFM56-7B26/2 DAC 2 26.30 5.10 1 40 85.6 93.1 96.6 3 50,52 Page 74 ### Page 80 04/24/2012 MANUFACTURER BOEING MODEL B-737-800W 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **174.20 146.30 CFM56-7B27/2 DAC 2 27.30 5.10 TO AP FLAPS 1 40 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 85.1 93.9 96.6 3 50,52 BOEING B-737-800W 174.20 146.30 CFM56-7B27/2B1 DAC 2 27.30 5.10 1 40 85.0 94.3 96.6 3 50,52 BOEING B-737-800W/BBJ 2 155.50 144.00 CFM56-7B26; -7B26/B1 2 26.30 5.10 1 40 83.5 94.2 96.3 3 52 BOEING B-737-800W/BBJ 2 155.50 144.00 CFM56-7B27/B1; -7B27/B2 2 27.30 5.10 1 40 83.0 95.5 96.3 3 52 BOEING B-737-800W/BBJ 2 155.50 144.00 CFM56-7B27; -7B27/B3 2 27.30 5.10 1 40 83.2 95.1 96.3 3 52 BOEING B-737-800W/BBJ 2 174.20 146.30 CFM56-7B26; -7B26/B1 2 26.30 5.10 1 40 86.4 93.8 96.3 3 52 Page 75 ### Page 81 04/24/2012 MANUFACTURER BOEING MODEL B-737-800W/BBJ 2 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** 174.20 146.30 CFM56-7B27/B1; -7B27/B2 2 27.30 5.10 TO AP FLAPS 1 40 AC 36-1H TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 85.8 95.0 96.3 3 52 BOEING B-737-800W/BBJ 2 174.20 146.30 CFM56-7B27; -7B27/B3 2 27.30 5.10 1 40 86.0 94.7 96.3 3 52 BOEING B-737-900 164.00 146.30 CFM56-7B24 2 24.20 5.30 1 40 86.6 92.0 96.4 3 BOEING B-737-900 164.00 146.30 CFM56-7B26 2 26.30 5.10 1 40 85.5 93.7 96.4 3 BOEING B-737-900 164.00 146.30 CFM56-7B27 2 27.30 5.10 1 40 85.1 94.5 96.4 3 BOEING B-737-900 164.00 146.30 CFM56-7B27/B1 2 27.30 5.10 1 40 85.0 95.0 96.4 3 Page 76 ### Page 82 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-737-900 174.20 147.30 CFM56-7B24 2 24.20 5.30 1 40 88.4 91.8 96.4 3 BOEING B-737-900 174.20 147.30 CFM56-7B26 2 26.30 5.10 1 40 87.2 93.5 96.4 3 BOEING B-737-900 174.20 147.30 CFM56-7B27 2 27.30 5.10 1 40 86.7 94.2 96.4 3 BOEING B-737-900 174.20 147.30 CFM56-7B27/B1 2 27.30 5.10 1 40 86.6 94.7 96.4 3 BOEING B-747-100 710.00 400.00 JT9D-3A 4 43.60 5.10 10 30 105.4 102.1 104.6 3 29 BOEING B-747-100 750.00 400.00 JT9D-7F 4 48.00 5.10 10 30 104.5 103.5 104.5 3 29 Page 77 ### Page 83 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-747-100 734.00 425.00 JT9D-7 4 46.30 5.10 10 30 105.1 102.7 104.6 3 29 BOEING B-747-100 734.00 460.00 JT9D-7A 4 47.00 5.10 10 30 104.3 102.6 105.3 3 29 BOEING B-747-100 750.00 520.00 JT9D-7F 4 48.00 5.10 10 25 104.5 103.5 104.5 3 29 BOEING B-747-100 710.00 540.00 JT9D-3A 4 43.60 5.10 10 25 105.4 102.1 104.6 3 29 BOEING B-747-100 734.00 540.00 JT9D-7 4 46.30 5.10 10 25 105.1 102.7 104.1 3 29 BOEING B-747-100 710.00 564.00 JT9D-3A 4 43.60 5.10 10 30 108.4 99.7 107.2 2 * ** Page 78 ### Page 84 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-747-100 734.00 564.00 JT9D-3A 4 43.60 5.10 10 30 109.4 99.6 107.2 2 * ** BOEING B-747-100 710.00 564.00 JT9D-7 4 46.30 5.10 10 30 108.0 100.2 107.4 2 * ** BOEING B-747-100 750.00 585.00 JT9D-7A 4 47.00 5.10 10 30 107.8 98.8 106.9 2 * ** BOEING B-747-100 750.00 585.00 JT9D-7F 4 48.00 5.10 10 30 107.7 99.0 107.4 2 * ** BOEING B-747-100 750.00 585.00 JT9D-7FW 4 50.00 5.10 10 30 107.6 99.4 107.4 2 * ** BOEING B-747-100 750.00 585.00 JT9D-7WET 4 47.90 5.10 10 30 107.4 99.3 106.9 2 * ** Page 79 ### Page 85 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-747-100 750.00 585.00 RB211-524C2 4 51.60 4.50 10 30 104.5 96.9 106.5 2 * ** BOEING B-747-100 734.00 630.00 JT9D-7A 4 47.00 5.10 10 25 104.3 102.6 105.5 3 29 BOEING B-747-200 770.00 475.00 JT9D-7J 4 50.00 5.10 10 30 103.6 103.0 105.9 3 30 BOEING B-747-200 710.00 520.00 JT9D-3A 4 43.60 5.10 10 30 104.4 100.8 106.9 3 30 BOEING B-747-200 750.00 520.00 JT9D-7F 4 48.00 5.10 10 30 103.5 102.0 106.9 3 30 BOEING B-747-200 734.00 540.00 JT9D-7 4 46.30 5.10 10 30 104.2 101.3 106.7 3 30 Page 80 ### Page 86 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-747-200 767.00 564.00 JT9D-3A 4 43.60 5.10 10 30 110.0 98.2 106.5 2 * ** BOEING B-747-200 770.00 564.00 JT9D-7 4 46.30 5.10 10 30 108.9 98.8 106.7 2 * ** BOEING B-747-200 734.00 564.00 JT9D-7A 4 47.00 5.10 10 30 103.5 101.2 106.9 3 30 BOEING B-747-200 775.00 564.00 JT9D-7F 4 48.00 5.10 10 30 108.6 98.9 107.2 2 * ** BOEING B-747-200 785.00 564.00 JT9D-7R4G2 4 54.75 4.80 10 30 100.1 98.6 105.4 2 ** BOEING B-747-200 775.00 585.00 CF6-50E 4 52.50 4.10 10 30 100.7 101.1 105.9 3 Page 81 ### Page 87 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-747-200 773.00 585.00 JT9D-3AWET 4 45.80 5.10 10 30 109.1 98.7 106.7 2 * ** BOEING B-747-200 833.00 585.00 RB211-524C2 4 51.60 4.50 10 30 106.5 99.7 107.0 3 * BOEING B-747-200 833.00 600.00 JT9D-7Q 4 53.00 4.90 10 30 103.2 103.5 106.6 3 BOEING B-747-200 820.00 630.00 CF6-50E 4 52.50 4.10 10 30 102.5 100.9 107.0 3 BOEING B-747-200 833.00 630.00 CF6-50E2 4 52.50 4.10 10 30 102.6 101.7 106.5 3 BOEING B-747-200 820.00 630.00 CF6-50E2 4 52.50 4.10 10 30 102.1 101.7 106.5 3 Page 82 ### Page 88 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-747-200 710.00 630.00 JT9D-3A 4 43.60 5.10 10 25 104.4 100.8 105.7 3 30 BOEING B-747-200 734.00 630.00 JT9D-7 4 46.30 5.10 10 25 104.2 101.3 105.2 3 30 BOEING B-747-200 820.00 630.00 JT9D-70A 4 53.00 4.90 10 30 101.1 98.5 106.0 3 BOEING B-747-200 785.00 630.00 JT9D-7A 4 47.00 5.10 10 30 109.3 98.7 107.3 2 * ** BOEING B-747-200 734.00 630.00 JT9D-7A 4 47.00 5.10 10 25 103.5 101.2 105.0 3 30 BOEING B-747-200 750.00 630.00 JT9D-7F 4 48.00 5.10 10 25 103.5 102.0 106.0 3 30 Page 83 ### Page 89 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-747-200 800.00 630.00 JT9D-7F 4 48.00 5.10 10 30 109.7 98.8 107.8 2 * ** BOEING B-747-200 805.00 630.00 JT9D-7FW 4 50.00 5.10 10 30 109.4 99.2 107.8 2 * ** BOEING B-747-200 812.00 630.00 JT9D-7FW/-7J 4 50.00 5.10 10 30 109.7 99.2 107.4 2 * ** BOEING B-747-200 770.00 630.00 JT9D-7J 4 50.00 5.10 10 25 103.6 103.0 106.0 3 30 BOEING B-747-200 800.00 630.00 JT9D-7J 4 50.00 5.10 10 30 109.3 99.2 107.8 2 * ** BOEING B-747-200 833.00 630.00 JT9D-7Q 4 53.00 4.90 10 25 103.2 103.5 104.4 3 Page 84 ### Page 90 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-747-200 833.00 630.00 JT9D-7R4G2 4 54.75 4.80 10 30 102.4 97.9 106.6 2 ** BOEING B-747-200 785.00 630.00 JT9D-7WET 4 47.90 5.10 10 30 108.7 99.1 107.3 2 * ** BOEING B-747-200 800.00 630.00 RB211-524B/B2 4 50.10 4.30 10 30 105.5 96.0 107.3 2 * ** BOEING B-747-200 820.00 630.00 RB211-524B/B2 4 50.10 4.30 10 30 105.5 95.6 107.3 2 ** BOEING B-747-200 833.00 630.00 RB211-524D4 4 53.10 4.20 10 30 103.9 99.7 104.9 3 BOEING B-747-300 600.00 564.00 CF6-80C2B1 4 56.70 5.00 10 30 89.8 99.1 102.5 3 Page 85 ### Page 91 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-747-300 775.00 564.00 RB211-524D4 4 53.10 4.20 10 30 101.5 97.1 104.3 2 ** BOEING B-747-300 800.00 585.00 JT9D-70A 4 53.00 4.90 10 30 99.2 95.8 105.4 2 ** BOEING B-747-300 775.00 585.00 RB211-524B2 4 50.10 4.30 10 30 103.3 96.1 106.5 2 ** BOEING B-747-300 800.00 630.00 CF6-50E2 4 52.50 4.10 10 30 101.6 101.8 106.5 3 BOEING B-747-300 820.00 630.00 JT9D-70A 4 53.00 4.90 10 30 100.2 95.5 105.3 2 ** BOEING B-747-300 833.00 630.00 JT9D-7R4G2 4 54.75 4.80 10 30 102.4 101.3 106.6 3 Page 86 ### Page 92 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-747-300 785.00 630.00 JT9D-7R4G2 4 54.75 4.80 10 30 100.1 101.5 106.6 3 BOEING B-747-300 820.00 630.00 RB211-524B2 4 50.10 4.30 10 30 105.5 95.6 107.3 2 ** BOEING B-747-300 833.00 630.00 RB211-524D4 4 53.10 4.20 10 30 103.9 96.5 104.9 2 ** BOEING B-747-300 833.00 666.00 CF6-80C2B1 4 56.70 5.00 10 30 99.0 98.2 105.2 3 BOEING B-747-400 600.00 564.00 CF6-80C2B1F 4 57.90 5.00 10 30 89.6 99.1 101.7 3 BOEING B-747-400 830.00 564.00 CF6-80C2B5F 4 60.80 5.00 10 30 96.0 100.4 101.7 3 Page 87 ### Page 93 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-747-400 600.00 564.00 PW4056 4 56.75 4.80 10 30 89.5 100.7 103.1 3 BOEING B-747-400 600.00 564.00 RB211-524G 4 58.00 4.30 10 30 89.1 98.9 102.4 3 BOEING B-747-400 600.00 564.00 RB211-524H 4 60.60 4.10 10 30 88.7 99.7 102.4 3 BOEING B-747-400 870.00 652.00 CF6-80C2B1F 4 60.20 5.20 25 99.7 98.3 101.4 3 BOEING B-747-400 875.00 652.00 CF6-80C2B1F 4 57.90 5.00 10 30 99.8 98.2 103.8 3 BOEING B-747-400 875.00 652.00 CF6-80C2B1F W/N1 MOD 4 57.30 5.00 10 30 99.9 97.9 103.8 3 Page 88 ### Page 94 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-747-400 875.00 652.00 CF6-80C2B5F 4 60.80 5.00 10 30 97.5 100.3 103.8 3 BOEING B-747-400 870.00 652.00 PW 4056 4 56.75 4.80 10 30 101.5 99.7 104.7 3 BOEING B-747-400 875.00 652.00 PW4056 4 56.75 4.80 10 30 101.6 99.7 104.7 3 BOEING B-747-400 875.00 652.00 PW4056 PH3 (FB2B) 4 56.80 4.80 10 30 99.7 98.6 103.6 3 BOEING B-747-400 875.00 652.00 PW4056 PH3 (FB2C) 4 56.80 4.80 10 30 98.6 98.4 103.0 3 BOEING B-747-400 875.00 652.00 PW4056 PH3 (FB2C) NR 4 56.80 4.80 10 30 97.4 98.1 102.1 3 Page 89 ### Page 95 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-747-400 875.00 652.00 PW4056 PKG B/PHASE I 4 56.80 4.80 10 30 99.3 98.5 103.4 3 BOEING B-747-400 875.00 652.00 RB211-524G 4 58.00 4.30 10 30 99.2 98.0 103.8 3 BOEING B-747-400 870.00 652.00 RB211-524H 4 60.60 4.10 10 30 97.8 98.8 103.8 3 BOEING B-747-400 875.00 652.00 RB211-524H2 4 58.00 4.10 10 30 98.0 98.8 103.8 3 BOEING B747-8 700.00 600.00 Genx-2B(EIS) 4 0.00 0.00 0 30 85.3 94.8 99.6 4 BOEING B747-8 987.00 688.00 Genx-2B(EIS) 4 0.00 0.00 0 30 94.5 94.0 100.4 4 Page 90 ### Page 96 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B747-8F 700.00 600.00 Genx-2B(EIS) 4 0.00 0.00 0 30 85.3 94.8 99.6 4 BOEING B747-8F 975.00 761.00 Genx-2B(EIS) 4 0.00 0.00 0 30 94.0 94.0 100.9 4 BOEING B-747-SP 702.00 410.00 RB211-524D4 4 53.10 4.20 10 30 99.2 99.8 107.0 3 BOEING B-747-SP 660.00 450.00 JT9D-7A 4 47.00 5.10 10 30 99.6 101.3 102.5 3 BOEING B-747-SP 702.00 450.00 JT9D-7J 4 50.00 5.10 10 30 100.1 103.3 103.2 3 BOEING B-747-SP 696.00 450.00 RB211-524B2 4 50.10 4.30 10 30 99.5 99.8 103.2 3 Page 91 ### Page 97 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-747-SP 701.00 465.00 JT9D-7A 4 47.00 5.10 10 30 102.0 101.1 102.9 3 BOEING B-747-SP 660.00 475.00 JT9D-7F 4 48.00 5.10 10 30 98.7 102.3 103.8 3 BOEING B-747-SP 702.00 475.00 JT9D-7J 4 50.00 5.10 10 30 100.1 103.3 103.8 3 BOEING B-747-SP 696.00 475.00 JT9D-7J 4 50.00 5.10 10 30 99.8 103.5 103.8 3 BOEING B-747-SR 571.00 564.00 CF6-45A2 4 46.50 4.10 10 30 98.4 93.2 105.4 3 BOEING B-747-SR 570.00 564.00 JT9D-7A 4 47.00 5.10 10 30 100.2 101.8 106.9 2 * Page 92 ### Page 98 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-747-SR 610.00 564.00 JT9D-7A 4 47.00 5.10 10 30 101.8 101.6 106.9 3 * BOEING B-757-200 187.00 198.00 PW 2037 2 37.00 5 30 81.5 94.3 97.7 3 BOEING B-757-200 220.00 198.00 PW 2037 2 38.20 5.80 5 30 86.2 94.0 97.7 3 BOEING B-757-200 187.00 198.00 PW 2037QFC 2 37.00 5 30 80.1 93.7 97.0 3 59 BOEING B-757-200 220.00 198.00 PW 2040 2 41.70 5.70 5 30 84.6 94.5 97.7 3 BOEING B-757-200 190.00 198.00 PW 2040QFC 2 40.00 5 30 79.4 95.1 97.0 3 59 Page 93 ### Page 99 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-757-200 220.00 198.00 RB211-535C 2 37.40 4.50 5 30 85.5 94.0 100.3 3 BOEING B-757-200 220.00 198.00 RB211-535-E4 2 40.10 4.10 5 30 82.2 93.3 95.0 3 BOEING B-757-200 220.00 198.00 RB211-535-E4 2 40.10 4.10 5 30 82.9 93.4 95.0 3 58 BOEING B-757-200 220.00 198.00 RB211-535E4-B 2 43.10 4.10 5 30 82.1 94.2 95.0 3 58 BOEING B-757-200 220.00 198.00 RB211-535E4-B 2 43.10 4.10 5 30 81.3 94.4 95.0 3 BOEING B-757-200 255.50 210.00 PW 2037 2 38.20 5.80 5 30 91.4 93.7 98.1 3 Page 94 ### Page 100 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-757-200 255.50 210.00 PW 2037QFC 2 37.00 5 30 89.7 92.7 97.3 3 59 BOEING B-757-200 255.50 210.00 PW 2040 2 41.70 5.70 5 30 89.7 94.2 98.1 3 BOEING B-757-200 255.50 210.00 PW 2040QFC 2 40.00 5 30 88.1 94.0 97.3 3 59 BOEING B-757-200 240.00 210.00 RB211-535C 2 37.40 4.50 5 25 88.1 93.8 99.6 3 BOEING B-757-200 255.50 210.00 RB211-535-E4 2 40.10 4.10 5 30 86.8 93.0 95.2 3 BOEING B-757-200 255.50 210.00 RB211-535-E4 2 40.10 4.10 5 30 87.3 93.0 95.2 3 58 Page 95 ### Page 101 04/24/2012 MANUFACTURER BOEING MODEL B-757-200 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **255.50 210.00 RB211-535E4-B 2 43.10 4.10 TO AP FLAPS 5 30 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 85.7 94.1 95.2 3 BOEING B-757-200 255.50 210.00 RB211-535E4-B 2 43.10 4.10 5 30 86.2 93.8 95.2 3 58 BOEING B757-200 (STC ST02200LA) 220.00 198.42 RB211-535E4 2 0.00 0.00 5 30 83.9 96.0 98.1 4 BOEING B757-200 (STC ST02200LA) 255.50 210.00 RB211-535E4 2 0.00 0.00 5 30 89.3 95.5 98.4 4 BOEING B-757-300 236.00 210.00 RB211-535-E4 2 40.10 4.10 5 30 84.8 93.9 95.2 3 58 BOEING B-757-300 235.87 210.00 RB211-535E4-B 2 43.10 4.10 5 30 84.0 95.2 95.2 3 58 Page 96 ### Page 102 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-757-300 235.87 210.00 RB211-535E4-C 2 43.00 5 30 84.0 95.2 95.2 3 58 BOEING B-757-300 275.00 224.00 RB211-535-E4 2 40.10 4.10 5 30 89.8 93.5 95.4 3 58 BOEING B-757-300 275.00 224.00 RB211-535E4-B 2 43.10 4.10 5 30 88.4 94.8 95.4 3 58 BOEING B-757-300 275.00 224.00 RB211-535E4-C 2 43.00 5 30 88.4 94.8 95.4 3 58 BOEING B-767-200 279.90 257.00 CF6-80A 2 48.00 4.60 1 30 84.9 95.5 101.4 3 BOEING B-767-200 279.90 257.00 CF6-80A2 2 50.00 4.60 1 30 84.2 97.2 101.4 3 Page 97 ### Page 103 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-767-200 282.00 257.00 JT9D-7R4D(A) 2 48.00 5.00 1 30 87.7 95.7 101.8 3 BOEING B-767-200 282.00 257.00 JT9D-7R4D(B) 2 48.00 5.00 1 30 88.4 95.9 101.9 3 BOEING B-767-200 282.00 257.00 JT9D-7R4E 2 50.00 5.00 1 30 87.5 96.8 101.9 3 BOEING B-767-200 300.00 270.00 CF6-80C2-B2 2 52.50 5.00 1 30 85.2 94.1 95.7 3 BOEING B-767-200 351.00 270.00 CF6-80C2-B4 2 57.90 5.00 1 30 87.7 95.3 95.7 3 BOEING B-767-200 335.00 270.00 PW4052 2 52.00 4.80 1 30 89.4 95.0 97.8 3 Page 98 ### Page 104 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-767-200 340.00 270.00 PW4056 2 56.75 4.80 1 30 88.5 96.0 97.8 3 BOEING B-767-200 351.00 285.00 PW4052 2 52.00 4.80 1 30 90.9 94.9 98.2 3 BOEING B-767-200 360.00 300.00 CF6-80A 2 48.00 4.60 1 30 92.8 94.8 101.7 3 BOEING B-767-200 360.00 300.00 CF6-80A2 2 50.00 4.60 1 30 91.7 96.5 101.7 3 BOEING B-767-200 351.00 300.00 CF6-80C2-B2 2 52.50 5.00 1 30 89.5 93.7 96.4 3 BOEING B-767-200 387.00 300.00 CF6-80C2-B4 2 57.90 5.00 1 30 90.6 95.0 96.4 3 Page 99 ### Page 105 MANUFACTURER 04/24/2012 BOEING MODEL B-767-200 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **351.00 300.00 JT9D-7R4D(A) 2 48.00 5.00 TO AP FLAPS 1 30** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) AC 36-1H APPENDIX 1, CHANGE 1 95.1 95.2 102.7 3 BOEING B-767-200 360.00 300.00 JT9D-7R4D(B) 2 48.00 5.00 1 30 96.2 95.3 102.6 3 BOEING B-767-200 360.00 300.00 JT9D-7R4E 2 50.00 5.00 1 30 95.4 96.2 102.6 3 BOEING B-767-200 400.00 300.00 PW 4056 2 56.75 4.80 1 30 93.7 95.5 98.6 3 BOEING B-767-200/200ER 300.00 270.00 CF6-80C2B2F 2 52.50 5.00 1 30 85.1 93.8 95.8 3 BOEING B-767-200/200ER 300.00 270.00 CF6-80C2B4F 2 57.90 5.00 1 30 83.7 95.2 95.8 3 Page 100 ### Page 106 04/24/2012 MANUFACTURER BOEING MODEL B-767-200/200ER 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **299.60 270.00 PW4056 PH3 (FB2C) NRI 2 56.80 4.80 TO AP FLAPS 1 30 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 81.8 95.1 95.9 3 BOEING B-767-200/200ER 340.00 270.00 PW4060 2 60.00 4.80 1 30 87.7 97.3 97.8 3 BOEING B-767-200/200ER 299.60 270.00 PW4060 PH3 (FB2C) NRI 2 60.00 4.80 1 30 81.6 96.4 95.9 3 BOEING B-767-200/200ER 360.00 300.00 CF6-80C2B2F 2 52.50 5.00 1 30 90.2 93.4 96.5 3 BOEING B-767-200/200ER 360.00 300.00 CF6-80C2B4F 2 57.90 5.00 1 30 88.5 94.8 96.5 3 BOEING B-767-200/200ER 387.00 300.00 CF6-80C2B4F W/N1 MOD 2 57.90 5.00 1 30 90.6 94.6 96.5 3 Page 101 ### Page 107 04/24/2012 MANUFACTURER BOEING MODEL B-767-200/200ER 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **400.00 300.00 CF6-80C2B6F W/N1 MOD 2 61.50 5.00 TO AP FLAPS 1 30 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 90.5 95.5 96.5 3 BOEING B-767-200/200ER 395.00 300.00 PW4056 PH3 (FB2C) NRI 2 56.80 4.80 1 30 89.8 94.5 96.6 3 BOEING B-767-200/200ER 387.00 300.00 PW4060 2 60.00 4.80 1 30 91.6 96.9 98.6 3 BOEING B-767-200/200ER 395.00 300.00 PW4060 PH3 (FB2C) NRI 2 60.00 4.80 1 30 89.0 95.9 96.6 3 BOEING B-767-300 300.00 280.00 CF6-80A 2 48.00 4.60 5 30 87.5 95.2 101.7 3 BOEING B-767-300 300.00 280.00 CF6-80A2 2 50.00 4.60 5 30 86.7 96.9 101.7 3 Page 102 ### Page 108 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-767-300 288.70 280.00 CF6-80C2B2 2 52.50 5.00 5 30 83.1 94.3 96.5 3 BOEING B-767-300 380.00 280.00 CF6-80C2-B4 2 57.90 5.00 5 30 90.2 95.3 96.5 3 BOEING B-767-300 380.00 280.00 CF6-80C2-B6 2 61.50 5.00 5 30 89.2 96.4 96.5 3 BOEING B-767-300 380.00 280.00 CF6-80C2B6F 2 61.50 5.00 5 30 89.1 96.1 96.6 3 BOEING B-767-300 300.00 280.00 JT9D-7R4D(B) 2 48.00 5.00 5 30 91.0 95.7 102.3 3 BOEING B-767-300 300.00 280.00 JT9D-7R4E 2 50.00 5.00 5 30 90.0 96.5 102.3 3 Page 103 ### Page 109 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-767-300 380.00 280.00 PW 4056 2 56.75 4.80 5 30 92.0 96.0 98.8 3 BOEING B-767-300 380.00 280.00 PW4060 2 60.00 4.80 5 30 91.2 97.2 98.8 3 BOEING B-767-300 340.00 280.00 RB211-524G 2 58.00 4.30 5 30 89.4 94.3 98.5 3 BOEING B-767-300 340.00 280.00 RB211-524H 2 60.60 4.10 5 30 88.7 95.2 98.5 3 BOEING B-767-300 351.00 320.00 CF6-80A 2 48.00 4.60 5 30 92.0 94.9 101.7 3 BOEING B-767-300 351.00 320.00 CF6-80A2 2 50.00 4.60 5 30 91.2 96.5 101.7 3 Page 104 ### Page 110 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-767-300 407.00 320.00 CF6-80C2-B4 2 57.90 5.00 5 30 92.1 95.2 98.4 3 BOEING B-767-300 407.00 320.00 CF6-80C2-B6 2 61.50 5.00 5 30 91.1 96.3 98.4 3 BOEING B-767-300 407.00 320.00 CF6-80C2B6F 2 61.50 5.00 5 30 90.9 96.0 98.5 3 BOEING B-767-300 351.00 320.00 JT9D-7R4D(B) 2 48.00 5.00 5 30 95.7 95.4 103.0 3 BOEING B-767-300 351.00 320.00 JT9D-7R4E 2 50.00 5.00 5 30 95.0 96.2 103.0 3 BOEING B-767-300 407.00 320.00 PW 4056 2 56.75 4.80 5 30 94.2 95.7 100.2 3 Page 105 ### Page 111 04/24/2012 MANUFACTURER BOEING MODEL B-767-300 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **407.00 320.00 PW 4060 2 60.00 4.80 TO AP FLAPS 5 30 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 93.2 97.0 100.2 3 BOEING B-767-300 407.00 320.00 RB211-524G 2 58.00 4.30 5 30 93.8 94.0 99.8 3 BOEING B-767-300 407.00 320.00 RB211-524H 2 60.60 4.10 5 30 92.9 94.8 99.8 3 BOEING B-767-300/300ER 295.00 280.00 PW4056 PH3 (FB2C) NRI 2 56.80 4.80 5 30 81.9 95.3 96.6 3 BOEING B-767-300/300ER 295.00 280.00 PW4060 PH3 (FB2C) NRI 2 60.00 4.80 5 30 81.5 96.6 96.6 3 BOEING B-767-300/300ER 345.00 280.00 PW4062 PH3 (FB2C) NRI 2 62.00 4.80 5 30 84.6 98.0 96.6 3 Page 106 ### Page 112 04/24/2012 MANUFACTURER BOEING MODEL B-767-300/300ER 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **412.00 320.00 PW4056 PH3 (FB2C) NRI 2 56.80 4.80 TO AP FLAPS 5 30 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 91.0 94.6 97.6 3 BOEING B-767-300/300ER 412.00 320.00 PW4060 PH3 (FB2C) NRI 2 60.00 4.80 5 30 90.3 95.9 97.9 3 BOEING B-767-300/300ER 412.00 320.00 PW4062 (FB2B) 2 62.00 4.80 5 30 92.2 99.0 100.2 3 BOEING B-767-300/300ER 412.00 320.00 PW4062 PH3 (FB2C) NRI 2 62.00 4.80 5 30 89.9 97.6 97.9 3 BOEING B-767-400 350.00 320.00 CF6-80C2B8F 2 63.50 5.00 5 30 85.5 97.8 97.6 3 BOEING B-767-400 450.00 350.00 CF6-80C2B8F 2 63.50 5.00 5 30 91.2 96.8 98.7 3 Page 107 ### Page 113 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-777-200 440.90 440.90 PW4074 2 74.00 6.80 5 30 85.2 95.5 98.9 3 BOEING B-777-200 506.00 445.00 GE90-76B 2 76.00 8.40 5 30 86.7 93.3 97.6 3 53 BOEING B-777-200 506.00 445.00 GE90-76B (BLK IV) 2 76.00 8.40 5 30 87.6 94.3 97.9 3 54 BOEING B-777-200 506.00 445.00 GE90-77B 2 77.00 8.30 5 30 86.7 93.4 97.6 3 53 BOEING B-777-200 506.00 445.00 GE90-77B (BLK IV) 2 77.00 8.30 5 30 87.4 94.3 97.9 3 54 BOEING B-777-200 545.00 445.00 GE90-85B 2 85.00 8.30 5 30 87.3 94.4 97.6 3 53 Page 108 ### Page 114 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-777-200 545.00 445.00 GE90-85B (BLK IV) 2 85.00 8.30 5 30 87.8 95.3 97.9 3 54 BOEING B-777-200 545.00 445.00 GE90-90B 2 90.00 8.20 5 30 86.3 95.4 97.6 3 53 BOEING B-777-200 545.00 445.00 GE90-90B (BLK IV) 2 90.00 8.20 5 30 86.5 96.1 97.9 3 54 BOEING B-777-200 580.00 445.00 GE90-94B (BLK IV) 2 94.00 8.10 5 30 87.5 96.7 97.9 3 54 BOEING B-777-200 535.00 445.00 PW4074 2 74.00 6.80 5 30 90.9 95.1 99.0 3 BOEING B-777-200 445.00 445.00 PW4077 2 77.00 6.60 5 30 84.9 96.2 98.9 3 Page 109 ### Page 115 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-777-200 545.00 445.00 PW4090 2 90.00 6.10 5 30 88.3 98.7 98.9 3 55 BOEING B-777-200 535.00 445.00 PW4090 at PW4074 rating 2 74.00 6.80 5 30 90.8 95.2 98.9 3 55 BOEING B-777-200 447.40 445.00 PW4090 at PW4074 rating 2 74.00 6.80 5 30 85.7 95.5 98.9 3 55 BOEING B-777-200 447.50 445.00 PW4090 at PW4077 rating 2 77.00 6.60 5 30 85.1 96.3 98.9 3 55 BOEING B-777-200 545.00 445.00 PW4090 at PW4077 rating 2 77.00 6.60 5 30 90.6 95.9 98.9 3 55 BOEING B-777-200 458.00 445.00 RR TRENT 875 2 75.00 6.30 5 30 87.1 96.1 99.2 3 Page 110 ### Page 116 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-777-200 458.00 445.00 RR TRENT 877 2 77.00 6.20 5 30 86.7 96.5 99.2 3 BOEING B-777-200 545.00 445.00 RR TRENT 884 2 84.00 6.00 5 30 89.4 97.2 99.2 3 BOEING B-777-200 545.00 445.00 RR TRENT 892 2 90.00 5.90 5 30 88.3 98.1 99.2 3 BOEING B-777-200 632.50 445.00 RR TRENT 895 2 93.40 5.80 5 30 92.4 98.4 99.2 3 BOEING B-777-200 545.00 460.00 GE90-76B 2 76.00 8.40 5 30 88.8 93.2 97.8 3 53 BOEING B-777-200 545.00 460.00 GE90-76B (BLK IV) 2 76.00 8.40 5 30 89.5 94.1 98.1 3 54 Page 111 ### Page 117 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-777-200 545.00 460.00 GE90-77B 2 77.00 8.30 5 30 88.8 93.3 97.8 3 53 BOEING B-777-200 545.00 460.00 GE90-77B (BLK IV) 2 77.00 8.30 5 30 89.4 94.2 98.1 3 54 BOEING B-777-200 632.50 460.00 GE90-85B 2 85.00 8.30 5 30 91.3 94.2 97.8 3 53 BOEING B-777-200 656.00 460.00 GE90-90B 2 90.00 8.20 5 30 91.3 95.0 97.8 3 53 BOEING B-777-200 545.00 460.00 PW4077 2 77.00 6.60 5 30 90.7 95.8 99.0 3 BOEING B-777-200 632.50 470.00 GE90-85B (BLK IV) 2 85.00 8.30 5 30 92.0 95.0 98.3 3 54 Page 112 ### Page 118 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-777-200 656.00 470.00 GE90-90B (BLK IV) 2 90.00 8.20 5 30 91.5 95.7 98.3 3 54 BOEING B-777-200 656.00 470.00 GE90-94B BLK IV) 2 94.00 8.10 5 30 91.1 96.4 98.3 3 54 BOEING B-777-200 656.00 470.00 PW4090 2 90.00 6.10 5 30 93.9 98.2 99.2 3 55 BOEING B-777-200 545.00 470.00 RR TRENT 875 2 75.00 6.30 5 30 92.0 95.8 99.5 3 BOEING B-777-200 555.00 470.00 RR TRENT 877 2 77.00 6.20 5 30 91.7 96.1 99.5 3 BOEING B-777-200 632.50 470.00 RR TRENT 884 2 84.00 6.00 5 30 94.3 96.9 99.5 3 Page 113 ### Page 119 04/24/2012 MANUFACTURER BOEING MODEL B-777-200 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **656.00 470.00 RR TRENT 892 2 90.00 5.90 TO AP FLAPS 5 30 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 94.0 97.7 99.5 3 BOEING B-777-200 656.00 470.00 RR TRENT 895 2 93.40 5.80 5 30 93.4 98.3 99.5 3 BOEING B777-200LR 632.50 487.00 GE90-110B1 2 0.00 0.00 0 30 87.0 98.6 99.7 3 BOEING B777-200LR 632.50 487.00 GE90-115B 2 0.00 0.00 0 30 86.5 100.1 99.7 3 BOEING B777-200LR 766.80 575.00 GE90-110B1 2 0.00 0.00 0 30 92.6 97.8 100.3 3 BOEING B777-200LR 766.80 575.00 GE90-115B 2 0.00 0.00 0 30 91.9 99.2 100.3 3 Page 114 ### Page 120 04/24/2012 MANUFACTURER BOEING MODEL B777-200LR/F 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **632.50 487.00 GE90-110B1 2 110.00 7.30 TO AP FLAPS 5 30 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 87.0 98.7 99.7 4 BOEING B777-200LR/F 632.50 487.00 GE90-115B 2 115.00 7.10 5 30 86.5 100.1 99.7 4 BOEING B777-200LR/F 766.80 575.00 GE90-110B1 2 110.00 7.30 5 30 92.7 97.9 100.3 4 BOEING B777-200LR/F 766.80 575.00 GE90-115B 2 115.00 7.10 5 30 92.0 99.2 100.3 4 BOEING B-777-300 450.00 445.00 PW4090 2 90.00 6.10 5 30 83.4 98.7 99.0 3 55 BOEING B-777-300 550.00 445.00 PW4098 2 98.00 5.80 5 30 87.7 99.3 100.0 3 Page 115 ### Page 121 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-777-300 550.00 445.00 RR TRENT 884 2 84.00 6.00 5 30 90.1 96.6 99.2 3 BOEING B-777-300 550.00 445.00 RR TRENT 892 2 90.00 5.90 5 30 88.4 97.5 99.2 3 BOEING B-777-300 660.00 524.00 PW4090 2 90.00 6.10 5 30 94.4 97.3 99.9 3 55 BOEING B-777-300 660.00 524.00 PW4098 2 98.00 5.80 5 30 93.1 98.5 101.1 3 BOEING B-777-300 660.00 524.00 RR TRENT 884 2 84.00 6.00 5 30 96.2 95.9 100.4 3 BOEING B-777-300 660.00 524.00 RR TRENT 892 2 90.00 5.90 5 30 94.2 96.9 100.4 3 Page 116 ### Page 122 04/24/2012 MANUFACTURER BOEING MODEL B777-300ER 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **515.80 515.80 GE90-115B (EIS) 2 115.00 7.10 TO AP FLAPS 5 30 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 83.1 100.5 100.2 4 BOEING B777-300ER 775.00 554.00 GE90-115B (EIS) 2 115.00 7.10 5 30 92.8 98.7 100.5 4 BOEING B787-8 392.40 345.00 Genx-1B BLK4@64K 4 0.00 0.00 0 30 82.6 90.6 99.5 4 BOEING B787-8 392.00 345.00 Genx-1B BLK4@70K 4 0.00 0.00 0 30 81.6 91.9 99.5 4 BOEING B787-8 440.00 345.00 RR TRENT 1000-A 2 32.06 0.00 0 30 84.0 90.1 96.8 4 BOEING B787-8 502.50 380.00 Genx-1B BLK4@64K 4 0.00 0.00 0 30 89.0 90.1 99.6 4 Page 117 ### Page 123 MANUFACTURER 04/24/2012 BOEING MODEL B787-8 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** 502.50 380.00 Genx-1B BLK4@70K 4 0.00 0.00 TO AP FLAPS 0 30 TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) AC 36-1H APPENDIX 1, CHANGE 1 87.4 91.5 99.6 4 BOEING B787-8 502.50 380.00 RR TRENT 1000-A 2 0.00 0.00 0 30 89.1 89.6 96.9 4 BOMBARDIER BD-100-1A10 (CHALLENGER 300) 38.50 33.75 AS907-1-1A 2 6.92 4.20 10 30 75.3 87.6 89.6 3 BOMBARDIER BD-700-1A10 93.50 78.60 BR710 2 14.75 5.00 6 30 86.7 88.7 89.8 3 * BOMBARDIER BD-700-1A10 98.00 78.60 BR710 2 14.75 5.00 6 30 83.4 88.4 89.8 3 BOMBARDIER BD-700-1A10 96.00 78.60 BR710 2 14.75 5.00 6 30 82.7 88.6 89.8 3 Page 118 ### Page 124 **MANUFACTURER 04/24/2012** BOMBARDIER MODEL BD-700-1A10 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **95.00 78.60 BR710 2 14.75 5.00 TO AP FLAPS 6 30** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) AC 36-1H APPENDIX 1, CHANGE 1 82.4 88.6 89.8 3 BOMBARDIER BD-700-1A10 93.50 78.60 BR710 2 14.75 5.00 6 30 82.1 88.7 89.8 3 BOMBARDIER BD-700-1A10 (Global Express) 96.00 78.50 BR700-710-A2-20 2 14.97 5.00 16 30 82.7 88.6 89.8 3 BOMBARDIER BD-700-1A10 (Global Express) 93.50 78.50 BR700-710-A2-20 2 14.97 5.00 16 30 82.1 88.7 89.8 3 BOMBARDIER BD700-1A10 (Global Express) (Learjet STC: SA8184NM-D) 75.00 75.00 Rolls Royce/ BR700-710-A2- 20 2 14.97 5.00 16 30 75.6 89.3 89.7 3 BOMBARDIER CL-600 36.00 33.00 ALF-502 2 7.50 5.00 20 45 81.6 89.3 91.2 3 * Page 119 ### Page 125 **MANUFACTURER 04/24/2012** BOMBARDIER MODEL CL-600 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **40.40 36.00 ALF 502L/L-2/L-2C 2 7.50 5.00 TO AP FLAPS 20 45** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) AC 36-1H APPENDIX 1, CHANGE 1 84.0 87.2 91.6 3 * BOMBARDIER CL-600 41.25 36.00 ALF-502L/L-2/L-2C 2 7.50 5.00 20 45 84.7 89.5 91.6 3 * BOMBARDIER CL-600 (WINGLETS) 41.25 36.00 ALF-502L/L-2/L-2C 2 7.50 5.00 20 45 84.8 89.5 91.6 3 BOMBARDIER CL-600-2B19 (CRJ) 53.00 47.00 CF-34-3A1 2 9.22 6.00 20 45 79.8 82.2 92.1 3 BOMBARDIER CL-600-2B19 (CRJ) 53.00 47.00 CF-34-3B1 2 9.22 20 45 78.7 82.4 92.1 3 BOMBARDIER CL-600-2C10 (CRJ700) 75.00 66.90 CF34-8C1 2 13.79 6.30 8 45 82.7 89.4 92.6 3 Page 120 ### Page 126 04/24/2012 **MANUFACTURER** BOMBARDIER MODEL CL-600-2C10 (CRJ700) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **72.50 66.90 CF34-8C1 2 13.79 6.30 TO AP FLAPS 8 45 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 82.1 89.5 92.6 3 BOMBARDIER CL-600-2C10 (CRJ-700) 75.00 67.00 CF34-8C1 2 13.79 6.30 8 45 82.7 89.4 92.6 3 BOMBARDIER CL-600-2C10 (CRJ-700) 72.74 67.00 CF34-8C1 2 13.79 6.30 10 45 83.2 89.6 92.5 3 BOMBARDIER CL-600-2D24 (CRJ-900) 80.47 73.50 CF34-8C5 & CF34-8C5A1 2 14.51 4.90 8 45 83.4 89.2 93.2 3 BOMBARDIER CL-600-2D24 (CRJ-900) 84.50 73.50 CF34-8C5 & CF34-8C5A1 2 14.51 4.90 8 45 84.6 89.1 93.2 3 BOMBARDIER CL-600-2D24 (CRJ-900) 84.50 73.50 CF34-8C5A1 (Normal 2 14.51 4.90 8 45 84.5 89.4 93.2 3 Takeoff + 2% (NTO+2%)) Page 121 ### Page 127 04/24/2012 **MANUFACTURER** BOMBARDIER MODEL CL-600-2D24 (CRJ-900) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** 80.47 73.50 CF34-8C5A1 (Normal Takeoff + 2% (NTO+2%)) 2 14.51 4.90 TO AP FLAPS 8 45 AC 36-1H TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 83.3 89.5 93.2 3 BOMBARDIER CL-600-2E25 (CRJ-1000) 91.80 81.50 CF-34-8C5A2 2 0.00 0.00 9 40 85.5 93.3 89.1 4 BOMBARDIER CL-600-2E25 (CRJ-1000) 85.97 81.50 CF-34-8C5A2 2 0.00 0.00 9 40 83.3 93.3 89.2 4 BOMBARDIER CL-601 43.00 36.00 CF34-1A 2 8.65 6.30 20 45 79.9 84.8 89.4 3 * BOMBARDIER CL-601 42.10 36.00 CF34-1A 2 8.65 6.30 20 45 79.4 84.9 89.4 3 * BOMBARDIER CL-601-1A 45.10 36.00 CF-34-1A 2 8.65 6.30 20 45 80.5 84.6 90.1 3 * Page 122 ### Page 128 04/24/2012 **MANUFACTURER** BOMBARDIER MODEL CL-601-3A 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **43.10 36.00 CF-34-3A 2 8.72 6.30 TO AP FLAPS 20 45 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 79.4 85.9 89.4 3 * BOMBARDIER CL-601-3A 45.10 36.00 CF-34-3A/-3A2 2 8.65 6.30 20 45 79.8 85.7 90.1 3 * BOMBARDIER CL-601-3R 45.10 36.00 CF-34-3A1 2 9.22 6.00 20 45 79.8 85.7 90.1 3 * BOMBARDIER CL-604 47.60 38.00 GE CF34-3B 2 8.72 6.30 20 45 80.9 86.2 90.3 3 * BOMBARDIER CL-604 48.20 38.00 GE CF34-3B 2 8.72 6.30 20 45 81.2 86.2 90.3 3 * CESSNA 500 CITATION 10.30 9.90 JT15D-1 2 2.20 3.30 15 40 76.4 86.1 87.7 3 * Page 123 ### Page 129 04/24/2012 MANUFACTURER CESSNA MODEL 500/501 CITATION I 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **11.80 11.30 JT15D-1/-1A 2 2.20 3.30 TO AP FLAPS 15 40 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 78.0 86.2 87.9 3 * CESSNA 525 CESSNA JET 10.40 9.70 FJ44-1A 2 1.50 15 35 73.4 83.7 92.1 3 CESSNA 525A CITATION JET II (CJ-2) 12.37 11.50 FJ44-2C 2 2.10 15 35 74.5 88.8 91.4 3 CESSNA 525B 13.87 12.75 FJ44-3A 2 2.82 0.00 15 35 74.0 88.8 88.6 3 CESSNA 550 CITATION II 13.30 12.70 JT15D-4 2 2.50 2.68 15 40 80.1 86.7 90.5 3 * CESSNA 550 CITATION Bravo 14.80 13.50 PW530A 2 2.20 15 40 73.7 85.2 91.2 3 Page 124 ### Page 130 04/24/2012 MANUFACTURER CESSNA MODEL 550 CITATION II 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **14.10 13.50 JT15D-4 2 2.50 2.68 TO AP FLAPS 0 40 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 71.6 86.4 90.5 3 CESSNA 551 CITATION II 12.50 12.00 JT15D-4 2 2.50 2.68 15 40 80.1 86.7 90.5 3 * CESSNA 552 15.50 14.30 JT15D-5 2 2.90 2.10 20 35 89.3 94.7 88.5 3 * CESSNA 560 CITATION Ultra 16.30 15.20 JT15D-5D 2 2.30 7 35 82.9 95.9 85.7 3 CESSNA 560 CITATION V 15.90 15.20 JT15D-5A 2 2.90 2.10 7 35 83.7 94.7 88.9 3 CESSNA 560 CITATION V 16.30 15.20 JT15D-5A 2 2.90 2.10 7 35 84.6 94.6 88.9 3 Page 125 ### Page 131 04/24/2012 MANUFACTURER CESSNA MODEL 560 ENCORE 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **16.63 15.20 PW535A 2 2.90 TO AP FLAPS 7 35 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 70.3 89.9 90.5 3 CESSNA 560XL EXCEL 20.00 18.70 PW545A 2 3.00 7 35 72.4 85.3 93.1 3 CESSNA 650 CITATION III 21.00 17.00 TFE731-3B-100S 2 2.90 3.11 20 37 84.9 92.5 92.4 3 CESSNA 650 CITATION III 22.00 20.00 TFE731-3B-100S 2 2.90 3.11 7 37 80.1 92.4 93.8 3 22 CESSNA 650 CITATION VI 22.45 20.00 TFE731-3C-100S 2 2.90 7 40 82.2 92.4 93.8 3 CESSNA 650 CITATION VII 23.00 20.00 TFE731-4R-3S 2 3.20 7 40 78.9 91.9 90.8 3 Page 126 ### Page 132 04/24/2012 MANUFACTURER CESSNA MODEL 750 CITATION X 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **35.70 31.80 AE3007C 2 5.00 5.30 TO AP FLAPS 15 35 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 72.3 83.0 90.2 3 CESSNA S550 CITATION S/II 14.70 14.00 JT15D-4B 2 2.50 2.68 20 35 87.9 91.6 85.1 3 * CESSNA S550 CITATION S/II 15.10 14.40 JT15D-4B 2 2.50 2.68 7 35 80.0 91.3 86.2 3 DASSAULT FALCON 10 19.30 17.64 TFE731-2-1C 2 3.23 2.80 15 52 82.2 86.2 95.2 3 DASSAULT FALCON 200 32.00 27.60 ATF3-6A-4C 2 5.20 2.90 5 40 83.9 89.0 93.9 3 DASSAULT FALCON 200 (M5634) 32.00 28.88 ATF3-6A-4C 2 5.20 2.90 5 40 83.9 89.0 94.2 3 Page 127 ### Page 133 **MANUFACTURER 04/24/2012** DASSAULT MODEL FALCON 2000 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **36.50 33.00 CFE738-1-1B 2 5.72 6.00 TO AP FLAPS 20 40** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) AC 36-1H APPENDIX 1, CHANGE 1 79.4 86.4 93.1 3 DASSAULT FALCON 20-Basic/D/E 28.66 27.32 CF700-2D-2 2 4.50 2.00 15 40 90.0 92.3 101.7 2 DASSAULT FALCON 20-Basic/D/E/F (M2851) 28.66 27.32 CF700-2D-2Q 2 4.50 2.00 0 40 81.9 94.0 99.7 3 DASSAULT FALCON 20-C5/D5/E5 (M3500) 29.10 27.73 TFE731-5AR-2C 2 4.50 3.70 15 40 82.9 88.4 90.7 3 DASSAULT FALCON 20-C5/D5/E5 (M3530) 29.10 27.73 TFE-731-5BR-2C 2 4.80 3.70 15 40 80.3 90.7 90.7 3 DASSAULT FALCON 20-C5/D5/E5 (M3547) 30.50 28.88 TFE731-5BR-2C 2 4.80 3.70 15 40 82.9 91.9 90.6 3 Page 128 ### Page 134 **MANUFACTURER 04/24/2012** DASSAULT MODEL FALCON 20-F (M1400) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **28.66 27.32 CF700-2D-2 2 4.50 2.00 TO AP FLAPS 10 40** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) AC 36-1H APPENDIX 1, CHANGE 1 90.0 92.3 103.0 2 DASSAULT FALCON 20-F5 (M3500) 29.10 27.73 TFE731-5AR-2C 2 4.50 3.70 10 40 81.8 88.6 90.0 3 DASSAULT FALCON 20-F5 (M3530) 29.10 27.73 TFE-731-5BR-2C 2 4.80 3.70 10 40 79.3 90.9 90.0 3 DASSAULT FALCON 20-F5 (M3547) 30.50 28.88 TFE731-5BR-2C 2 4.80 3.70 10 40 81.9 92.1 90.3 3 DASSAULT FALCON 20-G (M2500) 32.00 27.56 ATF3-6-2C 2 5.40 2.90 10 40 87.5 88.3 95.9 3 DASSAULT FALCON 50 38.80 35.72 TFE731-3-1C 3 3.70 2.80 20 48 84.3 91.6 97.4 3 Page 129 ### Page 135 **MANUFACTURER 04/24/2012** DASSAULT MODEL FALCON 50 ( M1810) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **40.79 35.72 TFE731-40-1 3 3.70 3.50 TO AP FLAPS 20 48** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) AC 36-1H APPENDIX 1, CHANGE 1 83.0 92.7 95.2 3 DASSAULT FALCON 50 (M1230) 40.78 35.71 TFE731-3-1C 3 3.70 2.80 20 48 84.8 91.5 97.1 3 DASSAULT FALCON 50 (M2193) 40.79 35.72 TFE731-40-1 3 3.70 3.50 20 48 83.8 92.0 95.2 3 DASSAULT FALCON 7X 69.00 62.40 PW307A 3 6.40 4.10 20 40 83.7 90.3 92.6 4 DASSAULT FALCON 7X (Take-off configuration SFI) 69.00 62.40 PW307A 3 6.40 4.10 9 40 81.9 90.1 92.6 4 DASSAULT FALCON 7X (Take-off configuration SFI) 70.00 62.40 PW307A 3 6.40 4.10 9 40 82.3 90.1 92.6 4 Page 130 ### Page 136 04/24/2012 **MANUFACTURER** DASSAULT MODEL FALCON 900 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **45.50 42.00 TFE731-5AR-1C 3 4.75 3.70 TO AP FLAPS 20 40 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 81.9 89.5 91.7 3 DASSAULT FALCON 900 (M1196) 46.50 42.00 TFE731-5AR-1C 3 4.75 3.70 20 40 82.9 89.5 91.7 3 DASSAULT FALCON 900B (M1200) 46.50 42.00 TFE731-5BR-1C 3 4.75 3.70 20 40 80.7 91.2 91.7 3 DASSAULT FALCON 900EX (M3000) 49.00 44.50 TFE731-60-1 3 5.00 4.40 20 40 79.8 90.5 92.3 3 ECLIPSE EA500 5.76 5.42 PW610F-A 2 15 32 67.8 79.1 81.8 4 ECLIPSE EA500 6.00 5.60 PW610F-A 2 15 32 69.2 78.9 81.9 4 Page 131 ### Page 137 04/24/2012 **MANUFACTURER** EMBRAER MODEL EMB-135LR 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **44.09 40.78 AE3007A1/3 2 7.20 4.77 TO AP FLAPS 9 45 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 77.9 84.4 92.3 3 EMBRAER EMB-145EP 46.29 41.22 AE3007A 2 7.58 5.23 9 45 83.7 84.2 92.6 3 * EMBRAER EMB-145ER 45.41 41.22 AE3007A 2 7.58 5.23 9 45 77.9 84.6 92.6 3 EMBRAER EMB-145LR 48.50 42.54 AE3007A1/1 2 7.58 4.76 9 45 79.4 84.6 92.5 3 EMBRAER ERJ-190-100 IGW 114.20 97.00 CF34-10E5 2 18.82 5.00 1 6 86.9 91.9 92.8 3 EMBRAER ERJ-190-100 IGW 114.20 97.00 CF34-10E5A1 2 18.82 5.00 1 6 86.1 93.1 92.8 3 Page 132 ### Page 138 04/24/2012 **MANUFACTURER** EMBRAER MODEL ERJ-190-100 IGW 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **114.20 97.00 CF34-10E6 2 18.82 5.00 TO AP FLAPS 1 6 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 86.9 91.9 92.8 3 EMBRAER ERJ-190-100 IGW 114.20 97.00 CF34-10E6A1 2 18.82 5.00 1 6 86.1 96.1 92.8 3 EMBRAER ERJ-190-100 LR 110.89 94.80 CF34-10E5 2 18.82 5.00 1 6 86.1 91.9 92.7 3 EMBRAER ERJ-190-100 LR 110.89 94.80 CF34-10E5A1 2 18.82 5.00 1 6 85.1 93.1 92.7 3 EMBRAER ERJ-190-100 LR 110.89 94.80 CF34-10E6 2 18.82 5.00 1 6 86.0 92.0 92.7 3 EMBRAER ERJ-190-100 LR 110.89 94.80 CF34-10E6A1 2 18.82 5.00 1 6 85.1 93.1 92.7 3 Page 133 ### Page 139 04/24/2012 **MANUFACTURER** EMBRAER MODEL ERJ-190-100 STD 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **105.36 94.80 CF34-10E5 2 18.82 5.00 TO AP FLAPS 1 6 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 84.7 92.1 92.7 3 EMBRAER ERJ-190-100 STD 105.36 94.80 CF34-10E5A1 2 18.82 5.00 1 6 83.7 93.3 92.7 3 EMBRAER ERJ-190-100 STD 105.36 94.80 CF34-10E6 2 18.82 5.00 1 6 84.7 92.1 92.7 3 EMBRAER ERJ-190-100 STD 105.36 94.80 CF34-10E6A1 2 18.82 5.00 1 6 83.7 93.3 92.7 3 FAIRCHILD DORNIER DORNIER 328-300 33.51 31.06 PW306B 2 6.05 5.60 12 32 76.1 89.8 91.1 3 FAIRCHILD DORNIER DORNIER 328-300 Mod 10 34.52 31.72 PW306B 2 6.05 5.60 12 32 76.5 89.8 92.1 3 Page 134 ### Page 140 04/24/2012 MANUFACTURER FOKKER MODEL F100 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **98.00 88.00 TAY MK650-15 2 14.73 3.00 TO AP FLAPS 0 42 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 81.8 91.7 93.0 3 FOKKER F28 MK1000 65.00 59.00 SPEY MK555-15 2 9.39 1.00 6 42 90.0 99.5 101.2 2 FOKKER F28 MK2000 65.00 SPEY MK555-15 2 9.39 1.00 6 42 90.0 99.5 101.8 2 * FOKKER F28 MK3000 71.00 64.00 SPEY MK555-15H 2 9.77 1.00 6 42 91.0 99.3 99.4 2 FOKKER F28 MK4000 73.00 65.80 SPEY MK555-15H 2 9.77 1.00 6 42 91.9 99.2 99.4 2 FOKKER F28 MK4000 73.00 69.50 SPEY MK555-15P 2 9.85 1.00 6 42 92.9 101.7 101.4 2 Page 135 ### Page 141 04/24/2012 MANUFACTURER FOKKER MODEL F70 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **81.00 75.00 TAY MK620-15 2 13.80 3.00 TO AP FLAPS 0 42 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 76.8 89.9 87.7 3 FOKKER F70 92.00 81.00 TAY MK620-15 2 13.80 3.00 0 42 80.1 89.5 88.3 3 GULFSTREAM G100 24.65 20.70 TFE731-40R-200G 2 4.25 2.90 25 40 79.1 89.5 91.9 3 GULFSTREAM G-1159 (GII) (STAGE III TECH. L.C.; STC ST01567LA) 62.00 58.50 SPEY RB 511-8 2 11.40 0.64 20 39 82.6 95.7 96.5 3 12 GULFSTREAM G-1159 (GII) (STAGE III TECH. L.C.; STC ST01567LA) 64.80 58.50 SPEY RB 511-8 2 11.40 0.64 20 39 83.6 95.6 96.5 3 12 GULFSTREAM G-1159 (GIIB) (STAGE III TECH. L.C.; STC ST01567LA) 68.20 58.50 SPEY RB 511-8 2 11.40 0.64 10 39 84.1 95.5 96.8 3 12 Page 136 ### Page 142 **APPENDIX 1, CHANGE 1** **MANUFACTURER** GULFSTREAM MODEL G-1159 (GIIB) (STAGE III TECH. L.C.; STC ST01567LA) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **69.70 58.50 SPEY RB 511-8 2 11.40 0.64 TO AP FLAPS 10 39** TO SL AP NOISE LEVEL (EPNdB) **84.6 95.5 96.8 STAGE 3 NOTES 12 GULFSTREAM G-1159 (GIII) (STAGE III TECH.** L.C.; STC ST01567LA) 69.70 58.50 SPEY RB 511-8 2 11.40 0.64 10 39 84.6 95.5 96.8 3 12 GULFSTREAM G-1159 (GIII) (STAGE III TECH. L.C.; STC ST01567LA) 68.20 58.50 SPEY RB 511-8 2 11.40 0.64 10 39 84.1 95.5 96.8 3 12 GULFSTREAM G-1159 (REALLY QUIET LLC; **STC SE01291LA)** 62.00 58.50 SPEY 511-8 2 11.40 0.64 10 39 84.1 95.7 97.8 3 12 GULFSTREAM G-1159 (REALLY QUIET LLC; **STC SE01291LA)** 64.80 58.50 SPEY 511-8 2 11.40 0.64 10 39 85.5 95.7 97.8 3 12 GULFSTREAM G200 34.85 28.00 PW306A 2 6.04 4.50 25 40 81.4 85.8 90.9 3 47 Page 137 ### Page 143 **MANUFACTURER 04/24/2012** GULFSTREAM MODEL G200 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **34.85 28.00 PW306A 2 6.04 4.50 TO AP FLAPS 25 40** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) AC 36-1H APPENDIX 1, CHANGE 1 81.4 85.8 92.7 3 46 GULFSTREAM GII (QUIET TECH. AERO.; STC ST02618AT) 61.20 58.50 SPEY 511-8 (RB 163-25) 2 11.40 0.64 10 39 84.3 95.7 97.5 3 12 GULFSTREAM G-II GULFSTREAM 62.00 58.50 SPEY 511-8 2 11.40 0.64 20 39 90.9 102.7 98.2 2 12 GULFSTREAM G-II GULFSTREAM 65.50 58.50 SPEY 511-8 2 11.40 0.64 10 39 92.5 103.0 98.3 2 12 GULFSTREAM G-IIB/G-III 69.70 58.50 SPEY 511-8 2 11.40 0.64 10 39 91.1 103.4 97.3 2 12 GULFSTREAM G-IIB/G-III (HAT STC; ST01567LA) 68.20 58.50 SPEY 511-8 (RB 163-25) 2 10 39 84.1 95.5 96.8 3 12 Page 138 ### Page 144 **MANUFACTURER 04/24/2012** GULFSTREAM MODEL G-IIB/G-III (HAT STC; ST01567LA) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **69.70 58.50 SPEY 511-8 (RB 163-25) 2 TO AP FLAPS 10 39** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) AC 36-1H APPENDIX 1, CHANGE 1 **84.6 95.5 96.8 3 12 GULFSTREAM GIIB/GIII (QUIET TECH.** AERO.; STC ST02618AT) 69.70 58.50 SPEY 511-8 (RB 163-25) 2 11.40 0.64 10 39 87.0 95.9 97.7 3 12 GULFSTREAM GIISP (HAT STC; ST01567LA) 64.80 58.50 SPEY 511-8 (RB 163-25) 2 20 39 83.6 95.6 96.5 3 12 GULFSTREAM GIISP (HAT STC; ST01567LA) 62.00 58.50 SPEY 511-8 (RB 163-25) 2 20 39 82.6 95.7 96.5 3 12 GULFSTREAM G-IV 73.20 58.50 TAY 611-8 2 13.85 3.00 10 39 76.8 87.3 91.0 3 GULFSTREAM G-IV GULFSTREAM w/ASC 190 74.60 66.00 TAY 611-8 2 13.85 3.00 20 39 77.5 86.6 92.0 3 Page 139 ### Page 145 **MANUFACTURER 04/24/2012** GULFSTREAM MODEL G-V 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **90.50 75.30 BR700-710A1-10 2 14.70 4.20 TO AP FLAPS 10 39** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) AC 36-1H APPENDIX 1, CHANGE 1 80.3 89.1 90.8 3 ISRAEL AIRCRAFT 1124 WESTWIND 22.90 19.00 TFE731-3-1G 2 3.70 2.80 20 40 81.2 88.4 93.0 3 ISRAEL AIRCRAFT 1124A WESTWIND 2 23.50 19.00 TFE731-3-1G 2 3.70 2.80 20 40 85.4 88.7 92.8 3 * ISRAEL AIRCRAFT 1125 ASTRA 23.50 20.70 TFE731-3A-200G 2 12 40 82.3 89.8 89.8 3 ISRAEL AIRCRAFT 1125 ASTRA 24.70 20.70 TFE731-3A-200G 2 12 40 84.1 89.7 89.8 3 ISRAEL AIRCRAFT 1125 ASTRA SPX 24.65 20.70 TFE731-40R 2 0 40 79.9 89.9 92.3 3 Page 140 ### Page 146 04/24/2012 **MANUFACTURER** ISRAEL AIRCRAFT MODEL Galaxy 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **34.85 28.00 PW306A 2 6.04 4.50 TO AP FLAPS 0 40 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 81.4 85.8 92.7 3 LEARJET 23 Raisbeck MK II 12.50 11.90 CJ610-1/-4 2 1.34 0.00 10 88.0 103.8 98.0 2 LEARJET 24 Raisbeck MK II 13.00 11.90 CJ610-1/-4 2 1.34 0.00 10 89.0 103.8 98.0 2 LEARJET 24/24D 13.50 11.90 CJ610-6 2 2.95 0.00 20 40 91.8 99.3 100.7 2 13 LEARJET 24B/D Raisbeck MK II 13.50 11.88 CJ610 2 10 40 87.6 104.0 98.0 2 LEARJET 24D 13.50 11.90 CJ610-6 2 2.95 0.00 20 40 91.8 99.3 101.7 2 14 Page 141 ### Page 147 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES LEARJET 24D 13.50 11.90 CJ610-6 2 2.95 0.00 20 40 91.9 104.0 96.7 2 LEARJET 24E 12.90 11.90 CJ610-6 2 2.95 0.00 8 40 84.3 103.9 95.3 2 LEARJET 24F 13.50 11.90 CJ610-6 2 2.95 0.00 8 40 85.8 103.7 95.3 2 LEARJET 24F-A 12.50 11.90 CJ610-6 2 2.95 0.00 8 40 83.6 103.9 95.3 2 LEARJET 25 15.00 13.30 CJ610-6 2 2.95 0.00 94.0 99.3 100.8 2 LEARJET 25 16.00 13.30 CJ610-6 2 2.95 0.00 10 40 93.5 103.9 99.0 2 Page 142 ### Page 148 04/24/2012 **MANUFACTURER** LEARJET MODEL 25/25B/C Raisb MK II 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **15.00 13.30 CJ610 2 TO AP FLAPS 10 40 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 91.0 103.8 99.0 2 LEARJET 25B/C/D/F XR Dee Hwd 16.30 13.30 CJ610-6/8A 2.95 0.00 10 40 93.5 103.9 99.0 2 LEARJET 25C 15.00 13.30 CJ610-6 2 2.95 0.00 20 40 94.0 99.3 100.8 2 13 LEARJET 25D 15.00 13.30 CJ610-6 2 2.95 0.00 20 40 94.0 99.3 102.7 2 14 LEARJET 25D/25F 15.00 13.30 CJ610-6/8A 2 2.95 0.00 8 40 90.1 103.7 95.2 2 LEARJET 28/29 15.00 14.30 CJ610-8A 2 2.95 0.00 8 40 87.0 99.7 101.7 2 Page 143 ### Page 149 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES LEARJET 31 15.50 15.30 TFE731-2-3B 2 3.50 8 40 79.6 87.2 92.6 3 * LEARJET 31 16.50 15.30 TFE731-2-3B 2 3.50 8 40 81.0 87.0 92.6 3 * LEARJET 31A 17.00 15.30 TFE731-2-3B 2 3.50 8 40 81.9 86.9 92.8 3 LEARJET 31A 17.00 16.00 TFE731-2-3B 2 3.50 8 40 82.9 86.8 93.1 3 LEARJET 35/36 17.00 14.30 TFE731-2-2B 2 3.50 2.64 20 40 84.0 86.9 92.2 3 * LEARJET 35/36 18.00 14.30 TFE731-2-2B 2 3.50 2.64 20 40 84.5 87.9 92.2 3 * Page 144 ### Page 150 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES LEARJET 35A 18.00 14.30 TFE731-2-2B 2 3.50 2.64 8 40 83.6 87.4 91.3 3 * LEARJET 35A/36A 18.00 14.30 TFE731-2-2B 2 3.50 2.64 8 40 78.7 87.4 91.3 3 LEARJET 35A/36A 18.30 15.30 TFE731-2-2B 2 3.50 2.64 8 40 79.2 86.7 91.4 3 LEARJET 36A 18.30 15.30 TFE731-2-2B 2 3.50 2.64 20 40 83.9 87.8 91.4 3 * LEARJET 45 20.50 19.20 TFE731-20R-1B or (-20AR- 2 8 40 74.4 85.2 93.4 3 1B) LEARJET 55 21.00 17.00 TFE731-3A-2B 2 3.70 8 40 85.5 90.7 90.6 3 * Page 145 ### Page 151 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES LEARJET 55 19.50 17.00 TFE731-3A-2B 2 3.70 8 40 84.2 90.9 90.6 3 * LEARJET 55B 21.50 18.00 TFE731-3A-2B 2 3.70 20 40 86.3 90.7 91.0 3 * LEARJET 55C 21.50 17.00 TFE731-3AR-3B 2 3.90 2.90 20 40 87.0 91.4 92.4 3 * LEARJET 55C 21.00 17.00 TFE731-3AR-3B 2 3.90 2.90 20 40 86.7 91.5 92.4 3 * LEARJET 55C 21.50 18.00 TFE731-3AR-2B 2 3.90 2.90 20 40 86.7 90.9 92.4 3 * LEARJET 55C 21.00 18.00 TFE731-3AR-2B 2 3.90 2.90 20 40 86.2 91.0 92.4 3 * Page 146 ### Page 152 04/24/2012 **MANUFACTURER** LEARJET MODEL 60 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **23.10 19.50 PW305A 2 4.67 TO AP FLAPS 8 40 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 70.8 83.1 87.7 3 LEARJET 60 23.50 19.50 PW305A 2 4.67 8 40 70.8 83.2 87.7 3 LOCKHEED 1329-23 (AIRESEARCH) 43.80 TFE731-3-1E 4 3.70 2.80 20 59 92.7 88.1 96.9 2 * ** LOCKHEED 1329-23A/D/E (STAR 3 STC ST00258SE) 44.25 36.00 TFE731-3-1R 4 3.70 2.80 20 59 85.2 90.7 96.9 3 LOCKHEED 1329-25 (AIRESEARCH) 44.50 36.00 TFE731-3 4 3.70 2.80 93.1 88.1 96.9 2 * ** LOCKHEED 1329-25 (STAR 3 STC# ST00259SE) 44.50 36.00 TFE731-3-1R 4 3.70 2.80 20 59 85.4 90.7 96.9 3 Page 147 ### Page 153 **MANUFACTURER 04/24/2012** LOCKHEED MODEL L-1011 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **430.00 358.00 RB211-22B 3 41.00 4.70 TO AP FLAPS 14 42** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) AC 36-1H APPENDIX 1, CHANGE 1 95.9 95.1 102.8 3 5 * LOCKHEED L-1011-1 430.00 358.00 RB211-22B 3 41.00 4.70 10 42 96.0 95.0 102.8 3 5 * LOCKHEED L-1011-100 466.00 368.00 RB211-22B 3 41.00 4.70 10 42 98.5 94.9 102.8 3 5 * LOCKHEED L-1011-200 466.00 368.00 RB211-524B 3 50.00 4.50 10 33 98.1 97.9 101.4 3 5 * LOCKHEED L1011-385-1-14/15 474.00 368.00 RB211-22B 3 41.00 4.70 4 42 98.6 94.1 102.8 3 LOCKHEED L1011-385-1-14/15 466.00 368.00 RB211-524B4 3 50.00 4.50 10 42 97.9 95.9 103.3 3 * Page 148 ### Page 154 **MANUFACTURER 04/24/2012** LOCKHEED MODEL L-1011-500 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **496.00 368.00 RB211-524B 3 50.00 4.50 TO AP FLAPS 14 33** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) AC 36-1H APPENDIX 1, CHANGE 1 98.4 97.8 101.5 3 5 * LOCKHEED L-1011-500 504.00 368.00 RB211-524B3 3 50.00 4.50 22 33 98.0 96.9 100.2 3 5 * LOCKHEED L-1011-500 496.00 368.00 RB211-524B3 3 50.00 4.50 14 33 97.4 96.7 100.3 3 5 * LOCKHEED L-1011-500 510.00 368.00 RB211-524B4 3 50.00 4.50 10 33 99.3 96.4 102.0 3 * MCDONNELL DOUGLAS DC-08-51 (BAC STC: SA3915NM) 276.00 199.50 JT3D-1 4 17.00 1.40 15 50 99.5 101.2 107.8 2 6,26,** MCDONNELL DOUGLAS DC-08-51 (BAC STC: SA3915NM) 276.00 199.50 JT3D-1 4 17.00 1.40 15 35 101.2 101.3 103.4 2 6,** Page 149 ### Page 155 **MANUFACTURER 04/24/2012** MCDONNELL DOUGLAS MODEL DC-08-51 (BAC STC: SA3915NM) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **276.00 199.50 JT3D-3B 4 18.00 1.40 TO AP FLAPS 15 35** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) AC 36-1H APPENDIX 1, CHANGE 1 98.6 101.6 103.4 2 6,** MCDONNELL DOUGLAS DC-08-51 (BAC STC: SA3915NM) 286.00 199.50 JT3D-3B 4 18.00 1.40 15 50 98.4 101.5 107.8 2 6,26,** MCDONNELL DOUGLAS DC-08-51 (BAC STC: SA3915NM) 276.00 199.50 JT3D-3B 4 18.00 1.40 15 50 97.0 101.5 107.8 2 6,26,** MCDONNELL DOUGLAS DC-08-51 (QNC PLS QN) 276.00 199.50 JT3D-1 4 35 101.9 99.9 107.1 2 6,** MCDONNELL DOUGLAS DC-08-51 (QNC PLS QN) 276.00 199.50 JT3D-3B 4 18.00 1.40 35 99.5 101.5 107.1 2 6,** MCDONNELL DOUGLAS DC-08-51 (QNC PLS QN) 276.00 199.50 JT3D-3B 4 18.00 1.40 35 99.1 101.5 107.0 2 6,26,** Page 150 ### Page 156 04/24/2012 **MANUFACTURER** MCDONNELL DOUGLAS MODEL DC-08-51 (QNC PLS QN) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **286.00 207.00 JT3D-3B 4 18.00 1.40 TO AP FLAPS 35 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 100.7 101.4 107.1 2 6,26,** MCDONNELL DOUGLAS DC-08-51 (QNC QN) 276.00 199.50 JT3D-3B 4 18.00 1.40 15 25 99.9 103.1 104.5 2 6,** MCDONNELL DOUGLAS DC-08-51 (QNC QN) 276.00 199.50 JT3D-3B 4 18.00 1.40 15 25 99.3 103.1 104.2 2 6,26,** MCDONNELL DOUGLAS DC-08-51 (QNC QN) 286.00 207.00 JT3D-3B 4 18.00 1.40 15 25 101.3 103.0 104.6 2 6,26,** MCDONNELL DOUGLAS DC-08-52 (BAC STC: SA3915NM) 305.00 201.90 JT3D-3B 4 18.00 1.40 15 50 100.9 101.4 108.0 2 6,26,** MCDONNELL DOUGLAS DC-08-52 (QNC PLS QN) 300.00 202.00 JT3D-3B 4 18.00 1.40 35 102.9 101.3 107.0 2 6,26,** Page 151 ### Page 157 04/24/2012 **MANUFACTURER** MCDONNELL DOUGLAS MODEL DC-08-52 (QNC PLS QN) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **300.00 202.00 JT3D-3B 4 18.00 1.40 TO AP FLAPS 35 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 103.2 101.3 107.2 2 6,** MCDONNELL DOUGLAS DC-08-52 (QNC QN) 300.00 202.00 JT3D-3B 4 18.00 1.40 15 25 103.7 102.9 104.3 2 6,26,** MCDONNELL DOUGLAS DC-08-52 (QNC QN) 300.00 202.00 JT3D-3B 4 18.00 1.40 15 25 104.2 102.9 104.7 2 6,** MCDONNELL DOUGLAS DC-08-53 (BAC STC: SA3915NM) 315.00 203.30 JT3D-3B 4 18.00 1.40 15 50 102.3 101.3 108.1 2 6,26,** MCDONNELL DOUGLAS DC-08-53 (QNC PLS QN) 318.00 207.00 JT3D-3B 4 18.00 1.40 35 105.3 101.1 107.1 2 6,26,** MCDONNELL DOUGLAS DC-08-53 (QNC QN) 306.80 207.00 JT3D 4 15 25 105.2 102.8 105.0 2 6,** Page 152 ### Page 158 04/24/2012 **MANUFACTURER** MCDONNELL DOUGLAS MODEL DC-08-53 (QNC QN) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **315.00 207.00 JT3D-3B 4 18.00 1.40 TO AP FLAPS 35 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 104.9 101.2 107.1 2 6,** MCDONNELL DOUGLAS DC-08-53 (QNC QN) 309.80 207.00 JT3D-3B 4 18.00 1.40 15 25 105.2 102.8 104.6 2 6,26,** MCDONNELL DOUGLAS DC-08-55 (BAC STC: SA3915NM) 325.00 217.00 JT3D-3B 4 18.00 1.40 15 35 103.7 101.2 105.1 2 6,26,** MCDONNELL DOUGLAS DC-08-55 (BAC STC: SA3915NM) 325.00 240.00 JT3D-3B 4 18.00 1.40 15 35 103.7 101.2 107.9 2 6,26,** MCDONNELL DOUGLAS DC-08-55 (QNC PLS QN) 320.30 217.00 JT3D-3B 4 18.00 1.40 35 105.5 101.1 107.2 2 6,26,** MCDONNELL DOUGLAS DC-08-55 (QNC QN) 309.80 217.00 JT3D-3B 4 18.00 1.40 15 25 105.2 102.8 105.2 2 6,26,** Page 153 ### Page 159 04/24/2012 **MANUFACTURER** MCDONNELL DOUGLAS MODEL DC-08-55/F54 (BAC STC: SA3915NM) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **313.70 217.00 JT3D-3B 4 18.00 1.40 TO AP FLAPS 15 35 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 105.3 101.5 104.0 2 6,26,** MCDONNELL DOUGLAS DC-08-61 (BAC II STC: SA4892NM) 325.00 240.00 JT3D-3B 4 18.00 1.40 15 35 99.8 101.0 101.6 3 12 MCDONNELL DOUGLAS DC-08-61 (BAC STC: SA3915NM) 325.00 240.00 JT3D-3B 4 18.00 1.40 15 35 103.7 101.2 107.9 2 6,26,** MCDONNELL DOUGLAS DC-08-61 (QNC PLS QN) 270.00 240.00 JT3D-3B 4 18.00 1.40 35 98.6 101.5 107.2 2 6,26,** MCDONNELL DOUGLAS DC-08-61 (QNC PLS QN) 320.30 240.00 JT3D-3B 4 18.00 1.40 35 105.5 101.1 107.2 2 6,** MCDONNELL DOUGLAS DC-08-61 (QNC QN) 309.80 240.00 JT3D-3B 4 18.00 1.40 15 25 105.2 102.8 106.5 2 6,26,** Page 154 ### Page 160 04/24/2012 **MANUFACTURER** MCDONNELL DOUGLAS MODEL DC-08-61 (QNC QN) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **270.00 240.00 JT3D-3B 4 18.00 1.40 TO AP FLAPS 15 25 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 98.1 103.1 106.5 2 6,26,** MCDONNELL DOUGLAS DC-08-61F (QNC QN) 309.80 248.00 JT3D-3B 4 18.00 1.40 15 25 105.2 102.8 106.9 2 6,26,** MCDONNELL DOUGLAS DC-08-62 (ADC QN) 335.00 240.00 JT3D-3B 4 18.00 1.40 12 50 102.5 98.2 108.3 2 6,** MCDONNELL DOUGLAS DC-08-62 (ADC QN) 335.00 240.00 JT3D-7 4 19.00 1.40 12 50 101.6 98.8 108.3 2 6,** MCDONNELL DOUGLAS DC-08-62 (ADC QN) 350.00 250.00 JT3D-3B 4 18.00 1.40 12 50 104.3 98.1 108.3 2 6,** MCDONNELL DOUGLAS DC-08-62 (ADC QN) 350.00 250.00 JT3D-7 4 19.00 1.40 12 50 103.4 98.5 108.3 2 6,** Page 155 ### Page 161 **APPENDIX 1, CHANGE 1** **MANUFACTURER** MCDONNELL DOUGLAS MODEL DC-08-62 (BAC II STC: SA4892NM or SA5455NM) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **335.00 250.00 JT3D-7 4 19.00 1.40 TO AP FLAPS 12 35** TO SL AP NOISE LEVEL (EPNdB) 97.8 101.3 102.2 STAGE 3 NOTES 12 MCDONNELL DOUGLAS DC-08-62 (BAC II STC: SA4892NM) 348.00 240.00 JT3D-3B 4 18.00 1.40 12 35 100.5 101.2 100.7 3 12 MCDONNELL DOUGLAS DC-08-62 (BAC II STC: SA4892NM) 350.00 240.00 JT3D-7 4 19.00 1.40 12 35 98.6 101.6 102.0 3 12 MCDONNELL DOUGLAS DC-08-62 (BAC II STC: SA4892NM) 335.00 250.00 JT3D-3B 4 18.00 1.40 12 35 99.7 101.3 101.0 3 12 MCDONNELL DOUGLAS DC-08-62 (BAC II STC: SA5455NM) 350.00 240.00 JT3D-3B 4 18.00 1.40 12 35 100.5 101.2 100.2 3 12 MCDONNELL DOUGLAS DC-08-62 (TNC QN) 335.00 240.00 JT3D-3B 4 18.00 1.40 12 50 102.0 99.3 107.8 2 6,** Page 156 ### Page 162 04/24/2012 **MANUFACTURER** MCDONNELL DOUGLAS MODEL DC-08-62 (TNC QN) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **350.00 250.00 JT3D-3B 4 18.00 1.40 TO AP FLAPS 12 50 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 103.9 98.9 107.9 2 6,** MCDONNELL DOUGLAS DC-08-62 (TNC QN) 335.00 250.00 JT3D-7 4 19.00 1.40 12 35 101.6 101.7 106.4 2 6,** MCDONNELL DOUGLAS DC-08-62 (TNC QN) 355.00 275.00 JT3D-7 4 19.00 1.40 12 35 102.7 100.7 107.6 2 6,** MCDONNELL DOUGLAS DC-08-63 (ADC QN) 355.00 245.00 JT3D-3B 4 18.00 1.40 12 50 104.8 98.1 108.3 2 6,** MCDONNELL DOUGLAS DC-08-63 (ADC QN) 355.00 245.00 JT3D-7 4 19.00 1.40 12 50 104.1 98.4 108.3 2 6,** MCDONNELL DOUGLAS DC-08-63 (ADC QN) 355.00 275.00 JT3D-3B 4 18.00 1.40 12 50 104.8 98.1 108.5 2 6,** Page 157 ### Page 163 **MANUFACTURER 04/24/2012** MCDONNELL DOUGLAS MODEL DC-08-63 (ADC QN) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **355.00 275.00 JT3D-7 4 19.00 1.40 TO AP FLAPS 12 50** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) AC 36-1H APPENDIX 1, CHANGE 1 104.1 98.4 108.4 2 6,** MCDONNELL DOUGLAS DC-08-63 (BAC II STC: SA4892NM or SA5455NM) 353.00 258.00 JT3D-7 4 19.00 1.40 12 35 98.9 101.4 102.4 3 12 MCDONNELL DOUGLAS DC-08-63 (BAC II STC: SA4892NM or SA5455NM) 353.00 267.00 JT3D-7 4 19.00 1.40 12 35 98.9 101.4 102.7 3 12 MCDONNELL DOUGLAS DC-08-63 (BAC II STC: SA4892NM) 353.00 275.00 JT3D-7 4 19.00 1.40 12 50 98.9 99.0 107.6 2 6,26,** MCDONNELL DOUGLAS DC-08-63 (TNC QN) 335.00 240.00 JT3D-3B 4 18.00 1.40 12 50 101.7 99.1 107.8 2 6,** MCDONNELL DOUGLAS DC-08-63 (TNC QN) 350.00 250.00 JT3D-3B 4 18.00 1.40 12 50 103.9 98.9 107.9 2 6,** Page 158 ### Page 164 **MANUFACTURER 04/24/2012** MCDONNELL DOUGLAS MODEL DC-08-63 (TNC QN) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **335.00 250.00 JT3D-7 4 19.00 1.40 TO AP FLAPS 12 35** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) AC 36-1H APPENDIX 1, CHANGE 1 100.7 101.0 106.5 2 6,** MCDONNELL DOUGLAS DC-08-63 (TNC QN) 355.00 275.00 JT3D-7 4 19.00 1.40 12 35 103.8 101.3 107.3 2 6,** MCDONNELL DOUGLAS DC-08-71 325.00 240.00 CFM56-2-C1 4 22.00 6.00 15 50 94.3 92.9 98.3 3 * MCDONNELL DOUGLAS DC-08-71 325.00 240.00 CFM-56-2C5 4 22.00 6.00 94.3 92.9 98.3 3 * MCDONNELL DOUGLAS DC-08-71 328.00 258.00 CFM56-2-C1 4 22.00 6.00 15 50 94.5 92.9 98.6 3 * MCDONNELL DOUGLAS DC-08-72 335.00 240.00 CFM56-2-C1 4 22.00 6.00 12 50 94.4 92.9 98.1 3 * Page 159 ### Page 165 **MANUFACTURER 04/24/2012** MCDONNELL DOUGLAS MODEL DC-08-72 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **350.00 250.00 CFM56-2-C1 4 22.00 6.00 TO AP FLAPS 12 50** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) AC 36-1H APPENDIX 1, CHANGE 1 95.2 92.8 98.2 3 * MCDONNELL DOUGLAS DC-08-73 355.00 258.00 CFM56-2-C1 4 22.00 6.00 12 50 95.7 92.8 98.3 3 * MCDONNELL DOUGLAS DC-08-73 355.00 275.00 CFM56-2-C1 4 22.00 6.00 12 50 95.7 92.8 98.5 3 * MCDONNELL DOUGLAS DC-08F-54 (BAC STC: SA3915NM) 315.00 217.00 JT3D-3B 4 18.00 1.40 15 35 102.3 101.3 105.1 2 6,26,** MCDONNELL DOUGLAS DC-08F-54 (BAC STC: SA3915NM) 315.00 240.00 JT3D-3B 4 18.00 1.40 15 35 102.3 101.3 107.9 2 6,26,** MCDONNELL DOUGLAS DC-08F-54 (QNC PLS QN) 315.00 217.00 JT3D-3B 4 18.00 1.40 35 105.2 101.1 107.3 2 6,** Page 160 ### Page 166 04/24/2012 **MANUFACTURER** MCDONNELL DOUGLAS MODEL DC-08F-54 (QNC PLS QN) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **315.00 217.00 JT3D-3B 4 18.00 1.40 TO AP FLAPS 35 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 104.9 101.2 107.2 2 6,26,** MCDONNELL DOUGLAS DC-08F-54 (QNC PLS QN) 315.00 240.00 JT3D-3B 4 18.00 1.40 35 104.9 101.2 107.4 2 6,26,** MCDONNELL DOUGLAS DC-08F-54 (QNC QN) 306.80 207.00 JT3D-3B 4 18.00 1.40 15 25 105.2 102.8 105.0 2 6,** MCDONNELL DOUGLAS DC-08F-54 (QNC QN) 309.80 207.00 JT3D-3B 4 18.00 1.40 15 25 105.2 102.8 104.6 2 6,26,** MCDONNELL DOUGLAS DC-08F-54 (QNC QN) 306.80 217.00 JT3D-3B 4 18.00 1.40 15 25 105.2 102.8 105.6 2 6,** MCDONNELL DOUGLAS DC-08F-54 (QNC QN) 309.80 240.00 JT3D-3B 4 18.00 1.40 15 25 105.2 102.8 106.5 2 6,26,** Page 161 ### Page 167 04/24/2012 **MANUFACTURER** MCDONNELL DOUGLAS MODEL DC-08F-54/55 (BAC STC: SA3915NM) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **313.70 240.00 JT3D-3B 4 18.00 1.40 TO AP FLAPS 15 35 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 105.3 101.5 106.3 2 6,26,** MCDONNELL DOUGLAS DC-08F-55 (QNC PLS QN) 317.80 240.00 JT3D-3B 4 18.00 1.40 35 105.2 101.1 107.4 2 6,26,** MCDONNELL DOUGLAS DC-08F-55 (QNC QN) 309.80 240.00 JT3D-3B 4 18.00 1.40 15 25 105.2 102.8 106.5 2 6,26,** MCDONNELL DOUGLAS DC-09-10 90.70 81.70 JT8D-7 2 14.00 1.40 10 50 91.4 100.8 103.1 2 24 MCDONNELL DOUGLAS DC-09-10 90.70 81.70 JT8D-7/-7A 2 14.00 1.40 10 50 91.4 101.4 100.4 2 1 MCDONNELL DOUGLAS DC-09-10 (ABS) 90.70 81.70 JT8D-7/7A/7B 2 14.00 1.40 10 40 87.2 96.4 95.0 3 6 Page 162 ### Page 168 04/24/2012 **MANUFACTURER** MCDONNELL DOUGLAS MODEL DC-09-10 (AIRWELD STC ST00934LA) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **108.00 99.00 JT8D-9A 2 14.50 1.03 TO AP FLAPS 0 40 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 90.6 96.7 95.6 3 12 MCDONNELL DOUGLAS DC-09-20 (ABS;STC SA1613GL) 100.00 93.40 JT8D-9/9A 2 14.50 1.03 0 40 88.8 96.9 95.7 3 MCDONNELL DOUGLAS DC-09-30 98.00 93.40 JT8D-15 2 15.50 1.03 0 50 91.2 101.1 98.4 2 1 MCDONNELL DOUGLAS DC-09-30 103.00 95.30 JT8D-7 2 14.00 1.40 0 50 95.3 99.3 103.5 2 16,24 MCDONNELL DOUGLAS DC-09-30 108.00 98.10 JT8D-17 2 16.00 1.01 0 50 94.3 103.7 101.1 2 1 MCDONNELL DOUGLAS DC-09-30 103.00 98.10 JT8D-17 2 16.00 1.01 0 50 92.7 103.5 101.1 2 1 Page 163 ### Page 169 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES MCDONNELL DOUGLAS DC-09-30 108.00 99.00 JT8D-7A 2 14.00 1.40 0 50 95.1 97.3 97.3 2 1 MCDONNELL DOUGLAS DC-09-30 108.00 99.00 JT8D-9 2 14.50 1.03 0 50 96.4 100.3 103.7 2 24 MCDONNELL DOUGLAS DC-09-30 103.00 99.00 JT8D-9 2 14.50 1.03 0 50 94.3 99.0 99.0 2 1 MCDONNELL DOUGLAS DC-09-30 110.00 101.00 JT8D-7 2 14.00 1.40 0 50 95.9 97.1 97.3 2 1 MCDONNELL DOUGLAS DC-09-30 110.00 101.00 JT8D-7 2 14.00 1.40 0 50 97.5 99.0 104.3 2 16,24 MCDONNELL DOUGLAS DC-09-30 110.00 101.00 JT8D-9 2 14.50 1.03 0 50 97.0 100.3 104.3 2 24 Page 164 ### Page 170 04/24/2012 **MANUFACTURER** MCDONNELL DOUGLAS MODEL DC-09-30 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **114.00 102.00 JT8D-15 2 15.50 1.03 TO AP FLAPS 0 50 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 95.8 100.5 99.0 2 1 MCDONNELL DOUGLAS DC-09-30 114.00 102.00 JT8D-9 2 14.50 1.03 0 50 97.1 99.0 99.4 2 1 MCDONNELL DOUGLAS DC-09-30 (ABS) 111.00 101.00 JT8D-11 2 15.00 1.00 0 40 90.3 97.3 96.0 3 MCDONNELL DOUGLAS DC-09-30 (ABS/SA16136L) 103.00 99.00 JT8D-9/9A 2 14.50 1.03 0 40 89.7 96.8 96.0 3 12 MCDONNELL DOUGLAS DC-09-30 (ABS;STC SA1613GL) 107.00 101.00 JT8D-9/9A 2 14.50 1.03 0 40 90.1 97.1 96.0 3 MCDONNELL DOUGLAS DC-09-30(ABS) 111.00 101.00 JT8D-11 2 15.00 1.00 0 40 90.3 97.3 96.0 3 12 Page 165 ### Page 171 04/24/2012 **MANUFACTURER** MCDONNELL DOUGLAS MODEL DC-09-30(ABS/SA1613GL) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **103.00 99.00 JT8D-7/7A/7B 2 14.00 1.40 TO AP FLAPS 0 40 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 90.3 95.9 96.0 3 MCDONNELL DOUGLAS DC-09-30(ABS/SA1613GL) 105.00 101.00 JT8D-7/7A/7B 2 14.00 1.40 0 40 91.0 95.8 96.0 3 MCDONNELL DOUGLAS DC-09-30(ABS/SA1613GL) 105.00 101.00 JT8D-9/9A 2 14.50 1.03 0 40 90.3 96.7 96.1 3 MCDONNELL DOUGLAS DC-09-30(ABS/SA1785GL) 103.00 99.00 JT8D-7/7A/7B 2 14.00 1.40 0 40 90.4 95.9 96.0 3 MCDONNELL DOUGLAS DC-09-30(ABS/SA1785GL) 103.00 99.00 JT8D-9/9A 2 14.50 1.03 0 40 89.7 96.8 96.0 3 MCDONNELL DOUGLAS DC-09-30(ABS/SA1785GL) 107.00 101.00 JT8D-7/7A/7B 2 14.00 1.40 0 40 91.0 96.2 96.0 3 Page 166 ### Page 172 04/24/2012 **MANUFACTURER** MCDONNELL DOUGLAS MODEL DC-09-30(ABS/SA1785GL) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **107.00 101.00 JT8D-9/9A 2 14.50 1.03 TO AP FLAPS 0 40 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 90.1 97.1 96.0 3 MCDONNELL DOUGLAS DC-09-31/32/32F/33F(ABS;STC SA1613GL) 103.00 99.00 JT8D-7/7A/7B 2 14.00 1.40 0 40 90.3 95.9 96.0 3 MCDONNELL DOUGLAS DC-09-31/32/32F/33F(ABS;STC SA1613GL) 107.00 101.00 JT8D-7/7A/7B 2 14.00 1.40 0 40 91.0 96.2 96.0 3 MCDONNELL DOUGLAS DC-09-34 110.00 101.00 JT8D-9 2 14.50 1.03 0 50 96.1 98.8 99.1 2 1 MCDONNELL DOUGLAS DC-09-34 121.00 110.00 JT8D-15 2 15.50 1.03 0 50 97.8 102.1 101.4 2 1 MCDONNELL DOUGLAS DC-09-34 121.00 110.00 JT8D-17 2 16.00 1.01 0 50 98.0 103.0 101.9 2 1 Page 167 ### Page 173 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES MCDONNELL DOUGLAS DC-09-40 114.00 102.00 JT8D-11 2 15.00 1.00 0 50 96.8 99.5 99.4 2 1 MCDONNELL DOUGLAS DC-09-40 114.00 102.00 JT8D-15 2 15.50 1.03 0 50 95.8 100.5 99.4 2 1 MCDONNELL DOUGLAS DC-09-50 115.00 104.00 JT8D-17 2 16.00 1.01 0 50 96.4 103.4 101.6 2 1 MCDONNELL DOUGLAS DC-09-50 115.00 110.00 JT8D-15 2 15.50 1.03 0 50 96.1 102.4 101.9 2 1 MCDONNELL DOUGLAS DC-09-50 121.00 110.00 JT8D-15 2 15.50 1.03 0 50 97.8 102.2 101.9 2 1 MCDONNELL DOUGLAS DC-09-50 121.00 110.00 JT8D-17 2 16.00 1.01 0 50 98.1 103.2 101.9 2 1 Page 168 ### Page 174 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES MCDONNELL DOUGLAS DC-10-10 410.00 347.80 CF6-6D 3 39.30 5.90 14 50 97.4 97.0 104.9 3 * MCDONNELL DOUGLAS DC-10-10 410.00 347.80 CF6-6K 3 39.30 5.90 14 50 96.8 96.3 103.3 3 * MCDONNELL DOUGLAS DC-10-10 430.00 347.80 CF6-6K2 3 40.90 5.90 11 50 97.4 96.5 103.3 3 * MCDONNELL DOUGLAS DC-10-10 455.00 363.50 CF6-6D 3 39.30 5.90 0 50 101.8 96.0 105.5 3 * MCDONNELL DOUGLAS DC-10-10 455.00 363.50 CF6-6D1 3 40.30 5.80 4 50 100.2 96.6 105.5 3 * MCDONNELL DOUGLAS DC-10-10 430.00 363.50 CF6-6D1 3 40.30 5.80 11 50 98.1 97.0 105.5 3 * Page 169 ### Page 175 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES MCDONNELL DOUGLAS DC-10-10 455.00 363.50 CF6-6D1A 3 40.90 5.80 4 50 100.2 96.6 105.5 3 * MCDONNELL DOUGLAS DC-10-10 430.00 363.50 CF6-6D1A 3 40.90 5.80 11 50 98.1 97.0 105.5 3 * MCDONNELL DOUGLAS DC-10-10 455.00 363.50 CF6-6K 3 39.30 5.90 0 50 100.9 95.5 103.8 3 * MCDONNELL DOUGLAS DC-10-10 455.00 363.50 CF6-6K2 3 40.90 5.90 4 50 99.3 96.1 103.8 3 * MCDONNELL DOUGLAS DC-10-15 455.00 363.50 CF6-50C2-F 3 45.60 4.60 5 50 93.8 95.6 103.1 3 MCDONNELL DOUGLAS DC-10-30 555.00 403.00 CF6-50A 3 48.40 4.30 5 50 101.8 96.9 106.3 3 * Page 170 ### Page 176 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES MCDONNELL DOUGLAS DC-10-30 555.00 403.00 CF6-50C/H 3 50.40 4.30 10 50 101.6 97.5 106.3 3 MCDONNELL DOUGLAS DC-10-30 572.00 403.00 CF6-50C1 3 51.80 4.20 10 50 102.1 98.3 106.3 3 MCDONNELL DOUGLAS DC-10-30 555.00 403.00 CF6-50C2 3 51.80 4.30 5 50 96.8 97.8 105.0 3 MCDONNELL DOUGLAS DC-10-30 555.00 403.00 CF6-50C2-B 3 53.20 4.30 5 50 96.1 98.4 105.0 3 MCDONNELL DOUGLAS DC-10-30 555.00 403.00 CF6-50C2-R 3 50.40 4.40 10 50 97.5 97.2 105.0 3 MCDONNELL DOUGLAS DC-10-30 565.00 411.00 CF6-50A 3 48.40 4.30 5 50 102.7 96.8 106.6 3 * Page 171 ### Page 177 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES MCDONNELL DOUGLAS DC-10-30 572.00 411.00 CF6-50C/H 3 50.40 4.30 10 50 102.3 97.5 106.6 3 MCDONNELL DOUGLAS DC-10-30 590.00 411.00 CF6-50C1 3 51.80 4.20 10 50 103.0 98.0 106.6 3 MCDONNELL DOUGLAS DC-10-30 590.00 411.00 CF6-50C2 3 51.80 4.30 15 50 99.0 97.9 105.3 3 MCDONNELL DOUGLAS DC-10-30 590.00 411.00 CF6-50C2-B 3 53.20 4.30 15 50 98.7 98.5 105.3 3 MCDONNELL DOUGLAS DC-10-30 572.00 421.00 CF6-50C2-R 3 50.40 4.40 10 50 98.4 97.3 105.8 3 MCDONNELL DOUGLAS DC-10-30 555.00 424.00 CF6-50C2 3 51.80 4.30 5 50 96.8 97.8 106.0 3 15 Page 172 ### Page 178 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES MCDONNELL DOUGLAS DC-10-30 572.00 424.00 CF6-50C2-B 3 53.20 4.30 10 50 97.4 98.5 106.0 3 15 MCDONNELL DOUGLAS DC-10-30 555.00 424.00 CF6-50C2-B 3 53.20 4.30 5 50 96.1 98.4 106.0 3 15 MCDONNELL DOUGLAS DC-10-30 590.00 436.00 CF6-50C2 3 51.80 4.30 15 50 99.0 97.7 106.4 3 15 MCDONNELL DOUGLAS DC-10-40 530.00 403.00 JT9D-20D 3 44.50 5.00 10 50 100.8 95.2 105.7 3 * MCDONNELL DOUGLAS DC-10-40 555.00 403.00 JT9D-59A 3 51.70 4.90 10 50 101.4 98.0 106.4 3 * MCDONNELL DOUGLAS MD-10-10 440.00 373.50 CF6-6D 3 39.30 5.70 5 50 100.0 96.5 105.9 3 56 Page 173 ### Page 179 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES MCDONNELL DOUGLAS MD-10-10 440.00 373.50 CF6-6D W/ FSMS 3 39.30 5.70 5 50 100.1 96.4 105.9 3 56 MCDONNELL DOUGLAS MD-10-10 440.00 375.00 CF6-6K 3 39.30 5.90 5 50 99.2 96.2 104.4 3 56 MCDONNELL DOUGLAS MD-10-10 440.00 375.00 CF6-6K W/ FSMS 3 39.30 5.90 5 50 99.2 95.9 104.4 3 56 MCDONNELL DOUGLAS MD-10-30 565.00 424.00 CF6-50C2 3 51.80 4.30 10 50 96.9 97.4 106.0 3 57 MCDONNELL DOUGLAS MD-10-30 580.00 436.00 CF6-50C2 3 51.80 4.30 15 50 97.9 97.4 106.3 3 57 MCDONNELL DOUGLAS MD-11 602.50 430.00 CF6-80C2 3 61.50 5.30 10 50 92.8 96.3 103.6 3 Page 174 ### Page 180 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES MCDONNELL DOUGLAS MD-11 602.50 430.00 CF6-80C2D1F 3 61.50 5.30 10 50 92.8 96.3 103.6 3 MCDONNELL DOUGLAS MD-11 602.50 430.00 PW4460 3 60.00 5.00 10 50 93.7 96.3 103.8 3 MCDONNELL DOUGLAS MD-11 602.50 430.00 PW4462 3 62.00 5.00 10 50 93.1 96.6 103.8 3 MCDONNELL DOUGLAS MD-11 618.00 471.50 CF6-80C2 3 61.50 5.30 10 50 93.9 96.3 104.3 3 MCDONNELL DOUGLAS MD-11 630.50 481.50 PW4460 3 60.00 5.00 10 50 95.8 96.1 104.4 3 MCDONNELL DOUGLAS MD-11 630.50 481.50 PW4462 3 62.00 5.00 10 50 95.0 96.5 104.4 3 Page 175 ### Page 181 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES MCDONNELL DOUGLAS MD-11 A-1 602.50 430.00 CF6-80C2D1F 3 61.50 5.30 10 50 92.8 96.4 103.6 3 MCDONNELL DOUGLAS MD-11 A-1 602.50 430.00 PW4460 (-3) 3 60.00 5.00 10 50 93.9 96.3 103.4 3 MCDONNELL DOUGLAS MD-11 A-1 602.50 430.00 PW4462 (-3) 3 62.00 5.00 10 50 93.3 96.6 103.4 3 MCDONNELL DOUGLAS MD-11 A-1 630.50 481.50 CF6-80C2D1F 3 61.50 5.30 10 50 94.6 96.4 104.5 3 MCDONNELL DOUGLAS MD-11 A-1 630.50 481.50 PW4460 (-3) 3 60.00 5.00 10 50 95.7 96.1 104.4 3 MCDONNELL DOUGLAS MD-11 A-1 630.50 481.50 PW4462 (-3) 3 62.00 5.00 10 50 95.0 96.5 104.4 3 Page 176 ### Page 182 **APPENDIX 1, CHANGE 1** **AIRCRAFT NOISE DATA FOR** UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES MCDONNELL DOUGLAS MD-80 140.00 128.00 JT8D-209 2 19.25 1.83 0 40 88.9 94.7 92.8 3 10 MCDONNELL DOUGLAS MD-80 140.00 128.00 JT8D-219 2 21.70 1.70 0 40 86.7 97.3 92.8 3 10 MCDONNELL DOUGLAS MD-80 149.50 130.00 JT8D-209 2 19.25 1.83 0 40 91.1 94.5 92.9 3 10 MCDONNELL DOUGLAS MD-80 149.50 130.00 JT8D-217 2 20.85 1.80 0 40 89.7 95.8 92.9 3 10 MCDONNELL DOUGLAS MD-80 142.00 130.00 JT8D-217 2 20.85 1.80 0 40 88.2 96.1 92.9 3 10 MCDONNELL DOUGLAS MD-80 149.50 130.00 JT8D-219 2 21.70 1.70 0 40 88.6 97.1 92.9 3 10 Page 177 ### Page 183 **APPENDIX 1, CHANGE 1** **MANUFACTURER** MCDONNELL DOUGLAS MODEL MD-80 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **160.00 150.00 JT8D-217A 2 20.85 1.80 TO AP FLAPS 2 40** TO SL AP NOISE LEVEL (EPNdB) 92.0 95.9 93.7 STAGE 3 NOTES 10 MCDONNELL DOUGLAS MD-80 160.00 150.00 JT8D-217C 2 20.85 1.70 2 40 91.5 96.3 93.7 3 10 MCDONNELL DOUGLAS MD-80 160.00 150.00 JT8D-219 2 21.70 1.70 2 40 90.8 97.2 93.7 3 10 MCDONNELL DOUGLAS MD-80 (AFS QUIETEAGLE MD- 80; STC SE01650SE) 134.50 128.00 JT8D-217A w/AFS Quiet MD-80 HWS Noise Abatement System 2 20.85 1.80 0 40 84.2 95.4 93.4 3 MCDONNELL DOUGLAS MD-80 (AFS QUIETEAGLE MD- 80; STC SE01650SE) 134.50 128.00 JT8D-217C w/AFS Quiet MD-80 HWS Noise Abatement System 2 20.85 1.70 0 40 84.0 95.7 93.4 3 MCDONNELL DOUGLAS MD-80 (AFS QUIETEAGLE MD- 80; STC SE01650SE) 149.50 130.00 JT8D-219 w/AFS Quiet MD- 80 HWS Noise Abatement System 2 21.70 1.70 0 40 87.1 96.4 93.4 3 Page 178 ### Page 184 **APPENDIX 1, CHANGE 1** **MANUFACTURER** MCDONNELL DOUGLAS MODEL MD-80 (AFS QUIETEAGLE MD- 80; STC SE01650SE) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** 149.50 139.50 JT8D-217A w/AFS Quiet MD-80 HWS Noise Abatement System 2 20.85 1.80 TO AP FLAPS 0 40 TO SL AP NOISE LEVEL (EPNdB) 88.1 95.1 93.2 STAGE 3 NOTES MCDONNELL DOUGLAS MD-80 (AFS QUIETEAGLE MD- 80; STC SE01650SE) 158.00 150.00 JT8D-217C w/AFS Quiet MD-80 HWS Noise Abatement System 2 20.85 1.70 1 40 89.9 95.4 93.0 3 MCDONNELL DOUGLAS MD-80 (AFS QUIETEAGLE MD- 80; STC SE01650SE) 156.00 150.00 JT8D-219 w/AFS Quiet MD- 80 HWS Noise Abatement System 2 21.70 1.70 1 40 88.7 96.6 93.0 3 MCDONNELL DOUGLAS MD-87 125.00 120.00 JT8D-217A 2 20.85 1.80 0 40 84.3 96.4 92.9 3 10 MCDONNELL DOUGLAS MD-87 125.00 120.00 JT8D-217C 2 20.85 1.70 0 40 84.1 96.5 92.9 3 10 MCDONNELL DOUGLAS MD-87 140.00 128.00 JT8D-219 2 21.70 1.70 0 40 86.5 97.1 93.3 3 10 Page 179 ### Page 185 **APPENDIX 1, CHANGE 1** **MANUFACTURER** MCDONNELL DOUGLAS MODEL MD-87 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **149.50 130.00 JT8D-217A 2 20.85 1.80 TO AP FLAPS 1 40** TO SL AP NOISE LEVEL (EPNdB) 89.7 95.9 93.3 STAGE 3 NOTES 10 MCDONNELL DOUGLAS MD-87 149.50 130.00 JT8D-217C 2 20.85 1.70 1 40 89.2 96.2 93.3 3 10 MCDONNELL DOUGLAS MD-87 149.50 130.00 JT8D-219 2 21.70 1.70 1 40 88.5 97.1 93.3 3 10 MCDONNELL DOUGLAS MD-87 (AFS QUIETEAGLE MD- 80; STC SE01650SE) 127.50 120.00 JT8D-217C w/AFS Quiet MD-80 HWS Noise Abatement System 2 20.85 1.70 0 40 82.1 95.8 93.5 3 MCDONNELL DOUGLAS MD-87 (AFS QUIETEAGLE MD- 80; STC SE01650SE) 140.00 128.00 JT8D-217A w/AFS Quiet MD-80 HWS Noise Abatement System 2 20.85 1.80 0 40 85.5 95.2 93.4 3 MCDONNELL DOUGLAS MD-87 (AFS QUIETEAGLE MD- 80; STC SE01650SE) 149.50 130.00 JT8D-217C w/AFS Quiet MD-80 HWS Noise Abatement System 2 20.85 1.70 0 40 87.7 95.3 93.3 3 Page 180 ### Page 186 **APPENDIX 1, CHANGE 1** **MANUFACTURER** MCDONNELL DOUGLAS MODEL MD-87 (AFS QUIETEAGLE MD- 80; STC SE01650SE) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** 149.50 130.00 JT8D-219 w/AFS Quiet MD- 80 HWS Noise Abatement System 2 21.70 1.70 TO AP FLAPS 0 40 TO SL AP NOISE LEVEL (EPNdB) 86.9 96.4 93.3 STAGE 3 NOTES MCDONNELL DOUGLAS MD-87 (AFS QUIETEAGLE MD- 80; STC SE01650SE) 149.50 135.50 JT8D-217A w/AFS Quiet MD-80 HWS Noise Abatement System 2 20.85 1.80 0 40 87.9 95.0 93.2 3 MCDONNELL DOUGLAS MD-90-30 135.00 130.00 V2525-D5 2 25.00 4.80 5 40 78.3 89.2 91.7 3 MCDONNELL DOUGLAS MD-90-30 135.00 130.00 V2528-D5 2 28.00 4.80 5 40 77.2 91.4 91.7 3 MCDONNELL DOUGLAS MD-90-30 166.00 142.00 V2525-D5 2 25.00 4.80 5 40 84.2 88.8 91.9 3 MCDONNELL DOUGLAS MD-90-30 166.00 142.00 V2528-D5 2 28.00 4.80 5 40 82.6 91.0 91.9 3 Page 181 ### Page 187 04/24/2012 **MANUFACTURER** MITSUBISHI MODEL MU-300 (DIAMOND I) 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **14.10 13.20 JT15D-4 2 2.50 2.68 TO AP FLAPS 10 30 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 86.3 88.0 85.8 3 * MITSUBISHI MU-300 (DIAMOND I) 15.50 13.20 JT15D-4D 2 2.50 2.68 0 30 81.2 88.4 85.8 3 MITSUBISHI MU-300-10 (DIAM. II) 15.78 14.22 JT15D-5 2 2.90 2.10 10 30 88.6 93.7 91.4 3 * RAYTHEON 390 PREMIER 12.50 11.60 FJ44-2A 2 2.30 0 30 76.6 87.9 92.0 3 RAYTHEON C-29A 28.00 23.35 TFE731-5R-1H 2 4.30 3.30 0 45 81.4 87.3 95.8 3 RAYTHEON HAWKER 125- 1A 21.20 19.60 TFE731-3-1H 2 3.70 2.70 0 45 83.4 90.1 96.0 3 Page 182 ### Page 188 04/24/2012 **MANUFACTURER** RAYTHEON MODEL HAWKER 125- 1A 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **21.70 19.60 TFE731-3-1H 2 3.70 2.70 TO AP FLAPS 0 45 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 84.2 90.0 96.0 3 RAYTHEON HAWKER 125- 3A 21.70 20.00 TFE731-3-1H 2 3.70 2.70 0 45 84.2 90.0 96.3 3 RAYTHEON HAWKER 125- 3A/RA 23.60 20.00 TFE731-3-1H 2 3.70 2.70 0 45 85.5 89.8 95.7 3 RAYTHEON HAWKER 125- 400A 23.60 20.00 TFE731-3-1H 2 3.70 2.70 0 45 85.5 89.8 95.7 3 RAYTHEON HAWKER 125- 600A 25.50 22.00 TFE731-3-1H 2 3.70 2.70 0 45 88.0 89.2 96.3 3 RAYTHEON HAWKER 125- 600A 25.50 22.00 VIPER 601-22 2 3.65 0.00 0 45 92.3 99.2 102.9 2 12 Page 183 ### Page 189 04/24/2012 **MANUFACTURER** RAYTHEON MODEL HAWKER 125- 700A 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **25.50 22.00 TFE731-3-1H 2 3.70 2.70 TO AP FLAPS 0 45 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 88.0 89.2 96.3 3 33 RAYTHEON HAWKER 125- 700A 25.50 22.00 TFE731-3-1H 2 3.70 2.70 0 45 91.6 92.1 96.0 2 25,33 RAYTHEON HAWKER 125- 800 27.40 23.35 TFE731-5R-1H 2 4.30 3.30 0 45 80.9 87.2 96.5 3 RAYTHEON HAWKER 125- 800A 27.40 23.35 TFE731-5R-1H 2 4.30 3.30 0 45 80.9 89.6 96.5 3 25 RAYTHEON HAWKER 125-1000 31.00 25.00 PW305 2 5.20 4.50 0 25 81.8 85.9 91.6 3 RAYTHEON HAWKER 125-1000 35.50 28.50 PW305 2 5.20 4.50 0 25 85.7 85.3 92.0 3 Page 184 ### Page 190 04/24/2012 **MANUFACTURER** SABRELINER MODEL SABRELINER 40 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **17.50 14.00 JT12A-8 2 3.30 TO AP FLAPS 0 25 AC 36-1H** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) APPENDIX 1, CHANGE 1 89.7 100.4 97.5 2 SABRELINER SABRELINER 40 20.20 17.50 JT12A-8 2 3.30 0 25 94.5 100.1 98.4 2 SABRELINER SABRELINER 60 20.20 JT12A-8 2 3.30 24 95.0 100.3 98.5 2 * SABRELINER SABRELINER 60A/60SC 22.70 20.60 JT12A-8 2 3.30 0 94.4 100.0 102.2 2 SABRELINER SABRELINER 65 24.00 21.80 TFE731-3R 2 3.70 2.80 84.0 93.0 90.6 3 * SABRELINER SABRELINER 65 22.70 21.80 TFE731-3R 2 3.70 2.80 0 36 82.3 93.1 90.6 3 * Page 185 ### Page 191 **APPENDIX 1, CHANGE 1** **MANUFACTURER** SABRELINER MODEL SABRELINER 75A 1000# 1000# ENGINE MODEL THRUST 1000# BPRNO. **AIRCRAFT NOISE DATA FOR** **UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES** **MTOW MLW** **23.00 CF700-2D-2 2 4.50 2.00 TO AP FLAPS 15 25** TO SL AP NOISE LEVEL (EPNdB) 90.7 91.3 100.2 STAGE 2 NOTES * SABRELINER SABRELINER 80 23.30 22.00 CF700-2D-2 2 4.50 2.00 90.7 91.3 100.2 2 * SABRELINER SABRELINER 80A/80SC 25.50 22.00 CF700-2D-2 2 4.50 2.00 0 91.2 91.4 101.1 2 * Page 186 ### Page 192 **APPENDIX 2** **AIRCRAFT NOISE DATA FOR** FOREIGN CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP CHAPTER NOTES AEROSPATIALE CARAVELLE 10-B1R 119.00 109.00 JT8D-7 2 14.0 1.10 5 35 93.7 98.1 105.1 2 AEROSPATIALE CARAVELLE 10-B1R 114.50 109.00 JT8D-7 2 14.0 1.10 5 35 92.3 98.2 105.1 2 AEROSPATIALE CARAVELLE 10-B3 119.00 109.00 JT8D-7 2 14.0 1.10 5 45 94.4 97.7 106.2 2 AEROSPATIALE CARAVELLE 10-B3 125.60 109.00 JT8D-9 2 14.2 1.10 5 45 95.7 98.2 106.2 2 AEROSPATIALE CARAVELLE 11R 114.50 109.00 JT8D-7 2 14.0 1.10 5 35 92.3 97.9 105.1 2 AEROSPATIALE CARAVELLE 12 127.00 109.00 JT8D-9 2 14.2 1.10 5 45 96.6 98.2 105.9 2 AEROSPATIALE CARAVELLE 12 123.40 109.00 JT8D-9 2 14.2 1.10 5 45 95.3 98.3 105.9 2 AEROSPATIALE CARAVELLE 12 119.00 109.00 JT8D-9 2 14.2 1.10 5 45 94.0 98.4 105.9 2 AIRBUS A300B1 302.03 268.96 CF6-50C2R 2 50.4 4.30 0 25 90.8 97.4 102.9 3 AIRBUS A300B1 302.10 269.00 CF6-50A 2 48.4 4.60 25 87.9 90.7 101.1 2 AIRBUS A300B2 K3C 313.10 286.70 CF6-50C 2 50.4 4.30 25 87.0 92.6 101.7 2 AIRBUS A300B2-1A 302.10 281.10 CF6-50A 2 48.3 4.60 25 87.9 90.7 101.1 2 AIRBUS A300B2-1C 291.01 268.96 CF6-50C 2 50.4 4.30 0 25 89.9 97.5 102.9 3 AIRBUS A300B2-1C 313.05 286.70 CF6-50C 2 50.4 4.30 0 25 91.8 97.4 103.1 3 AIRBUS A300B2-202 313.00 287.00 CF6-50C1 2 51.7 4.60 0 25 89.3 93.5 102.0 3 AIRBUS A300B2-320 330.80 293.30 JT9D-59A 2 50.4 4.90 8 15 90.3 98.5 100.5 3 AIRBUS A300B4-102 347.30 294.80 CF6-50C1 2 51.7 4.60 25 90.1 93.3 101.9 2 AIRBUS A300B4-120 313.07 286.60 JT9D-59A 2 0 25 90.0 98.0 101.9 3 AIRBUS A300B4-120 363.78 295.43 JT9D-59A 2 0 25 93.5 97.6 103.2 3 2 AIRBUS A300B4-120 347.24 295.43 JT9D-59A 2 0 25 92.2 97.7 103.2 3 2 AIRBUS A300B4-120 363.78 299.84 JT9D-59A 2 0 25 93.6 97.5 102.3 3 AIRBUS A300B4-203 302.04 275.59 CF650.C2 2 0 25 89.9 98.3 102.4 3 AIRBUS A300B4-203 363.78 299.84 CF650.C2 2 0 25 93.9 97.9 102.9 3 Page 1 ### Page 193 **APPENDIX 2** **AIRCRAFT NOISE DATA FOR** FOREIGN CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP CHAPTER NOTES AIRBUS A300B4-2C 330.80 293.30 CF6-50C 2 50.4 4.30 25 89.0 92.4 101.9 2 AIRBUS A300B4-2C 337.40 293.30 CF6-50C 2 50.4 4.30 25 89.6 92.4 101.9 2 AIRBUS A300B4-2C 347.30 293.30 CF6-50C 2 50.4 4.30 25 90.5 92.4 101.9 2 AIRBUS A300B42C-13 302.03 286.60 CF6-50C2R 2 50.4 4.30 0 25 89.8 96.9 102.4 3 AIRBUS A300B42C-13 347.22 299.83 CF6-50C2R 2 50.4 4.30 0 25 93.2 96.7 102.4 3 AIRBUS A300B4-620 330.69 288.80 JT9D-7R4H1 2 56.0 5.00 0 40 89.3 99.4 100.7 3 AIRBUS A300B4-620 385.81 319.67 JT9D-7R4H1 2 56.0 5.00 0 40 93.0 98.9 101.0 3 AIRBUS A300B4-622-R 330.69 288.80 PW4158 2 57.8 4.70 0 40 88.0 98.0 101.3 3 AIRBUS A300B4-622-R 385.81 319.67 PW4158 2 57.8 4.70 0 40 93.1 97.6 101.9 3 AIRBUS A310-203 275.58 261.25 CF6-80A3 2 50.0 4.60 0 40 87.5 97.1 99.7 3 AIRBUS A310-203 305.56 267.86 CF6-80A3 2 50.0 4.60 0 40 90.2 96.8 99.9 3 AIRBUS A310-222 275.58 261.25 JT9D-7R4 2 50.0 5.00 0 40 86.3 95.6 100.6 3 AIRBUS A310-222 305.56 267.86 JT9D-7R4 2 50.0 5.00 0 40 89.7 95.4 100.6 3 AIRBUS A320-111 132.28 130.07 CFM56-5A1 2 25.0 6.00 10 35 82.1 94.8 96.3 3 AIRBUS A320-111 169.75 147.71 CFM56-5A1 2 25.0 6.00 10 35 89.8 94.3 96.7 3 ANTONOV AN-124 864.20 727.50 D-18T 4 51.4 6.00 30 30 109.9 100.4 108.2 2 ANTONOV AN-124-100 864.20 727.51 D-18T 4 51.4 6.00 30 30 106.0 102.7 104.6 3 1 ANTONOV AN-72-100 76.72 72.75 D-36 2 14.9 5.50 10 19 89.3 90.5 98.3 3 ANTONOV AN-74T 76.72 72.75 D-36 2 14.9 5.50 10 19 89.3 90.5 98.3 3 ANTONOV AN-74T-100 80.46 74.95 D-36 2 14.9 5.50 10 19 90.0 90.5 98.3 3 BAe 1-11 475 92.00 84.00 SPEY 512-14DW 2 12.6 0.70 6 45 93.0 102.2 100.3 2 1 BAe 1-11 500 99.70 87.00 SPEY 512-14DW 2 12.6 0.70 6 45 95.3 101.6 100.0 2 1 BAe 1-11 500S 104.50 87.00 SPEY 512-14DW 2 12.6 0.70 6 45 97.0 101.0 100.0 2 1 Page 2 ### Page 194 **APPENDIX 2** **AIRCRAFT NOISE DATA FOR** FOREIGN CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP CHAPTER NOTES BAe 1-11 510 92.50 86.00 SPEY 512-14E 2 12.0 0.70 8 45 93.3 101.7 101.7 2 1 BAe 146-100-20 82.25 73.35 ALF502R-3 4 6.7 5.90 18 33 83.1 86.9 95.2 3 BAe 146-200-01 89.50 79.50 ALF502-5 4 7.0 5.70 18 33 84.9 87.3 95.6 3 BAe CONCORDE 400.00 245.00 OLYMPUS 610 4 38.5 119.5 112.0 117.0 BAe HS 125-1 20.00 18.10 VIPER 520 2 3.0 0.00 0 45 91.1 97.3 103.6 2 BAe HS 125-1B 21.20 19.55 VIPER 521 2 3.2 0.00 0 45 91.6 98.4 104.8 2 BAe HS 125-1B/522 21.20 19.55 VIPER 522 2 3.3 0.00 0 45 89.8 100.0 104.3 2 BAe HS 125-1B/R522 22.20 19.60 VIPER 522 2 3.3 0.00 0 45 90.5 100.0 104.4 2 BAe HS 125-3B 21.70 20.00 VIPER 522 2 3.3 0.00 0 45 90.6 100.0 104.4 2 BAe HS 125-3B/RA 22.80 20.00 VIPER 522 2 3.3 0.00 0 45 91.5 100.0 104.5 2 BAe HS 125-400B 23.30 20.00 VIPER 522 2 3.3 0.00 0 45 92.0 100.0 104.5 2 BAe HS 125-403B 23.60 20.00 VIPER 522 2 3.3 0.00 0 45 92.4 100.0 104.5 2 BAe HS 125-600B 25.50 22.00 VIPER 601-22 2 3.7 0.00 0 45 88.7 97.2 102.7 2 1 BAe HS 125-600B 25.50 22.00 VIPER 601-22 2 3.7 0.00 0 45 93.4 101.1 101.9 2 BAe HS 125-600F 25.50 22.00 TFE 731-3-1H 2 3.7 2.70 0 45 88.0 89.3 96.0 3 BAe HS 125-700B 25.50 22.00 TFE 731-3-1H 2 3.7 2.70 0 45 88.0 89.3 96.0 3 DASSAULT FALCON 20H 32.00 27.60 ATF3-6A-4C 2 5.2 2.90 5 40 83.9 89.0 93.9 3 FOKKER 614 44.10 44.10 M45H 2 6.9 3.10 35 90.5 89.6 99.0 2 FOKKER F28 MK2000 65.00 59.00 RB183MK555-15 2 41.8 1.00 6 42 90.0 99.5 101.8 2 ILYUSHIN IL-62M 363.76 231.48 D-30KU 4 24.3 2.40 30 30 106.9 95.2 103.5 2 ILYUSHIN IL-62M 368.16 235.89 D-30KU II 4 24.3 2.40 30 30 107.2 95.2 103.9 2 ILYUSHIN IL-62M 369.30 235.90 D-30KU 4 24.3 2.40 30 30 102.5 99.1 102.6 3 1 ILYUSHIN IL-76T(TD) 374.80 334.00 D-30KP 4 26.5 2.36 30 30 103.1 102.7 108.9 2 Page 3 ### Page 195 **APPENDIX 2** **AIRCRAFT NOISE DATA FOR** FOREIGN CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP CHAPTER NOTES ILYUSHIN IL-76TD 418.87 333.99 D-30KP II 4 26.5 2.21 30 30 107.3 102.7 108.9 2 ILYUSHIN IL-86 473.98 385.80 NK-86 4 28.7 1.30 30 40 109.2 104.2 105.1 2 ILYUSHIN IL-86 463.00 385.80 NK-86 4 28.7 1.30 30 40 107.4 104.2 105.1 2 ILYUSHIN IL-96-300 507.05 385.80 PS-90A 4 35.3 4.70 25 40 101.2 97.6 104.2 3 1 ILYUSHIN IL-96-300 529.10 385.80 PS-90A 4 35.3 4.70 25 40 102.1 97.6 104.2 3 1 ILYUSHIN IL-96T 595.24 485.01 PW2337 4 39.0 6.00 25 40 103.5 99.3 105.5 3 TUPOLEV TU-134 99.20 88.20 D-30-I 2 15.0 1.00 10 38 92.9 101.9 101.4 2 TUPOLEV TU-134A/B 103.62 94.79 D-30-II 2 15.0 1.00 10 38 95.3 101.9 102.1 2 TUPOLEV TU-134A-3/B-3 104.90 94.80 D-30-III 2 15.3 0.84 10 30 95.5 102.5 101.3 2 TUPOLEV TU-134A-3/B-3 108.00 94.80 D-30-III 2 15.3 0.84 10 30 96.7 102.5 101.3 2 TUPOLEV TU-154 216.05 171.96 NK-8-2U 3 23.2 1.00 28 45 101.1 97.8 106.0 2 TUPOLEV TU-154 211.60 172.00 NK-8-2U 3 23.2 1.00 28 45 100.1 97.8 106.0 2 TUPOLEV TU-154M 220.50 176.40 D-30KU-154 3 24.3 2.40 28 45 94.3 98.0 102.5 2 TUPOLEV TU-154M 220.50 176.40 D-30KU-154 3 24.3 2.40 15 45 92.5 99.5 102.0 3 1 TUPOLEV TU-204 208.55 194.44 PS-90A 2 35.3 4.70 18 37 86.2 95.1 100.0 3 1 TUPOLEV TU-204-100 227.07 194.44 PS-90A 2 35.3 4.70 18 37 89.3 95.0 100.0 3 1 TUPOLEV TU-204-120 227.07 194.44 RB211-535E4 2 40.1 4.30 18 37 87.5 96.4 94.4 3 YAKOLEV YAK-40 35.49 32.40 AI-25 3 3.3 2.00 20 35 88.7 85.5 99.3 3 YAKOLEV YAK-42 119.00 110.23 D-36 3 14.3 5.60 20 45 93.8 93.6 102.6 2 YAKOLEV YAK-42D 124.60 111.30 D-36 3 14.3 5.60 20 45 90.9 92.8 99.6 3 1 Page 4 ### Page 196 AC36-1H Appendix 2 11/15/01 Appendix 2 Notes 1 Equipped With Standard Hushkit 2 Equipped With Modifications 3305 And 3373 ### Page 197 APPENDIX 3 ***STAGE 3*** TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES AEROSPATIALE SN601 CORVETTE 13.90 12.40 JT15D-4 2 2.50 2.68 15 35 80.4 85.4 89.5 3 * AEROSPATIALE SN601 CORVETTE 14.60 13.20 JT15D-4 2 2.50 2.68 15 35 74.0 81.0 90.0 3 AIRBUS A300 B4-605R 330.40 290.00 CF6-80C2A5F 2 61.50 5.00 0 40 87.4 98.8 99.5 3 AIRBUS A300 B4-605R 385.46 319.38 CF6-80C2A5F 2 61.50 5.00 0 40 91.5 98.5 100.0 3 AIRBUS A300B2-1C 291.00 268.00 CF6-50C2-R 2 50.40 4.40 0 25 89.9 97.5 102.9 3 AIRBUS A300B2-1C 313.00 286.60 CF6-50C2-R 2 50.40 4.40 0 25 91.8 97.4 103.1 3 AIRBUS A300B2-203 313.10 286.60 CF6-50-C2 2 51.80 4.30 16 25 91.1 97.9 103.1 3 AIRBUS A300B4-103 347.20 295.40 CF6-50-C2 2 51.80 4.30 16 25 93.6 97.7 103.0 3 AIRBUS A300B4-203 313.05 286.60 CF6-50C2 2 51.80 4.30 0 25 90.5 97.3 102.4 3 31 AIRBUS A300B4-203 363.70 299.83 CF6-50-C2 2 51.80 4.30 0 25 94.0 96.9 102.4 3 31 AIRBUS A300B4-622R 330.00 275.00 PW-4158 2 58.00 4.85 0 40 88.0 98.3 101.3 3 AIRBUS A300B4-622R 385.00 304.50 PW-4158 2 58.00 4.85 0 40 93.1 97.9 101.9 3 AIRBUS A310-221 305.60 267.90 JT9D-7R4D1 2 48.00 4.50 15 40 90.5 94.8 100.6 3 AIRBUS A310-304 275.58 261.25 CF6-80C2A2 2 53.50 5.00 0 40 85.7 96.5 98.5 3 AIRBUS A310-304 352.74 286.60 CF6-80C2A2 2 53.50 5.00 0 40 92.9 96.1 98.8 3 AIRBUS A310-324 330.69 271.16 PW-4152 2 52.00 4.85 15 40 90.6 97.2 100.2 3 AIRBUS A319-112 123.45 121.25 CFM56-5B6/P 2 23.50 6.00 10 40 78.5 93.2 93.7 3 Page 1 ### Page 198 APPENDIX 3 ***STAGE 3*** TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES AIRBUS A319-112 166.44 149.91 CFM56-5B6/P 2 23.50 6.00 10 40 86.3 92.0 94.4 3 AIRBUS A319-113 123.46 121.25 CFM56-5A4 2 22.00 6.00 10 40 80.1 93.9 94.0 3 AIRBUS A319-113 158.73 149.91 CFM56-5A4 2 22.00 6.00 10 40 87.5 93.1 94.8 3 AIRBUS A319-114 123.45 121.25 CFM56-5A5 2 23.50 6.00 10 40 79.5 94.9 94.0 3 AIRBUS A319-114 163.14 149.91 CFM56-5A5 2 23.50 6.00 10 40 86.8 94.2 94.8 3 AIRBUS A319-131 123.46 121.25 V2522-A5 2 22.00 4.90 10 40 79.2 92.5 94.0 3 AIRBUS A319-131 158.73 149.91 V2522-A5 2 22.00 4.90 10 40 85.3 91.4 94.5 3 AIRBUS A320-211 162.00 142.20 CFM56-5A1 2 25.00 6.00 10 35 87.8 94.3 96.4 3 AIRBUS A320-211 149.90 142.20 CFM56-5A1 2 25.00 6.00 10 35 85.3 94.4 96.4 3 AIRBUS A320-214 132.16 127.80 CFM56-5B4/P 2 27.00 5.90 10 35 78.8 95.2 95.5 3 AIRBUS A320-214 182.80 150.00 CFM56-5B4/P 2 27.00 5.90 10 35 88.0 93.7 95.8 3 AIRBUS A320-231 149.90 142.20 V2500.A1 2 25.00 6.00 10 40 84.0 93.0 96.6 3 AIRBUS A320-231 162.00 142.20 V2500.A1 2 25.00 6.00 10 40 86.6 92.8 96.6 3 AIRBUS A321-211 165.34 143.29 CFM56-5B3/P; Mod. No. 2 32.00 5.60 25 82.9 97.9 95.6 3 27772 AIRBUS A321-211 205.02 171.51 CFM56-5B3/P; Mod. No. 2 32.00 5.60 25 89.8 97.5 96.6 3 27772 AIRBUS A321-231 165.34 143.29 V2533A5 2 33.00 4.46 25 81.8 95.6 95.1 3 AIRBUS A321-231 205.02 171.51 V2533A5 2 33.00 4.46 25 88.2 95.2 95.8 3 AIRBUS A330-301 396.83 361.56 CF6-80E1A2 2 65.80 5.05 14 32 87.0 97.9 98.5 3 Page 2 ### Page 199 APPENDIX 3 ***STAGE 3*** TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES AIRBUS A330-301 507.06 418.88 CF6-80E1A2 2 65.80 5.05 14 32 94.2 97.2 98.7 3 AIRBUS A330-321 396.83 330.69 PW4164 2 64.00 4.85 8 32 88.5 98.0 97.3 3 AIRBUS A330-321 507.06 418.88 PW4164 2 64.00 4.85 8 32 95.6 97.5 98.0 3 AIRBUS A330-322 396.83 330.69 PW4168 2 68.00 4.85 8 32 87.6 98.6 97.3 3 AIRBUS A330-322 507.06 418.88 PW4168 2 68.00 4.85 8 32 94.3 98.3 98.0 3 AIRBUS A340-212 485.01 363.76 CFM56-5C3 4 32.50 6.60 17 32 88.1 95.8 97.3 3 AIRBUS A340-212 595.25 440.92 CFM56-5C3 4 32.50 6.60 17 32 96.1 95.4 97.2 3 AIRBUS A340-312 485.02 363.76 CFM56-5C3 4 32.50 6.60 17 32 88.0 95.8 97.3 3 AIRBUS A340-312 595.24 440.92 CFM56-5C3 4 32.50 6.60 17 32 96.2 95.3 97.2 3 AIRBUS UK 1-11 400 (QTV STC: ST02167AT) 81.90 78.00 SPEY511-14/14W 2 11.40 0.70 26 90.0 96.2 93.8 3 BAE SYSTEMS (AVRO) 146-RJ 100 95.00 83.00 LF 507-1F 4 7.00 5.10 18 33 83.8 88.3 97.2 3 BAE SYSTEMS (AVRO) 146-RJ 100 101.50 88.50 LF 507-1F 4 7.00 5.10 18 33 86.1 88.1 97.6 3 BAE SYSTEMS (AVRO) 146-RJ 70 84.00 83.50 LF 507-1F 4 7.00 5.10 18 33 80.2 89.1 97.5 3 4 BAE SYSTEMS (AVRO) 146-RJ 70 84.00 83.50 LF 507-1F 4 6.13 5.10 18 33 81.9 87.2 97.5 3 BAE SYSTEMS (AVRO) 146-RJ 70 90.00 83.50 LF 507-1F 4 6.13 5.10 18 33 84.1 86.9 97.5 3 BAE SYSTEMS (AVRO) 146-RJ 70 95.00 83.50 LF 507-1F 4 7.00 5.10 18 33 83.6 88.6 97.5 3 4 BAE SYSTEMS (AVRO) 146-RJ 85 89.50 77.50 LF 507-1F 4 7.00 5.10 18 33 81.9 88.7 96.9 3 BAE SYSTEMS (AVRO) 146-RJ 85 97.00 85.00 LF 507-1F 4 7.00 5.10 18 33 84.3 88.4 97.3 3 Page 3 ### Page 200 APPENDIX 3 ***STAGE 3*** **TURBOJET POWERED AIRPLANES** MANUFACTURER BAE SYSTEMS (BAe) MODEL 146-100A 1000# MTOW 76.00 1000# MLW 72.35 **ENGINE MODEL ALF502R-3 NO.** 4 THRUST 1000# **6.70 BPR** **5.90 TO AP FLAPS 18 33** TO SL AP NOISE LEVEL (EPNdB) 80.7 87.2 95.1 STAGE NOTES 3 BAE SYSTEMS (BAe) 146-100A 76.00 72.35 ALF502R-3A 4 6.70 5.90 18 33 79.0 88.0 94.9 3 BAE SYSTEMS (BAe) 146-100A 82.25 73.35 ALF502R-3A 4 6.70 5.90 18 33 82.3 87.6 95.2 3 BAE SYSTEMS (BAe) 146-100A 82.25 73.35 ALF502R-5 4 6.97 5.70 18 33 82.3 87.6 95.2 3 BAE SYSTEMS (BAe) 146-100A 84.00 77.50 ALF502R-5 4 6.97 5.70 18 33 81.8 87.7 95.6 3 BAE SYSTEMS (BAe) 146-200A 89.50 77.50 ALF502R-3 4 6.97 5.90 18 33 85.9 86.6 95.6 3 BAE SYSTEMS (BAe) 146-200A 89.50 77.50 ALF502R-3A 4 6.70 5.90 18 33 84.9 87.3 95.6 3 BAE SYSTEMS (BAe) 146-200A 89.50 77.50 ALF502R-5 4 6.97 5.70 18 33 84.9 87.3 95.6 3 BAE SYSTEMS (BAe) 146-200A 93.00 81.00 ALF502R-5 4 6.97 5.70 18 33 85.2 87.3 95.8 3 BAE SYSTEMS (BAe) 146-300 95.00 83.00 LF 507-1H/-1F 4 7.00 5.10 18 33 84.0 87.9 97.2 3 BAE SYSTEMS (BAe) 146-300 101.50 88.50 LF 507-1H/-1F 4 7.00 5.10 18 33 86.3 87.6 97.6 3 BAE SYSTEMS (BAe) 146-300A 95.00 83.00 ALF 502R-5 4 6.97 5.70 18 33 86.0 87.0 96.0 3 BAE SYSTEMS (BAe) 146-300A 97.50 84.50 ALF502R-5 4 6.97 5.70 18 33 86.5 86.7 95.6 3 BEECH BEECHJET 400 15.78 14.22 JT15D-5 2 2.90 2.10 10 30 88.6 93.7 91.4 3 * BOEING BOEING BOEING BOEING B-707-100B (BAC II STC: ST00956LA) B-707-300B/C (QSI STC: ST00702LA) B-707-300B/C (QSI STC: ST00702LA) B-707-300B/C (QSI STC: ST00702LA) 200.00 215.00 336.00 336.00 160.00 190.00 247.00 247.00 JT3D-1 JT3D-3B JT3D-3B JT3D-7 4 4 4 4 17.00 18.00 18.00 19.00 1.40 1.40 1.40 1.40 20 14 14 14 30 25 25 25 95.5 96.2 99.5 98.5 99.5 99.6 98.2 99.3 101.1 101.4 102.9 102.7 3 3 3 3 12 12 12 12 Page 4 ### Page 201 APPENDIX 3 ***STAGE 3*** **TURBOJET POWERED AIRPLANES** MANUFACTURER BOEING MODEL B-717-200 1000# MTOW 104.50 1000# MLW 98.00 **ENGINE MODEL BR700-715A1-30 NO.** 2 THRUST 1000# **18.50 BPR** **4.66 TO AP FLAPS 5 40** TO SL AP NOISE LEVEL (EPNdB) 79.6 89.2 91.3 STAGE NOTES 3 48 BOEING B-717-200 104.50 98.00 BR700-715A1-30 (MP) 2 18.50 4.66 5 40 80.1 89.2 91.3 3 49 BOEING B-717-200 104.50 98.00 BR700-715C1-30 2 21.00 4.66 5 40 78.1 91.7 91.3 3 48 BOEING B-717-200 104.50 98.00 BR700-715C1-30 (MP) 2 21.00 4.66 5 40 78.7 91.7 91.3 3 49 BOEING B-717-200 121.00 110.00 BR700-715A1-30 2 18.00 4.66 5 40 84.0 89.0 91.6 3 48 BOEING B-717-200 121.00 110.00 BR700-715A1-30 (MP) 2 18.50 4.66 5 40 84.1 89.0 92.1 3 49 BOEING B-717-200 121.00 110.00 BR700-715C1-30 2 21.00 4.66 5 40 82.1 91.5 91.6 3 48 BOEING B-717-200 121.00 110.00 BR700-715C1-30 (MP) 2 21.00 4.66 5 40 82.2 91.5 92.1 3 49 BOEING B-727-100 (Dee Howard) 169.50 137.50 TAY 651-54 3 15.40 5 40 92.1 92.3 98.4 3 BOEING B-727-100 (Dee Howard) 169.50 142.50 TAY 651-54 3 15.40 5 30 92.1 92.3 95.3 3 BOEING B727-100 (DUGAN AIR STC) 160.50 142.50 JT8D-7 3 14.00 1.40 4 26 93.5 98.6 97.2 3 BOEING BOEING BOEING BOEING BOEING BOEING BOEING B727-100 (FED EX; STC SA3993NM) B727-100 (FED EX; STC SA3993NM) B727-100 (FED EX; STC SA3993NM) B727-100 (FED EX; STC SA3993NM) B727-100 (FED EX; STC SA3993NM) B727-100 (FED EX; STC SA3993NM) B727-100 (FED EX; STC SA3993NM) 160.50 163.50 169.50 169.50 169.50 169.50 174.50 137.50 137.50 137.50 142.50 142.50 142.50 142.50 JT8D-7 w/BOEING INLET+CHIN CSD JT8D-7 w/BOEING INLET+FAN CSD JT8D-9 w/BOEING INLET+CHIN CSD JT8D-7 w/BOEING INLET+FAN CSD JT8D-7 w/BURBANK INLET+ FAN CSD JT8D-7 w/BURBANK INLET+CHIN CSD JT8D-9 w/BOEING INLET+CHIN CSD 3 3 3 3 3 3 3 14.00 14.00 14.50 14.00 14.00 14.00 14.50 1.40 1.40 1.03 1.40 1.40 1.40 1.03 5 5 5 5 5 5 5 30 30 30 30 30 30 30 92.5 93.2 93.9 94.5 94.1 94.1 94.1 96.6 97.4 97.5 97.2 97.2 96.6 97.2 97.8 97.8 98.1 98.0 98.2 98.2 98.9 3 3 3 3 3 3 3 35 35 35 35 35 35 35 Page 5 ### Page 202 APPENDIX 3 ***STAGE 3*** **TURBOJET POWERED AIRPLANES** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL NO. THRUST 1000# BPR FLAPS TO AP NOISE LEVEL (EPNdB) TO SL AP STAGE NOTES BOEING BOEING BOEING BOEING BOEING BOEING BOEING BOEING BOEING BOEING BOEING BOEING B727-100 (FED EX; STC SA3993NM) B727-100 (FED EX; STC SA3993NM) B727-100 (FED EX; STC SA3993NM) B727-100 (FED EX; STC SA3993NM) B727-100 (FED EX; STC SA3993NM) B727-100 RE (ROHR STC SA4363NM) B727-100 RE (ROHR STC SA4363NM) B727-100 RE (ROHR STC SA4363NM) B727-100 RE (ROHR STC SA4363NM) B727-100 RE (ROHR STC SA4363NM) B727-100 RE (ROHR STC SA4363NM) B727-200 (DUGAN AIR STC) 169.50 160.50 174.50 175.50 175.50 160.50 174.50 169.50 174.50 169.50 174.50 190.50 142.50 142.50 142.50 154.50 154.50 142.50 142.50 142.50 142.50 142.50 142.50 164.00 JT8D-9 w/BOEING INLET+FAN CSD JT8D-9 w/BURBANK INLET+CHIN CSD JT8D-9 w/BURBANK INLET+CHIN CSD JT8D-7 w/BOEING INLET+CHIN CSD JT8D-7 w/BURBANK INLET+CHIN CSD JT8D-217C/JT8D-9 JT8D-217C/JT8D-9 JT8D-219/JT8D-7B JT8D-219/JT8D-7B JT8D-219/JT8D-9 JT8D-219/JT8D-9 JT8D-15 3 3 3 3 3 3 3 3 3 3 3 3 14.50 14.50 14.50 14.00 14.00 15.50 1.03 1.03 1.03 1.40 1.40 1.03 5 5 5 5 5 5 5 5 5 5 5 4 30 30 30 30 30 30 30 30 30 30 30 26 93.9 91.7 94.9 96.6 96.3 87.0 89.4 88.1 89.0 88.0 88.8 94.9 98.0 97.6 97.1 96.9 96.0 98.2 98.0 98.8 98.8 98.9 98.8 99.2 98.4 98.8 98.8 99.1 99.1 95.4 95.4 95.4 95.4 95.4 95.4 97.0 3 3 3 3 3 3 3 3 3 3 3 3 35 35 35 35 35 23 23 23 23 23 23 BOEING B727-200 (DUGAN AIR STC) 209.41 164.00 JT8D-15 3 15.50 1.03 4 26 97.0 99.5 97.0 3 BOEING B727-200 (DUGAN AIR STC) 190.50 164.00 JT8D-9 3 14.50 1.03 4 26 95.0 98.3 97.0 3 BOEING BOEING BOEING BOEING B727-200 (FED EX; STC SA4833NM) B727-200 (FED EX; STC SA4833NM) B727-200 (FED EX; STC SA4833NM) B727-200 (FED EX; STC SA4833NM) 172.50 172.50 172.50 172.50 148.00 150.00 150.00 150.00 JT8D-9 w/BURBANK INLET+CHIN CSD JT8D-7 w/BOEING INLET+CHIN CSD JT8D-7 w/BOEING INLET+FAN CSD JT8D-7 w/BURBANK INLET+ FAN CSD 3 3 3 3 14.50 14.00 14.00 14.00 1.03 1.40 1.40 1.40 5 5 5 5 30 30 30 30 94.6 95.9 95.9 95.6 97.2 96.3 97.0 96.5 100.1 99.0 99.0 98.9 3 3 3 3 35 35 35 35 Page 6 ### Page 203 APPENDIX 3 ***STAGE 3*** TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B727-200 (FED EX; STC 172.50 150.00 JT8D-7 w/BURBANK 3 14.00 1.40 5 30 95.6 95.8 98.9 3 35 SA4833NM) INLET+CHIN CSD BOEING B727-200 (FED EX; STC 169.50 150.00 JT8D-9 w/BURBANK 3 14.50 1.03 5 30 94.1 97.8 100.2 3 35 SA4833NM) INLET+ FAN CSD BOEING B727-200 (FED EX; STC 177.60 154.50 JT8D-7 w/BOEING 3 14.00 1.40 5 30 95.2 97.3 99.0 3 35 SA4833NM) INLET+CHIN CSD BOEING B727-200 (FED EX; STC 177.60 154.50 JT8D-7 w/BOEING 3 14.00 1.40 5 30 95.2 97.9 99.0 3 35 SA4833NM) INLET+FAN CSD BOEING B727-200 (FED EX; STC 177.60 154.50 JT8D-9 w/BOEING 3 14.50 1.03 5 30 94.7 97.7 99.7 3 35 SA4833NM) INLET+CHIN CSD BOEING B727-200 (FED EX; STC 177.60 154.50 JT8D-9 w/BOEING 3 14.50 1.03 5 30 94.7 98.2 99.7 3 35 SA4833NM) INLET+FAN CSD BOEING B727-200 (FED EX; STC 177.60 154.50 JT8D-9 w/BURBANK 3 14.50 1.03 5 30 94.1 98.0 100.3 3 35 SA4833NM) INLET+ FAN CSD BOEING B727-200 (FED EX; STC 177.60 154.50 JT8D-9 w/BURBANK 3 14.50 1.03 5 30 94.1 97.5 100.3 3 35 SA4833NM) INLET+CHIN CSD BOEING B727-200 (FED EX; STC 155.00 150.00 JT8D-9 w/BOEING 3 14.50 1.03 5 30 89.2 97.9 97.4 3 27 SA5839NM) INLET+CHIN CSD BOEING B727-200 (FED EX; STC 155.00 150.00 JT8D-9 w/BOEING 3 14.50 1.03 5 30 89.2 98.4 97.4 3 27 SA5839NM) INLET+FAN CSD BOEING B727-200 (FED EX; STC 155.00 150.00 JT8D-9 w/BURBANK 3 14.50 1.03 5 30 88.5 98.1 98.0 3 27 SA5839NM) INLET+ FAN CSD BOEING B727-200 (FED EX; STC 155.00 150.00 JT8D-9 w/BURBANK 3 14.50 1.03 5 30 88.5 97.6 98.0 3 27 SA5839NM) INLET+CHIN CSD BOEING B727-200 (FED EX; STC 160.00 154.50 JT8D-15 w/BOEING 3 15.50 1.03 5 30 92.2 98.0 97.6 3 27 SA5839NM) INLET+CHIN CSD BOEING B727-200 (FED EX; STC 160.00 154.50 JT8D-15 w/BOEING 3 15.50 1.03 5 30 92.2 98.2 97.6 3 27 SA5839NM) INLET+FAN CSD BOEING B727-200 (FED EX; STC 178.90 154.50 JT8D-15 w/BURBANK 3 15.50 1.03 5 30 94.3 97.3 98.2 3 27 SA5839NM) INLET+ FAN CSD BOEING B727-200 (FED EX; STC 184.20 154.50 JT8D-17 w/BOEING 3 16.00 1.01 5 30 95.3 98.8 97.6 3 27 SA5839NM) INLET+CHIN OR FAN CSD BOEING B727-200 (FED EX; STC 184.20 154.50 JT8D-17 w/BURBANK 3 16.00 1.01 5 30 94.8 98.6 98.2 3 27 SA5839NM) INLET+CHIN OR FAN CSD BOEING B727-200 (FED EX; STC 190.50 154.50 JT8D-17R w/BOEING 3 17.40 0.97 5 30 96.4 99.2 97.6 3 27 SA5839NM) INLET+CHIN OR FAN CSD Page 7 ### Page 204 APPENDIX 3 ***STAGE 3*** TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B727-200 (FED EX; STC 197.00 154.50 JT8D-17R w/BOEING 3 17.40 0.97 5 30 96.0 99.4 97.6 3 27 SA5839NM) INLET+CHIN OR FAN CSD BOEING B727-200 (FED EX; STC 184.50 154.50 JT8D-17R w/BURBANK 3 17.40 0.97 5 30 94.8 99.1 98.2 3 27 SA5839NM) INLET+CHIN OR FAN CSD BOEING B727-200 (FED EX; STC 197.50 161.00 JT8D-17R w/BURBANK 3 17.40 0.97 5 30 96.9 98.8 98.4 3 27 SA5839NM) INLET+CHIN OR FAN CSD BOEING B727-200 (FED EX; STC 199.05 166.00 JT8D-15 w/BOEING 3 15.50 1.03 5 30 97.6 98.0 98.1 3 27 SA5839NM) INLET+CHIN CSD BOEING B727-200 (FED EX; STC 199.05 166.00 JT8D-15 w/BOEING 3 15.50 1.03 5 30 97.6 98.2 98.1 3 27 SA5839NM) INLET+FAN CSD BOEING B727-200 (FED EX; STC 203.10 166.00 JT8D-17 w/BOEING 3 16.00 1.01 5 30 96.8 99.1 98.0 3 27 SA5839NM) INLET+CHIN OR FAN CSD BOEING B727-200 (FED EX; STC 196.00 166.00 JT8D-9 w/BOEING 3 14.50 1.03 5 30 97.5 96.1 98.0 3 27 SA5839NM) INLET+CHIN CSD BOEING B727-200 (FED EX; STC 196.00 166.00 JT8D-9 w/BOEING 3 14.50 1.03 5 30 97.5 96.6 98.0 3 27 SA5839NM) INLET+FAN CSD BOEING B727-200 (RAISBECK STC 166.40 153.30 JT8D-9 3 14.50 1.03 5 25 96.5 97.9 97.6 3 17,34,43 ST00399SE) BOEING B727-200 (RAISBECK STC 179.70 166.00 JT8D-9 3 14.50 1.03 5 30 97.0 97.6 97.2 3 34,44 ST00555SE) BOEING B727-200 (RAISBECK STC 193.00 161.00 JT8D-15 3 15.50 1.03 5 30 97.4 96.5 99.9 3 45 ST00685SE) BOEING B-727-200 RE (ROHR STC 190.50 152.50 JT8D-219/JT8D-9 3 5 30 90.9 99.2 98.8 3 23,60 SA4363NM) BOEING B-727-200 RE (ROHR STC 184.00 156.00 JT8D-217C/JT8D-15 3 5 30 89.8 99.2 98.9 3 23,61 SA4363NM) BOEING B-727-200 RE (ROHR STC 184.00 156.00 JT8D-217C/JT8D-9 3 5 30 90.2 98.4 98.9 3 23,60 SA4363NM) BOEING B-727-200 RE (ROHR STC 190.50 159.00 JT8D-217C/JT8D-17 3 5 30 91.2 99.3 99.0 3 23,62 SA4363NM) BOEING B-727-200 RE (ROHR STC 209.50 162.00 JT8D-217C/JT8D-17 3 5 30 95.2 99.2 99.0 3 23,62 SA4363NM) BOEING B-727-200 RE (ROHR STC 198.50 162.00 JT8D-217C/JT8D-9 3 5 30 93.7 98.2 99.0 3 23,60 SA4363NM) BOEING B-727-200 RE (ROHR STC 198.70 162.00 JT8D-219/JT8D-15 3 5 30 92.7 99.4 99.0 3 7,23,64 SA4363NM) Page 8 ### Page 205 APPENDIX 3 ***STAGE 3*** TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-727-200 RE (ROHR STC 198.70 162.00 JT8D-219/JT8D-9 3 5 30 93.0 99.1 99.0 3 23,60 SA4363NM) BOEING B-727-200 RE (ROHR STC 209.42 164.00 JT8D-217C/JT8D-15 3 5 30 95.3 98.8 99.1 3 23,61 SA4363NM) BOEING B-737-200 (AVAERO;STC 128.10 88.00 JT8D-17 2 16.00 1.01 1 40 91.4 97.5 96.7 3 27 ST223CH) BOEING B-737-200 (AVAERO;STC 100.80 95.00 JT8D-15 2 15.50 1.03 1 40 83.7 96.8 97.2 3 27,42 ST223CH) BOEING B-737-200 (AVAERO;STC 100.80 95.00 JT8D-9 2 14.50 1.03 1 40 85.2 95.5 97.2 3 27,41 ST223CH) BOEING B-737-200 (AVAERO;STC 100.50 98.00 JT8D-15 2 15.50 1.03 1 40 84.9 96.9 98.6 3 35,42 ST223CH) BOEING B-737-200 (AVAERO;STC 100.50 98.00 JT8D-9 2 14.50 1.03 1 40 86.3 95.7 98.6 3 35,41 ST223CH) BOEING B-737-200 (AVAERO;STC 121.50 107.00 JT8D-15 2 15.50 1.03 1 30 91.3 96.9 96.3 3 35,42 ST223CH) BOEING B-737-200 (AVAERO;STC 128.10 107.00 JT8D-17 2 16.00 1.01 1 30 91.4 97.5 94.8 3 27 ST223CH) BOEING B-737-200 (AVAERO;STC 118.50 107.00 JT8D-9 2 14.50 1.03 1 30 91.5 94.9 96.3 3 35,41 ST223CH) BOEING B-737-200 (AVAERO;STC 121.50 107.00 JT8D-9 2 14.50 1.03 1 40 91.5 94.8 98.0 3 27,41 ST223CH) BOEING B-737-200 (NORDAM;STC 119.50 103.00 JT8D-15 w/LGW HUSHKIT 2 15.50 1.03 1 30 91.1 97.0 95.8 3 37 ST00131SE) BOEING B-737-200 (NORDAM;STC 119.50 103.00 JT8D-15 w/LGW-L 2 15.50 1.03 1 30 90.2 96.8 95.8 3 37 ST00131SE) HUSHKIT BOEING B-737-200 ADV (NORDAM; 110.20 98.00 JT8D-9 2 14.50 1.03 1 40 87.3 94.7 98.2 3 27,41 STC SA5730NM) BOEING B-737-200 ADV (NORDAM; 105.60 103.00 JT8D-15 2 15.50 1.03 1 40 84.6 96.3 98.4 3 27,42 STC SA5730NM) BOEING B-737-200 ADV (NORDAM; 115.50 103.00 JT8D-17 2 16.00 1.01 1 40 86.8 97.0 98.4 3 27 STC SA5730NM) BOEING B-737-200 ADV (NORDAM; 124.50 107.00 JT8D-9 2 14.50 1.03 1 40 91.9 94.4 98.6 3 27,41 STC SA5730NM) BOEING B-737-200 ADV (NORDAM; 100.50 95.00 JT8D-9 w/LGW HUSHKIT 2 14.50 1.03 1 30 86.1 96.7 96.2 3 36 STC ST00131SE) Page 9 ### Page 206 APPENDIX 3 ***STAGE 3*** TURBOJET POWERED AIRPLANES MANUFACTURER MODEL 1000# MTOW 1000# MLW ENGINE MODEL NO. THRUST 1000# BPR TO AP FLAPS TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) BOEING BOEING BOEING BOEING BOEING BOEING BOEING BOEING BOEING BOEING BOEING BOEING BOEING BOEING B-737-200 ADV (NORDAM; STC ST00131SE) B-737-200 ADV (NORDAM; STC ST00131SE) B-737-200 ADV (NORDAM; STC ST00131SE) B-737-200 ADV (NORDAM; STC ST00131SE) B-737-200 ADV (NORDAM; STC ST00131SE) B-737-200 ADV (NORDAM; STC ST00131SE) B-737-200 ADV (NORDAM; STC ST00131SE) B-737-200 ADV(AVAERO;STC ST223CH) B-737-200 ADV(AVAERO;STC ST223CH) B-737-200 ADV(AVAERO;STC ST223CH) B-737-200 ADV(AVAERO;STC ST223CH) B-737-200 ADV(AVAERO;STC ST223CH) B-737-200 ADV(AVAERO;STC ST223CH) B-737-300 109.00 100.50 100.50 121.60 118.70 122.90 118.50 100.80 100.80 100.50 124.50 128.10 121.50 124.50 98.00 98.00 99.00 107.00 107.00 107.00 107.00 95.00 95.00 98.00 107.00 107.00 107.00 110.00 JT8D-7 w/LGW-N HUSHKIT JT8D-9 w/LGW-N HUSHKIT JT8D-9 w/LGW-L HUSHKIT JT8D-15 w/LGW HUSHKIT JT8D-9 w/LGW HUSHKIT JT8D-9 w/LGW-L HUSHKIT JT8D-9 w/LGW-N HUSHKIT JT8D-15 JT8D-9 JT8D-9 JT8D-15 JT8D-17 JT8D-9 CFM56-3 w/HWFAP 2 2 2 2 2 2 2 2 2 2 2 2 2 2 14.00 14.50 14.50 15.50 14.50 14.50 14.50 15.50 14.50 14.50 15.50 16.00 14.50 20.00 1.40 1.03 1.03 1.03 1.03 1.03 1.03 1.03 1.03 1.03 1.03 1.01 1.03 5.00 1 1 1 1 1 1 1 1 1 1 1 1 1 1 30 30 30 30 30 30 30 40 40 40 30 30 40 40 89.2 86.1 86.9 91.7 91.6 91.8 91.6 83.7 85.3 86.4 91.8 91.2 91.5 82.4 96.3 96.9 96.5 96.7 96.1 96.0 96.5 96.9 95.7 95.8 96.7 97.7 95.0 89.7 96.2 96.2 95.8 95.9 95.9 95.9 96.2 96.9 96.9 98.3 96.3 94.8 97.7 98.5 3 3 3 3 3 3 3 3 3 3 3 3 3 3 40 36 36 37 36 36 36 27,42 27,41 35,41 35,42 27 27,41 BOEING B-737-300 124.50 110.00 CFM56-3 w/HWFAP 2 22.00 5.00 1 40 81.6 91.2 98.5 3 BOEING B-737-300 124.50 110.00 CFM56-3 w/HWFAP 2 22.00 5.00 1 40 81.6 91.2 97.4 3 38 BOEING B-737-300 124.50 110.00 CFM56-3 w/HWFAP 2 20.00 5.00 1 40 82.4 89.7 97.4 3 38 BOEING B-737-300 124.50 110.00 CFM56-3-B1 2 20.00 5.00 1 40 84.4 90.4 99.6 3 Page 10 ### Page 207 APPENDIX 3 ***STAGE 3*** TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-737-300 124.50 110.00 CFM56-3B-2 2 22.00 4.90 1 40 82.8 92.2 99.6 3 BOEING B-737-300 139.50 121.00 CFM56-3 w/HWFAP 2 22.00 5.00 1 40 83.9 90.9 97.6 3 38 BOEING B-737-300 139.50 121.00 CFM56-3 w/HWFAP 2 20.00 5.00 1 40 85.2 89.2 97.6 3 38 BOEING B-737-300 139.50 121.00 CFM56-3 w/HWFAP 2 20.00 5.00 1 40 85.2 89.2 98.6 3 BOEING B-737-300 139.50 121.00 CFM56-3 w/HWFAP 2 22.00 5.00 1 40 83.9 90.9 98.6 3 BOEING B-737-300 139.50 121.00 CFM56-3-B1 2 20.00 5.00 1 40 87.5 89.9 100.1 3 BOEING B-737-300 139.50 121.00 CFM56-3B-2 2 22.00 4.90 1 40 85.7 91.9 100.1 3 BOEING B-737-400 130.00 121.00 CFM56-3 w/HWFAP 2 20.00 5.00 5 40 83.8 89.8 97.7 3 38 BOEING B-737-400 130.00 121.00 CFM56-3 w/HWFAP 2 22.00 5.00 5 40 82.8 91.2 97.7 3 38 BOEING B-737-400 130.00 121.00 CFM56-3 w/HWFAP 2 22.00 5.00 5 40 82.8 91.2 98.6 3 BOEING B-737-400 130.00 121.00 CFM56-3 w/HWFAP 2 20.00 5.00 5 40 83.8 89.8 98.6 3 BOEING B-737-400 130.00 121.00 CFM56-3 w/HWFAP 2 23.50 5.00 5 40 82.4 92.1 98.6 3 BOEING B-737-400 130.00 121.00 CFM56-3 w/HWFAP 2 23.50 5.00 5 40 82.4 92.1 97.7 3 38 BOEING B-737-400 138.50 121.00 CFM56-3-B1 2 20.00 5.00 5 40 87.2 90.0 100.2 3 BOEING B-737-400 142.50 121.00 CFM56-3-B1 2 20.00 5.00 5 40 88.9 89.6 100.2 3 BOEING B-737-400 138.50 121.00 CFM56-3B-2 2 22.00 4.90 5 40 85.7 92.1 100.2 3 BOEING B-737-400 138.50 121.00 CFM56-3C-1 2 23.50 5.00 5 40 85.0 93.2 100.2 3 BOEING B-737-400 150.00 124.00 CFM56-3 w/HWFAP 2 23.50 5.00 5 40 85.9 91.8 97.7 3 38 Page 11 ### Page 208 APPENDIX 3 ***STAGE 3*** TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-737-400 150.00 124.00 CFM56-3 w/HWFAP 2 22.00 5.00 5 40 86.3 90.7 98.6 3 BOEING B-737-400 150.00 124.00 CFM56-3 w/HWFAP 2 22.00 5.00 5 40 86.3 90.7 97.7 3 38 BOEING B-737-400 142.50 124.00 CFM56-3 w/HWFAP 2 20.00 5.00 5 40 86.9 88.9 97.7 3 38 BOEING B-737-400 142.50 124.00 CFM56-3 w/HWFAP 2 20.00 5.00 5 40 86.9 88.9 98.6 3 BOEING B-737-400 150.00 124.00 CFM56-3 w/HWFAP 2 23.50 5.00 5 40 85.9 91.8 98.6 3 BOEING B-737-400 150.00 124.00 CFM56-3B-2 2 22.00 4.90 5 40 87.7 91.7 100.2 3 BOEING B-737-400 150.00 124.00 CFM56-3C-1 2 23.50 4.90 5 40 87.1 93.1 100.2 3 BOEING B-737-500 108.00 105.00 CFM56-3 w/HWFAP 2 18.50 5.00 5 40 81.0 89.3 97.2 3 38 BOEING B-737-500 108.00 105.00 CFM56-3 w/HWFAP 2 18.50 5.00 5 40 81.0 89.3 98.4 3 BOEING B-737-500 108.00 105.00 CFM56-3 w/HWFAP 2 20.00 5.00 5 40 80.4 90.2 98.4 3 BOEING B-737-500 108.00 105.00 CFM56-3 w/HWFAP 2 20.00 5.00 5 40 80.4 90.2 97.2 3 38 BOEING B-737-500 115.50 105.00 CFM56-3-B1 2 20.00 5.00 5 40 82.7 90.8 99.4 3 BOEING B-737-500 115.50 105.00 CFM56-3-B1(R) 2 18.50 5.00 5 40 83.6 89.9 99.4 3 BOEING B-737-500 132.80 114.00 CFM56-3 w/HWFAP 2 20.00 5.00 5 40 85.4 88.2 98.7 3 BOEING B-737-500 139.00 114.00 CFM56-3 w/HWFAP 2 20.00 5.00 5 40 85.4 89.2 97.6 3 38 BOEING B-737-500 139.00 114.00 CFM56-3 w/HWFAP 2 20.00 5.00 5 40 85.4 89.2 98.7 3 BOEING B-737-500 132.80 114.00 CFM56-3 w/HWFAP 2 18.50 5.00 5 40 85.4 88.2 97.6 3 38 BOEING B-737-500 139.00 114.00 CFM56-3-B1 2 20.00 5.00 5 40 87.3 90.0 100.0 3 Page 12 ### Page 209 **APPENDIX 3** MANUFACTURER BOEING MODEL B-737-500 ***STAGE 3*** TURBOJET POWERED AIRPLANES 1000# 1000# ENGINE MODEL NO. **MTOW MLW** 132.80 114.00 CFM56-3-B1(R) 2 THRUST 1000# BPR **18.50 5.00 TO AP FLAPS 5 40** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) **87.7 88.9 100.0 3 BOEING BOEING BOEING B-737-600 B-737-600 B-737-600** 143.50 120.50 124.00 120.50 143.50 120.50 CFM56-7B/2 DAC (B18 derate) CFM56-7B/2 DAC (B18 derate) CFM56-7B18 2 2 2 19.50 19.50 19.50 5.60 5.60 5.60 1 1 1 40 40 40 85.2 82.0 85.7 88.7 89.7 89.3 95.8 95.8 95.5 3 3 3 50 50 BOEING B-737-600 124.00 120.50 CFM56-7B18 2 19.50 5.60 1 40 82.6 90.3 95.5 3 BOEING B-737-600 124.00 120.50 CFM56-7B20 2 20.60 5.60 1 40 81.9 91.3 95.5 3 BOEING B-737-600 143.50 120.50 CFM56-7B20 2 20.60 5.60 1 40 85.4 90.7 95.5 3 BOEING B-737-600 143.50 120.50 CFM56-7B20/2 DAC 2 20.60 5.60 1 40 84.9 90.0 95.8 3 50 BOEING B-737-600 124.00 120.50 CFM56-7B20/2 DAC 2 20.60 5.60 1 40 81.3 90.7 95.8 3 50 BOEING B-737-600 143.50 120.50 CFM56-7B22 2 22.70 5.40 1 40 84.4 92.3 95.5 3 BOEING B-737-600 124.00 120.50 CFM56-7B22 2 22.70 5.40 1 40 80.9 92.9 95.5 3 BOEING B-737-600 124.00 120.50 CFM56-7B22/2 DAC 2 22.70 5.40 1 40 80.2 92.2 95.8 3 50 BOEING B-737-600 143.50 120.50 CFM56-7B22/2 DAC 2 22.70 5.40 1 40 83.7 91.6 95.8 3 50 BOEING B-737-700 133.00 128.00 CFM56-7B20 2 20.60 5.60 1 40 83.8 90.9 95.8 3 BOEING B-737-700 133.00 128.00 CFM56-7B20/2 DAC 2 20.60 5.60 1 40 83.0 90.3 96.1 3 50 BOEING B-737-700 133.00 128.00 CFM56-7B22 2 22.70 5.40 1 40 82.6 92.5 95.8 3 BOEING B-737-700 133.00 128.00 CFM56-7B22/2 DAC 2 22.70 5.40 1 40 81.8 91.8 96.1 3 50 BOEING B-737-700 133.00 128.00 CFM56-7B24 2 24.20 5.30 1 40 82.1 93.6 95.8 3 Page 13 ### Page 210 APPENDIX 3 ***STAGE 3*** TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-737-700 133.00 128.00 CFM56-7B24/2 DAC 2 24.20 5.30 1 40 81.1 93.0 96.1 3 50 BOEING B-737-700 133.00 128.00 CFM56-7B26 2 26.30 5.10 1 40 81.4 95.4 95.8 3 BOEING B-737-700 133.00 128.00 CFM56-7B26/2 DAC 2 26.30 5.10 1 40 80.3 94.7 96.1 3 50 BOEING B-737-700 154.50 129.20 CFM56-7B20 2 20.60 5.60 1 40 87.1 89.8 95.9 3 BOEING B-737-700 154.50 129.20 CFM56-7B20/2 DAC 2 20.60 5.60 1 40 86.4 89.2 96.2 3 50 BOEING B-737-700 154.50 129.20 CFM56-7B22 2 22.70 5.40 1 40 86.3 91.9 95.9 3 BOEING B-737-700 154.50 129.20 CFM56-7B22/2 DAC 2 22.70 5.40 1 40 85.6 91.2 96.2 3 50 BOEING B-737-700 154.50 129.20 CFM56-7B24 2 24.20 5.30 1 40 85.9 93.0 95.9 3 BOEING B-737-700 154.50 129.20 CFM56-7B24/2 DAC 2 24.20 5.30 1 40 84.7 92.3 96.2 3 50 BOEING B-737-700 154.50 129.20 CFM56-7B26 2 26.30 5.10 1 40 84.6 94.7 95.9 3 BOEING B-737-700 154.50 129.20 CFM56-7B26/2 DAC 2 26.30 5.10 1 40 83.8 94.0 96.2 3 50 BOEING B-737-700 IGW/-700C 159.00 134.00 CFM56-7B24 2 24.20 5.30 1 40 86.6 92.9 96.1 3 51 BOEING B-737-700 IGW/-700C 171.00 134.00 CFM56-7B24 2 24.20 5.30 1 40 88.6 92.5 96.1 3 51 BOEING B-737-700 IGW/-700C/BBJ 159.00 134.00 CFM56-7B26; -7B26/B1 2 26.30 5.10 1 40 85.2 94.6 96.1 3 51 BOEING B-737-700 IGW/-700C/BBJ 171.00 134.00 CFM56-7B26; -7B26/B1 2 26.30 5.10 1 40 87.1 94.3 96.1 3 51 BOEING B-737-700 IGW/BBJ 171.00 134.00 CFM56-7B27/B3 2 27.30 5.10 1 40 86.6 95.2 96.1 3 51 BOEING B-737-700 IGW/BBJ 159.00 134.00 CFM56-7B27/B3 2 27.30 5.10 1 40 84.8 95.5 96.1 3 51 BOEING B-737-800 155.50 144.00 CFM56-7B24 2 24.20 5.30 1 40 85.5 92.5 96.4 3 Page 14 ### Page 211 APPENDIX 3 ***STAGE 3*** TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-737-800 155.50 144.00 CFM56-7B24/2 DAC 2 24.20 5.30 1 40 84.7 91.8 96.7 3 50 BOEING B-737-800 155.50 144.00 CFM56-7B26/2 DAC 2 26.30 5.10 1 40 83.7 93.5 96.7 3 50 BOEING B-737-800 155.50 144.00 CFM56-7B27/2 DAC 2 27.30 5.10 1 40 83.2 94.4 96.7 3 50 BOEING B-737-800 155.50 144.00 CFM56-7B27/2B1 DAC 2 27.30 5.10 1 40 83.1 94.7 96.7 3 50 BOEING B-737-800 174.20 146.30 CFM56-7B24 2 24.20 5.30 1 40 88.6 92.1 96.5 3 BOEING B-737-800 174.20 146.30 CFM56-7B24/2 DAC 2 24.20 5.30 1 40 87.8 91.4 96.8 3 50 BOEING B-737-800 174.20 146.30 CFM56-7B26/2 DAC 2 26.30 5.10 1 40 86.7 93.1 96.8 3 50 BOEING B-737-800 174.20 146.30 CFM56-7B27/2 DAC 2 27.30 5.10 1 40 86.1 93.9 96.8 3 50 BOEING B-737-800 174.20 146.30 CFM56-7B27/2B1 DAC 2 27.30 5.10 1 40 85.9 94.3 96.8 3 50 BOEING B-737-800/BBJ 2 155.50 144.00 CFM56-7B26; -7B26/B1 2 26.30 5.10 1 40 84.4 94.2 96.4 3 BOEING B-737-800/BBJ 2 155.50 144.00 CFM56-7B27/B1; -7B27/B2 2 27.30 5.10 1 40 84.0 95.5 96.4 3 BOEING B-737-800/BBJ 2 155.50 144.00 CFM56-7B27; -7B27/B3 2 27.30 5.10 1 40 84.1 95.2 96.4 3 BOEING B-737-800/BBJ 2 174.20 146.30 CFM56-7B26; -7B26/B1 2 26.30 5.10 1 40 87.4 93.8 96.5 3 BOEING B-737-800/BBJ 2 174.20 146.30 CFM56-7B27/B1; -7B27/B2 2 27.30 5.10 1 40 86.8 95.0 96.5 3 BOEING B-737-800/BBJ 2 174.20 146.30 CFM56-7B27; -7B27/B3 2 27.30 5.10 1 40 87.0 94.7 96.5 3 BOEING B-737-800W 155.50 144.00 CFM56-7B24 2 24.20 5.30 1 40 84.5 92.5 96.3 3 52 BOEING B-737-800W 155.50 144.00 CFM56-7B24/2 DAC 2 24.20 5.30 1 40 83.8 91.8 96.5 3 50,52 BOEING B-737-800W 155.50 144.00 CFM56-7B26/2 DAC 2 26.30 5.10 1 40 82.7 93.5 96.5 3 50,52 Page 15 ### Page 212 APPENDIX 3 ***STAGE 3*** TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-737-800W 155.50 144.00 CFM56-7B27/2 DAC 2 27.30 5.10 1 40 82.3 94.4 96.5 3 50,52 BOEING B-737-800W 155.50 144.00 CFM56-7B27/2B1 DAC 2 27.30 5.10 1 40 82.2 94.7 96.5 3 50,52 BOEING B-737-800W 174.20 146.30 CFM56-7B24 2 24.20 5.30 1 40 87.5 92.1 96.3 3 52 BOEING B-737-800W 174.20 146.30 CFM56-7B24/2 DAC 2 24.20 5.30 1 40 86.9 91.4 96.6 3 50,52 BOEING B-737-800W 174.20 146.30 CFM56-7B26/2 DAC 2 26.30 5.10 1 40 85.6 93.1 96.6 3 50,52 BOEING B-737-800W 174.20 146.30 CFM56-7B27/2 DAC 2 27.30 5.10 1 40 85.1 93.9 96.6 3 50,52 BOEING B-737-800W 174.20 146.30 CFM56-7B27/2B1 DAC 2 27.30 5.10 1 40 85.0 94.3 96.6 3 50,52 BOEING B-737-800W/BBJ 2 155.50 144.00 CFM56-7B26; -7B26/B1 2 26.30 5.10 1 40 83.5 94.2 96.3 3 52 BOEING B-737-800W/BBJ 2 155.50 144.00 CFM56-7B27/B1; -7B27/B2 2 27.30 5.10 1 40 83.0 95.5 96.3 3 52 BOEING B-737-800W/BBJ 2 155.50 144.00 CFM56-7B27; -7B27/B3 2 27.30 5.10 1 40 83.2 95.1 96.3 3 52 BOEING B-737-800W/BBJ 2 174.20 146.30 CFM56-7B26; -7B26/B1 2 26.30 5.10 1 40 86.4 93.8 96.3 3 52 BOEING B-737-800W/BBJ 2 174.20 146.30 CFM56-7B27/B1; -7B27/B2 2 27.30 5.10 1 40 85.8 95.0 96.3 3 52 BOEING B-737-800W/BBJ 2 174.20 146.30 CFM56-7B27; -7B27/B3 2 27.30 5.10 1 40 86.0 94.7 96.3 3 52 BOEING B-737-900 164.00 146.30 CFM56-7B24 2 24.20 5.30 1 40 86.6 92.0 96.4 3 BOEING B-737-900 164.00 146.30 CFM56-7B26 2 26.30 5.10 1 40 85.5 93.7 96.4 3 BOEING B-737-900 164.00 146.30 CFM56-7B27 2 27.30 5.10 1 40 85.1 94.5 96.4 3 BOEING B-737-900 164.00 146.30 CFM56-7B27/B1 2 27.30 5.10 1 40 85.0 95.0 96.4 3 BOEING B-737-900 174.20 147.30 CFM56-7B24 2 24.20 5.30 1 40 88.4 91.8 96.4 3 Page 16 ### Page 213 APPENDIX 3 ***STAGE 3*** TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-737-900 174.20 147.30 CFM56-7B26 2 26.30 5.10 1 40 87.2 93.5 96.4 3 BOEING B-737-900 174.20 147.30 CFM56-7B27 2 27.30 5.10 1 40 86.7 94.2 96.4 3 BOEING B-737-900 174.20 147.30 CFM56-7B27/B1 2 27.30 5.10 1 40 86.6 94.7 96.4 3 BOEING B-747-100 710.00 400.00 JT9D-3A 4 43.60 5.10 10 30 105.4 102.1 104.6 3 29 BOEING B-747-100 750.00 400.00 JT9D-7F 4 48.00 5.10 10 30 104.5 103.5 104.5 3 29 BOEING B-747-100 734.00 425.00 JT9D-7 4 46.30 5.10 10 30 105.1 102.7 104.6 3 29 BOEING B-747-100 734.00 460.00 JT9D-7A 4 47.00 5.10 10 30 104.3 102.6 105.3 3 29 BOEING B-747-100 750.00 520.00 JT9D-7F 4 48.00 5.10 10 25 104.5 103.5 104.5 3 29 BOEING B-747-100 710.00 540.00 JT9D-3A 4 43.60 5.10 10 25 105.4 102.1 104.6 3 29 BOEING B-747-100 734.00 540.00 JT9D-7 4 46.30 5.10 10 25 105.1 102.7 104.1 3 29 BOEING B-747-100 734.00 630.00 JT9D-7A 4 47.00 5.10 10 25 104.3 102.6 105.5 3 29 BOEING B-747-200 770.00 475.00 JT9D-7J 4 50.00 5.10 10 30 103.6 103.0 105.9 3 30 BOEING B-747-200 710.00 520.00 JT9D-3A 4 43.60 5.10 10 30 104.4 100.8 106.9 3 30 BOEING B-747-200 750.00 520.00 JT9D-7F 4 48.00 5.10 10 30 103.5 102.0 106.9 3 30 BOEING B-747-200 734.00 540.00 JT9D-7 4 46.30 5.10 10 30 104.2 101.3 106.7 3 30 BOEING B-747-200 734.00 564.00 JT9D-7A 4 47.00 5.10 10 30 103.5 101.2 106.9 3 30 BOEING B-747-200 775.00 585.00 CF6-50E 4 52.50 4.10 10 30 100.7 101.1 105.9 3 BOEING B-747-200 833.00 585.00 RB211-524C2 4 51.60 4.50 10 30 106.5 99.7 107.0 3 * Page 17 ### Page 214 APPENDIX 3 ***STAGE 3*** TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-747-200 833.00 600.00 JT9D-7Q 4 53.00 4.90 10 30 103.2 103.5 106.6 3 BOEING B-747-200 820.00 630.00 CF6-50E 4 52.50 4.10 10 30 102.5 100.9 107.0 3 BOEING B-747-200 820.00 630.00 CF6-50E2 4 52.50 4.10 10 30 102.1 101.7 106.5 3 BOEING B-747-200 833.00 630.00 CF6-50E2 4 52.50 4.10 10 30 102.6 101.7 106.5 3 BOEING B-747-200 710.00 630.00 JT9D-3A 4 43.60 5.10 10 25 104.4 100.8 105.7 3 30 BOEING B-747-200 734.00 630.00 JT9D-7 4 46.30 5.10 10 25 104.2 101.3 105.2 3 30 BOEING B-747-200 820.00 630.00 JT9D-70A 4 53.00 4.90 10 30 101.1 98.5 106.0 3 BOEING B-747-200 734.00 630.00 JT9D-7A 4 47.00 5.10 10 25 103.5 101.2 105.0 3 30 BOEING B-747-200 750.00 630.00 JT9D-7F 4 48.00 5.10 10 25 103.5 102.0 106.0 3 30 BOEING B-747-200 770.00 630.00 JT9D-7J 4 50.00 5.10 10 25 103.6 103.0 106.0 3 30 BOEING B-747-200 833.00 630.00 JT9D-7Q 4 53.00 4.90 10 25 103.2 103.5 104.4 3 BOEING B-747-200 833.00 630.00 RB211-524D4 4 53.10 4.20 10 30 103.9 99.7 104.9 3 BOEING B-747-300 600.00 564.00 CF6-80C2B1 4 56.70 5.00 10 30 89.8 99.1 102.5 3 BOEING B-747-300 800.00 630.00 CF6-50E2 4 52.50 4.10 10 30 101.6 101.8 106.5 3 BOEING B-747-300 785.00 630.00 JT9D-7R4G2 4 54.75 4.80 10 30 100.1 101.5 106.6 3 BOEING B-747-300 833.00 630.00 JT9D-7R4G2 4 54.75 4.80 10 30 102.4 101.3 106.6 3 BOEING B-747-300 833.00 666.00 CF6-80C2B1 4 56.70 5.00 10 30 99.0 98.2 105.2 3 BOEING B-747-400 600.00 564.00 CF6-80C2B1F 4 57.90 5.00 10 30 89.6 99.1 101.7 3 Page 18 ### Page 215 APPENDIX 3 ***STAGE 3*** TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-747-400 830.00 564.00 CF6-80C2B5F 4 60.80 5.00 10 30 96.0 100.4 101.7 3 BOEING B-747-400 600.00 564.00 PW4056 4 56.75 4.80 10 30 89.5 100.7 103.1 3 BOEING B-747-400 600.00 564.00 RB211-524G 4 58.00 4.30 10 30 89.1 98.9 102.4 3 BOEING B-747-400 600.00 564.00 RB211-524H 4 60.60 4.10 10 30 88.7 99.7 102.4 3 BOEING B-747-400 875.00 652.00 CF6-80C2B1F 4 57.90 5.00 10 30 99.8 98.2 103.8 3 BOEING B-747-400 870.00 652.00 CF6-80C2B1F 4 60.20 5.20 25 99.7 98.3 101.4 3 BOEING B-747-400 875.00 652.00 CF6-80C2B1F W/N1 MOD 4 57.30 5.00 10 30 99.9 97.9 103.8 3 BOEING B-747-400 875.00 652.00 CF6-80C2B5F 4 60.80 5.00 10 30 97.5 100.3 103.8 3 BOEING B-747-400 870.00 652.00 PW 4056 4 56.75 4.80 10 30 101.5 99.7 104.7 3 BOEING B-747-400 875.00 652.00 PW4056 4 56.75 4.80 10 30 101.6 99.7 104.7 3 BOEING B-747-400 875.00 652.00 PW4056 PH3 (FB2B) 4 56.80 4.80 10 30 99.7 98.6 103.6 3 BOEING B-747-400 875.00 652.00 PW4056 PH3 (FB2C) 4 56.80 4.80 10 30 98.6 98.4 103.0 3 BOEING B-747-400 875.00 652.00 PW4056 PH3 (FB2C) NR 4 56.80 4.80 10 30 97.4 98.1 102.1 3 BOEING B-747-400 875.00 652.00 PW4056 PKG B/PHASE I 4 56.80 4.80 10 30 99.3 98.5 103.4 3 BOEING B-747-400 875.00 652.00 RB211-524G 4 58.00 4.30 10 30 99.2 98.0 103.8 3 BOEING B-747-400 870.00 652.00 RB211-524H 4 60.60 4.10 10 30 97.8 98.8 103.8 3 BOEING B-747-400 875.00 652.00 RB211-524H2 4 58.00 4.10 10 30 98.0 98.8 103.8 3 BOEING B-747-SP 702.00 410.00 RB211-524D4 4 53.10 4.20 10 30 99.2 99.8 107.0 3 Page 19 ### Page 216 APPENDIX 3 ***STAGE 3*** TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-747-SP 660.00 450.00 JT9D-7A 4 47.00 5.10 10 30 99.6 101.3 102.5 3 BOEING B-747-SP 702.00 450.00 JT9D-7J 4 50.00 5.10 10 30 100.1 103.3 103.2 3 BOEING B-747-SP 696.00 450.00 RB211-524B2 4 50.10 4.30 10 30 99.5 99.8 103.2 3 BOEING B-747-SP 701.00 465.00 JT9D-7A 4 47.00 5.10 10 30 102.0 101.1 102.9 3 BOEING B-747-SP 660.00 475.00 JT9D-7F 4 48.00 5.10 10 30 98.7 102.3 103.8 3 BOEING B-747-SP 696.00 475.00 JT9D-7J 4 50.00 5.10 10 30 99.8 103.5 103.8 3 BOEING B-747-SP 702.00 475.00 JT9D-7J 4 50.00 5.10 10 30 100.1 103.3 103.8 3 BOEING B-747-SR 571.00 564.00 CF6-45A2 4 46.50 4.10 10 30 98.4 93.2 105.4 3 BOEING B-747-SR 610.00 564.00 JT9D-7A 4 47.00 5.10 10 30 101.8 101.6 106.9 3 * BOEING B-757-200 187.00 198.00 PW 2037 2 37.00 5 30 81.5 94.3 97.7 3 BOEING B-757-200 220.00 198.00 PW 2037 2 38.20 5.80 5 30 86.2 94.0 97.7 3 BOEING B-757-200 187.00 198.00 PW 2037QFC 2 37.00 5 30 80.1 93.7 97.0 3 59 BOEING B-757-200 220.00 198.00 PW 2040 2 41.70 5.70 5 30 84.6 94.5 97.7 3 BOEING B-757-200 190.00 198.00 PW 2040QFC 2 40.00 5 30 79.4 95.1 97.0 3 59 BOEING B-757-200 220.00 198.00 RB211-535C 2 37.40 4.50 5 30 85.5 94.0 100.3 3 BOEING B-757-200 220.00 198.00 RB211-535-E4 2 40.10 4.10 5 30 82.2 93.3 95.0 3 BOEING B-757-200 220.00 198.00 RB211-535-E4 2 40.10 4.10 5 30 82.9 93.4 95.0 3 58 BOEING B-757-200 220.00 198.00 RB211-535E4-B 2 43.10 4.10 5 30 82.1 94.2 95.0 3 58 Page 20 ### Page 217 APPENDIX 3 ***STAGE 3*** TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-757-200 220.00 198.00 RB211-535E4-B 2 43.10 4.10 5 30 81.3 94.4 95.0 3 BOEING B-757-200 255.50 210.00 PW 2037 2 38.20 5.80 5 30 91.4 93.7 98.1 3 BOEING B-757-200 255.50 210.00 PW 2037QFC 2 37.00 5 30 89.7 92.7 97.3 3 59 BOEING B-757-200 255.50 210.00 PW 2040 2 41.70 5.70 5 30 89.7 94.2 98.1 3 BOEING B-757-200 255.50 210.00 PW 2040QFC 2 40.00 5 30 88.1 94.0 97.3 3 59 BOEING B-757-200 240.00 210.00 RB211-535C 2 37.40 4.50 5 25 88.1 93.8 99.6 3 BOEING B-757-200 255.50 210.00 RB211-535-E4 2 40.10 4.10 5 30 86.8 93.0 95.2 3 BOEING B-757-200 255.50 210.00 RB211-535-E4 2 40.10 4.10 5 30 87.3 93.0 95.2 3 58 BOEING B-757-200 255.50 210.00 RB211-535E4-B 2 43.10 4.10 5 30 86.2 93.8 95.2 3 58 BOEING B-757-200 255.50 210.00 RB211-535E4-B 2 43.10 4.10 5 30 85.7 94.1 95.2 3 BOEING B-757-300 236.00 210.00 RB211-535-E4 2 40.10 4.10 5 30 84.8 93.9 95.2 3 58 BOEING B-757-300 235.87 210.00 RB211-535E4-B 2 43.10 4.10 5 30 84.0 95.2 95.2 3 58 BOEING B-757-300 235.87 210.00 RB211-535E4-C 2 43.00 5 30 84.0 95.2 95.2 3 58 BOEING B-757-300 275.00 224.00 RB211-535-E4 2 40.10 4.10 5 30 89.8 93.5 95.4 3 58 BOEING B-757-300 275.00 224.00 RB211-535E4-B 2 43.10 4.10 5 30 88.4 94.8 95.4 3 58 BOEING B-757-300 275.00 224.00 RB211-535E4-C 2 43.00 5 30 88.4 94.8 95.4 3 58 BOEING B-767-200 279.90 257.00 CF6-80A 2 48.00 4.60 1 30 84.9 95.5 101.4 3 BOEING B-767-200 279.90 257.00 CF6-80A2 2 50.00 4.60 1 30 84.2 97.2 101.4 3 Page 21 ### Page 218 APPENDIX 3 ***STAGE 3*** TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-767-200 282.00 257.00 JT9D-7R4D(A) 2 48.00 5.00 1 30 87.7 95.7 101.8 3 BOEING B-767-200 282.00 257.00 JT9D-7R4D(B) 2 48.00 5.00 1 30 88.4 95.9 101.9 3 BOEING B-767-200 282.00 257.00 JT9D-7R4E 2 50.00 5.00 1 30 87.5 96.8 101.9 3 BOEING B-767-200 300.00 270.00 CF6-80C2-B2 2 52.50 5.00 1 30 85.2 94.1 95.7 3 BOEING B-767-200 351.00 270.00 CF6-80C2-B4 2 57.90 5.00 1 30 87.7 95.3 95.7 3 BOEING B-767-200 335.00 270.00 PW4052 2 52.00 4.80 1 30 89.4 95.0 97.8 3 BOEING B-767-200 340.00 270.00 PW4056 2 56.75 4.80 1 30 88.5 96.0 97.8 3 BOEING B-767-200 351.00 285.00 PW4052 2 52.00 4.80 1 30 90.9 94.9 98.2 3 BOEING B-767-200 360.00 300.00 CF6-80A 2 48.00 4.60 1 30 92.8 94.8 101.7 3 BOEING B-767-200 360.00 300.00 CF6-80A2 2 50.00 4.60 1 30 91.7 96.5 101.7 3 BOEING B-767-200 351.00 300.00 CF6-80C2-B2 2 52.50 5.00 1 30 89.5 93.7 96.4 3 BOEING B-767-200 387.00 300.00 CF6-80C2-B4 2 57.90 5.00 1 30 90.6 95.0 96.4 3 BOEING B-767-200 351.00 300.00 JT9D-7R4D(A) 2 48.00 5.00 1 30 95.1 95.2 102.7 3 BOEING B-767-200 360.00 300.00 JT9D-7R4D(B) 2 48.00 5.00 1 30 96.2 95.3 102.6 3 BOEING B-767-200 360.00 300.00 JT9D-7R4E 2 50.00 5.00 1 30 95.4 96.2 102.6 3 BOEING B-767-200 400.00 300.00 PW 4056 2 56.75 4.80 1 30 93.7 95.5 98.6 3 BOEING B-767-200/200ER 300.00 270.00 CF6-80C2B2F 2 52.50 5.00 1 30 85.1 93.8 95.8 3 BOEING B-767-200/200ER 300.00 270.00 CF6-80C2B4F 2 57.90 5.00 1 30 83.7 95.2 95.8 3 Page 22 ### Page 219 APPENDIX 3 ***STAGE 3*** TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-767-200/200ER 299.60 270.00 PW4056 PH3 (FB2C) NRI 2 56.80 4.80 1 30 81.8 95.1 95.9 3 BOEING B-767-200/200ER 340.00 270.00 PW4060 2 60.00 4.80 1 30 87.7 97.3 97.8 3 BOEING B-767-200/200ER 299.60 270.00 PW4060 PH3 (FB2C) NRI 2 60.00 4.80 1 30 81.6 96.4 95.9 3 BOEING B-767-200/200ER 360.00 300.00 CF6-80C2B2F 2 52.50 5.00 1 30 90.2 93.4 96.5 3 BOEING B-767-200/200ER 360.00 300.00 CF6-80C2B4F 2 57.90 5.00 1 30 88.5 94.8 96.5 3 BOEING B-767-200/200ER 387.00 300.00 CF6-80C2B4F W/N1 MOD 2 57.90 5.00 1 30 90.6 94.6 96.5 3 BOEING B-767-200/200ER 400.00 300.00 CF6-80C2B6F W/N1 MOD 2 61.50 5.00 1 30 90.5 95.5 96.5 3 BOEING B-767-200/200ER 395.00 300.00 PW4056 PH3 (FB2C) NRI 2 56.80 4.80 1 30 89.8 94.5 96.6 3 BOEING B-767-200/200ER 387.00 300.00 PW4060 2 60.00 4.80 1 30 91.6 96.9 98.6 3 BOEING B-767-200/200ER 395.00 300.00 PW4060 PH3 (FB2C) NRI 2 60.00 4.80 1 30 89.0 95.9 96.6 3 BOEING B-767-300 300.00 280.00 CF6-80A 2 48.00 4.60 5 30 87.5 95.2 101.7 3 BOEING B-767-300 300.00 280.00 CF6-80A2 2 50.00 4.60 5 30 86.7 96.9 101.7 3 BOEING B-767-300 288.70 280.00 CF6-80C2B2 2 52.50 5.00 5 30 83.1 94.3 96.5 3 BOEING B-767-300 380.00 280.00 CF6-80C2-B4 2 57.90 5.00 5 30 90.2 95.3 96.5 3 BOEING B-767-300 380.00 280.00 CF6-80C2-B6 2 61.50 5.00 5 30 89.2 96.4 96.5 3 BOEING B-767-300 380.00 280.00 CF6-80C2B6F 2 61.50 5.00 5 30 89.1 96.1 96.6 3 BOEING B-767-300 300.00 280.00 JT9D-7R4D(B) 2 48.00 5.00 5 30 91.0 95.7 102.3 3 BOEING B-767-300 300.00 280.00 JT9D-7R4E 2 50.00 5.00 5 30 90.0 96.5 102.3 3 Page 23 ### Page 220 APPENDIX 3 ***STAGE 3*** TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-767-300 380.00 280.00 PW 4056 2 56.75 4.80 5 30 92.0 96.0 98.8 3 BOEING B-767-300 380.00 280.00 PW4060 2 60.00 4.80 5 30 91.2 97.2 98.8 3 BOEING B-767-300 340.00 280.00 RB211-524G 2 58.00 4.30 5 30 89.4 94.3 98.5 3 BOEING B-767-300 340.00 280.00 RB211-524H 2 60.60 4.10 5 30 88.7 95.2 98.5 3 BOEING B-767-300 351.00 320.00 CF6-80A 2 48.00 4.60 5 30 92.0 94.9 101.7 3 BOEING B-767-300 351.00 320.00 CF6-80A2 2 50.00 4.60 5 30 91.2 96.5 101.7 3 BOEING B-767-300 407.00 320.00 CF6-80C2-B4 2 57.90 5.00 5 30 92.1 95.2 98.4 3 BOEING B-767-300 407.00 320.00 CF6-80C2-B6 2 61.50 5.00 5 30 91.1 96.3 98.4 3 BOEING B-767-300 407.00 320.00 CF6-80C2B6F 2 61.50 5.00 5 30 90.9 96.0 98.5 3 BOEING B-767-300 351.00 320.00 JT9D-7R4D(B) 2 48.00 5.00 5 30 95.7 95.4 103.0 3 BOEING B-767-300 351.00 320.00 JT9D-7R4E 2 50.00 5.00 5 30 95.0 96.2 103.0 3 BOEING B-767-300 407.00 320.00 PW 4056 2 56.75 4.80 5 30 94.2 95.7 100.2 3 BOEING B-767-300 407.00 320.00 PW 4060 2 60.00 4.80 5 30 93.2 97.0 100.2 3 BOEING B-767-300 407.00 320.00 RB211-524G 2 58.00 4.30 5 30 93.8 94.0 99.8 3 BOEING B-767-300 407.00 320.00 RB211-524H 2 60.60 4.10 5 30 92.9 94.8 99.8 3 BOEING B-767-300/300ER 295.00 280.00 PW4056 PH3 (FB2C) NRI 2 56.80 4.80 5 30 81.9 95.3 96.6 3 BOEING B-767-300/300ER 295.00 280.00 PW4060 PH3 (FB2C) NRI 2 60.00 4.80 5 30 81.5 96.6 96.6 3 BOEING B-767-300/300ER 345.00 280.00 PW4062 PH3 (FB2C) NRI 2 62.00 4.80 5 30 84.6 98.0 96.6 3 Page 24 ### Page 221 APPENDIX 3 ***STAGE 3*** TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-767-300/300ER 412.00 320.00 PW4056 PH3 (FB2C) NRI 2 56.80 4.80 5 30 91.0 94.6 97.6 3 BOEING B-767-300/300ER 412.00 320.00 PW4060 PH3 (FB2C) NRI 2 60.00 4.80 5 30 90.3 95.9 97.9 3 BOEING B-767-300/300ER 412.00 320.00 PW4062 (FB2B) 2 62.00 4.80 5 30 92.2 99.0 100.2 3 BOEING B-767-300/300ER 412.00 320.00 PW4062 PH3 (FB2C) NRI 2 62.00 4.80 5 30 89.9 97.6 97.9 3 BOEING B-767-400 350.00 320.00 CF6-80C2B8F 2 63.50 5.00 5 30 85.5 97.8 97.6 3 BOEING B-767-400 450.00 350.00 CF6-80C2B8F 2 63.50 5.00 5 30 91.2 96.8 98.7 3 BOEING B-777-200 440.90 440.90 PW4074 2 74.00 6.80 5 30 85.2 95.5 98.9 3 BOEING B-777-200 506.00 445.00 GE90-76B 2 76.00 8.40 5 30 86.7 93.3 97.6 3 53 BOEING B-777-200 506.00 445.00 GE90-76B (BLK IV) 2 76.00 8.40 5 30 87.6 94.3 97.9 3 54 BOEING B-777-200 506.00 445.00 GE90-77B 2 77.00 8.30 5 30 86.7 93.4 97.6 3 53 BOEING B-777-200 506.00 445.00 GE90-77B (BLK IV) 2 77.00 8.30 5 30 87.4 94.3 97.9 3 54 BOEING B-777-200 545.00 445.00 GE90-85B 2 85.00 8.30 5 30 87.3 94.4 97.6 3 53 BOEING B-777-200 545.00 445.00 GE90-85B (BLK IV) 2 85.00 8.30 5 30 87.8 95.3 97.9 3 54 BOEING B-777-200 545.00 445.00 GE90-90B 2 90.00 8.20 5 30 86.3 95.4 97.6 3 53 BOEING B-777-200 545.00 445.00 GE90-90B (BLK IV) 2 90.00 8.20 5 30 86.5 96.1 97.9 3 54 BOEING B-777-200 580.00 445.00 GE90-94B (BLK IV) 2 94.00 8.10 5 30 87.5 96.7 97.9 3 54 BOEING B-777-200 535.00 445.00 PW4074 2 74.00 6.80 5 30 90.9 95.1 99.0 3 BOEING B-777-200 445.00 445.00 PW4077 2 77.00 6.60 5 30 84.9 96.2 98.9 3 Page 25 ### Page 222 APPENDIX 3 ***STAGE 3*** TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-777-200 545.00 445.00 PW4090 2 90.00 6.10 5 30 88.3 98.7 98.9 3 55 BOEING B-777-200 535.00 445.00 PW4090 at PW4074 rating 2 74.00 6.80 5 30 90.8 95.2 98.9 3 55 BOEING B-777-200 447.40 445.00 PW4090 at PW4074 rating 2 74.00 6.80 5 30 85.7 95.5 98.9 3 55 BOEING B-777-200 545.00 445.00 PW4090 at PW4077 rating 2 77.00 6.60 5 30 90.6 95.9 98.9 3 55 BOEING B-777-200 447.50 445.00 PW4090 at PW4077 rating 2 77.00 6.60 5 30 85.1 96.3 98.9 3 55 BOEING B-777-200 458.00 445.00 RR TRENT 875 2 75.00 6.30 5 30 87.1 96.1 99.2 3 BOEING B-777-200 458.00 445.00 RR TRENT 877 2 77.00 6.20 5 30 86.7 96.5 99.2 3 BOEING B-777-200 545.00 445.00 RR TRENT 884 2 84.00 6.00 5 30 89.4 97.2 99.2 3 BOEING B-777-200 545.00 445.00 RR TRENT 892 2 90.00 5.90 5 30 88.3 98.1 99.2 3 BOEING B-777-200 632.50 445.00 RR TRENT 895 2 93.40 5.80 5 30 92.4 98.4 99.2 3 BOEING B-777-200 545.00 460.00 GE90-76B 2 76.00 8.40 5 30 88.8 93.2 97.8 3 53 BOEING B-777-200 545.00 460.00 GE90-76B (BLK IV) 2 76.00 8.40 5 30 89.5 94.1 98.1 3 54 BOEING B-777-200 545.00 460.00 GE90-77B 2 77.00 8.30 5 30 88.8 93.3 97.8 3 53 BOEING B-777-200 545.00 460.00 GE90-77B (BLK IV) 2 77.00 8.30 5 30 89.4 94.2 98.1 3 54 BOEING B-777-200 632.50 460.00 GE90-85B 2 85.00 8.30 5 30 91.3 94.2 97.8 3 53 BOEING B-777-200 656.00 460.00 GE90-90B 2 90.00 8.20 5 30 91.3 95.0 97.8 3 53 BOEING B-777-200 545.00 460.00 PW4077 2 77.00 6.60 5 30 90.7 95.8 99.0 3 BOEING B-777-200 632.50 470.00 GE90-85B (BLK IV) 2 85.00 8.30 5 30 92.0 95.0 98.3 3 54 Page 26 ### Page 223 APPENDIX 3 ***STAGE 3*** TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-777-200 656.00 470.00 GE90-90B (BLK IV) 2 90.00 8.20 5 30 91.5 95.7 98.3 3 54 BOEING B-777-200 656.00 470.00 GE90-94B BLK IV) 2 94.00 8.10 5 30 91.1 96.4 98.3 3 54 BOEING B-777-200 656.00 470.00 PW4090 2 90.00 6.10 5 30 93.9 98.2 99.2 3 55 BOEING B-777-200 545.00 470.00 RR TRENT 875 2 75.00 6.30 5 30 92.0 95.8 99.5 3 BOEING B-777-200 555.00 470.00 RR TRENT 877 2 77.00 6.20 5 30 91.7 96.1 99.5 3 BOEING B-777-200 632.50 470.00 RR TRENT 884 2 84.00 6.00 5 30 94.3 96.9 99.5 3 BOEING B-777-200 656.00 470.00 RR TRENT 892 2 90.00 5.90 5 30 94.0 97.7 99.5 3 BOEING B-777-200 656.00 470.00 RR TRENT 895 2 93.40 5.80 5 30 93.4 98.3 99.5 3 BOEING B-777-300 450.00 445.00 PW4090 2 90.00 6.10 5 30 83.4 98.7 99.0 3 55 BOEING B-777-300 550.00 445.00 PW4098 2 98.00 5.80 5 30 87.7 99.3 100.0 3 BOEING B-777-300 550.00 445.00 RR TRENT 884 2 84.00 6.00 5 30 90.1 96.6 99.2 3 BOEING B-777-300 550.00 445.00 RR TRENT 892 2 90.00 5.90 5 30 88.4 97.5 99.2 3 BOEING B-777-300 660.00 524.00 PW4090 2 90.00 6.10 5 30 94.4 97.3 99.9 3 55 BOEING B-777-300 660.00 524.00 PW4098 2 98.00 5.80 5 30 93.1 98.5 101.1 3 BOEING B-777-300 660.00 524.00 RR TRENT 884 2 84.00 6.00 5 30 96.2 95.9 100.4 3 BOEING B-777-300 660.00 524.00 RR TRENT 892 2 90.00 5.90 5 30 94.2 96.9 100.4 3 BOMBARDIER BD-700-1A10 (Global Express) 93.50 78.50 BR700-710-A2-20 2 14.97 5.00 16 30 82.1 88.7 89.8 3 BOMBARDIER BD-700-1A10 (Global Express) 96.00 78.50 BR700-710-A2-20 2 14.97 5.00 16 30 82.7 88.6 89.8 3 Page 27 ### Page 224 APPENDIX 3 ***STAGE 3*** TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOMBARDIER BD700-1A10 (Global Express) 75.00 75.00 Rolls Royce/ BR700-710­ 2 14.97 5.00 16 30 75.6 89.3 89.7 3 (Learjet STC: SA8184NM-D) A2-20 BOMBARDIER CL-600 36.00 33.00 ALF-502 2 7.50 5.00 20 45 81.6 89.3 91.2 3 * BOMBARDIER CL-600 40.40 36.00 ALF 502L/L-2/L-2C 2 7.50 5.00 20 45 84.0 87.2 91.6 3 * BOMBARDIER CL-600 41.25 36.00 ALF-502L/L-2/L-2C 2 7.50 5.00 20 45 84.7 89.5 91.6 3 * BOMBARDIER CL-600 (WINGLETS) 41.25 36.00 ALF-502L/L-2/L-2C 2 7.50 5.00 20 45 84.8 89.5 91.6 3 BOMBARDIER CL-600-2B19 (CRJ) 53.00 47.00 CF-34-3A1 2 9.22 6.00 20 45 79.8 82.2 92.1 3 BOMBARDIER CL-600-2B19 (CRJ) 53.00 47.00 CF-34-3B1 2 9.22 20 45 78.7 82.4 92.1 3 BOMBARDIER CL-600-2C10 (CRJ700) 72.50 66.90 CF34-8C1 2 13.79 6.30 8 45 82.1 89.5 92.6 3 BOMBARDIER CL-600-2C10 (CRJ700) 75.00 66.90 CF34-8C1 2 13.79 6.30 8 45 82.7 89.4 92.6 3 BOMBARDIER CL-601 42.10 36.00 CF34-1A 2 8.65 6.30 20 45 79.4 84.9 89.4 3 * BOMBARDIER CL-601 43.00 36.00 CF34-1A 2 8.65 6.30 20 45 79.9 84.8 89.4 3 * BOMBARDIER CL-601-1A 45.10 36.00 CF-34-1A 2 8.65 6.30 20 45 80.5 84.6 90.1 3 * BOMBARDIER CL-601-3A 43.10 36.00 CF-34-3A 2 8.72 6.30 20 45 79.4 85.9 89.4 3 * BOMBARDIER CL-601-3A 45.10 36.00 CF-34-3A/-3A2 2 8.65 6.30 20 45 79.8 85.7 90.1 3 * BOMBARDIER CL-601-3R 45.10 36.00 CF-34-3A1 2 9.22 6.00 20 45 79.8 85.7 90.1 3 * BOMBARDIER CL-604 47.60 38.00 GE CF34-3B 2 8.72 6.30 20 45 80.9 86.2 90.3 3 * BOMBARDIER CL-604 48.20 38.00 GE CF34-3B 2 8.72 6.30 20 45 81.2 86.2 90.3 3 * CESSNA 500 CITATION 10.30 9.90 JT15D-1 2 2.20 3.30 15 40 76.4 86.1 87.7 3 * Page 28 ### Page 225 APPENDIX 3 ***STAGE 3*** TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES CESSNA 500/501 CITATION I 11.80 11.30 JT15D-1/-1A 2 2.20 3.30 15 40 78.0 86.2 87.9 3 * CESSNA 525 CESSNA JET 10.40 9.70 FJ44-1A 2 1.50 15 35 73.4 83.7 92.1 3 CESSNA 525A CITATION JET II (CJ-2) 12.37 11.50 FJ44-2C 2 2.10 15 35 74.5 88.8 91.4 3 CESSNA 550 CITATION II 13.30 12.70 JT15D-4 2 2.50 2.68 15 40 80.1 86.7 90.5 3 * CESSNA 550 CITATION Bravo 14.80 13.50 PW530A 2 2.20 15 40 73.7 85.2 91.2 3 CESSNA 550 CITATION II 14.10 13.50 JT15D-4 2 2.50 2.68 0 40 71.6 86.4 90.5 3 CESSNA 551 CITATION II 12.50 12.00 JT15D-4 2 2.50 2.68 15 40 80.1 86.7 90.5 3 * CESSNA 552 15.50 14.30 JT15D-5 2 2.90 2.10 20 35 89.3 94.7 88.5 3 * CESSNA 560 CITATION Ultra 16.30 15.20 JT15D-5D 2 2.30 7 35 82.9 95.9 85.7 3 CESSNA 560 CITATION V 16.30 15.20 JT15D-5A 2 2.90 2.10 7 35 84.6 94.6 88.9 3 CESSNA 560 CITATION V 15.90 15.20 JT15D-5A 2 2.90 2.10 7 35 83.7 94.7 88.9 3 CESSNA 560 ENCORE 16.63 15.20 PW535A 2 2.90 7 35 70.3 89.9 90.5 3 CESSNA 560XL EXCEL 20.00 18.70 PW545A 2 3.00 7 35 72.4 85.3 93.1 3 CESSNA 650 CITATION III 21.00 17.00 TFE731-3B-100S 2 2.90 3.11 20 37 84.9 92.5 92.4 3 CESSNA 650 CITATION III 22.00 20.00 TFE731-3B-100S 2 2.90 3.11 7 37 80.1 92.4 93.8 3 22 CESSNA 650 CITATION VI 22.45 20.00 TFE731-3C-100S 2 2.90 7 40 82.2 92.4 93.8 3 CESSNA 650 CITATION VII 23.00 20.00 TFE731-4R-3S 2 3.20 7 40 78.9 91.9 90.8 3 CESSNA 750 CITATION X 35.70 31.80 AE3007C 2 5.00 5.30 15 35 72.3 83.0 90.2 3 Page 29 ### Page 226 APPENDIX 3 ***STAGE 3*** TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES CESSNA S550 CITATION S/II 14.70 14.00 JT15D-4B 2 2.50 2.68 20 35 87.9 91.6 85.1 3 * CESSNA S550 CITATION S/II 15.10 14.40 JT15D-4B 2 2.50 2.68 7 35 80.0 91.3 86.2 3 DASSAULT FALCON 10 19.30 17.64 TFE731-2-1C 2 3.23 2.80 15 52 82.2 86.2 95.2 3 DASSAULT FALCON 200 32.00 27.60 ATF3-6A-4C 2 5.20 2.90 5 40 83.9 89.0 93.9 3 DASSAULT FALCON 200 (M5634) 32.00 28.88 ATF3-6A-4C 2 5.20 2.90 5 40 83.9 89.0 94.2 3 DASSAULT FALCON 2000 36.50 33.00 CFE738-1-1B 2 5.72 6.00 20 40 79.4 86.4 93.1 3 DASSAULT FALCON 20-Basic/D/E/F 28.66 27.32 CF700-2D-2Q 2 4.50 2.00 0 40 81.9 94.0 99.7 3 (M2851) DASSAULT FALCON 20-C5/D5/E5 (M3500) 29.10 27.73 TFE731-5AR-2C 2 4.50 3.70 15 40 82.9 88.4 90.7 3 DASSAULT FALCON 20-C5/D5/E5 (M3530) 29.10 27.73 TFE-731-5BR-2C 2 4.80 3.70 15 40 80.3 90.7 90.7 3 DASSAULT FALCON 20-C5/D5/E5 (M3547) 30.50 28.88 TFE731-5BR-2C 2 4.80 3.70 15 40 82.9 91.9 90.6 3 DASSAULT FALCON 20-F5 (M3500) 29.10 27.73 TFE731-5AR-2C 2 4.50 3.70 10 40 81.8 88.6 90.0 3 DASSAULT FALCON 20-F5 (M3530) 29.10 27.73 TFE-731-5BR-2C 2 4.80 3.70 10 40 79.3 90.9 90.0 3 DASSAULT FALCON 20-F5 (M3547) 30.50 28.88 TFE731-5BR-2C 2 4.80 3.70 10 40 81.9 92.1 90.3 3 DASSAULT FALCON 20-G (M2500) 32.00 27.56 ATF3-6-2C 2 5.40 2.90 10 40 87.5 88.3 95.9 3 DASSAULT FALCON 50 38.80 35.72 TFE731-3-1C 3 3.70 2.80 20 48 84.3 91.6 97.4 3 DASSAULT FALCON 50 ( M1810) 40.79 35.72 TFE731-40-1 3 3.70 3.50 20 48 83.0 92.7 95.2 3 DASSAULT FALCON 50 (M1230) 40.78 35.71 TFE731-3-1C 3 3.70 2.80 20 48 84.8 91.5 97.1 3 DASSAULT FALCON 50 (M2193) 40.79 35.72 TFE731-40-1 3 3.70 3.50 20 48 83.8 92.0 95.2 3 Page 30 ### Page 227 APPENDIX 3 ***STAGE 3*** TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES DASSAULT FALCON 900 45.50 42.00 TFE731-5AR-1C 3 4.75 3.70 20 40 81.9 89.5 91.7 3 DASSAULT FALCON 900 (M1196) 46.50 42.00 TFE731-5AR-1C 3 4.75 3.70 20 40 82.9 89.5 91.7 3 DASSAULT FALCON 900B (M1200) 46.50 42.00 TFE731-5BR-1C 3 4.75 3.70 20 40 80.7 91.2 91.7 3 DASSAULT FALCON 900EX (M3000) 49.00 44.50 TFE731-60-1 3 5.00 4.40 20 40 79.8 90.5 92.3 3 EMBRAER EMB-135LR 44.09 40.78 AE3007A1/3 2 7.20 4.77 9 45 77.9 84.4 92.3 3 EMBRAER EMB-145EP 46.29 41.22 AE3007A 2 7.58 5.23 9 45 83.7 84.2 92.6 3 * EMBRAER EMB-145ER 45.41 41.22 AE3007A 2 7.58 5.23 9 45 77.9 84.6 92.6 3 EMBRAER EMB-145LR 48.50 42.54 AE3007A1/1 2 7.58 4.76 9 45 79.4 84.6 92.5 3 FAIRCHILD DORNIER DORNIER 328-300 33.51 31.06 PW306B 2 6.05 5.60 12 32 76.1 89.8 91.1 3 FAIRCHILD DORNIER DORNIER 328-300 Mod 10 34.52 31.72 PW306B 2 6.05 5.60 12 32 76.5 89.8 92.1 3 FOKKER F100 98.00 88.00 TAY MK650-15 2 14.73 3.00 0 42 81.8 91.7 93.0 3 FOKKER F70 81.00 75.00 TAY MK620-15 2 13.80 3.00 0 42 76.8 89.9 87.7 3 FOKKER F70 92.00 81.00 TAY MK620-15 2 13.80 3.00 0 42 80.1 89.5 88.3 3 GULFSTREAM G100 24.65 20.70 TFE731-40R-200G 2 4.25 2.90 25 40 79.1 89.5 91.9 3 GULFSTREAM G200 34.85 28.00 PW306A 2 6.04 4.50 25 40 81.4 85.8 90.9 3 47 GULFSTREAM G200 34.85 28.00 PW306A 2 6.04 4.50 25 40 81.4 85.8 92.7 3 46 GULFSTREAM G-IV 73.20 58.50 TAY 611-8 2 13.85 3.00 10 39 76.8 87.3 91.0 3 GULFSTREAM G-IV GULFSTREAM w/ASC 190 74.60 66.00 TAY 611-8 2 13.85 3.00 20 39 77.5 86.6 92.0 3 Page 31 ### Page 228 APPENDIX 3 ***STAGE 3*** TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES GULFSTREAM G-V 90.50 75.30 BR700-710A1-10 2 14.70 4.20 10 39 80.3 89.1 90.8 3 ISRAEL AIRCRAFT 1124 WESTWIND 22.90 19.00 TFE731-3-1G 2 3.70 2.80 20 40 81.2 88.4 93.0 3 ISRAEL AIRCRAFT 1124A WESTWIND 2 23.50 19.00 TFE731-3-1G 2 3.70 2.80 20 40 85.4 88.7 92.8 3 * ISRAEL AIRCRAFT 1125 ASTRA 23.50 20.70 TFE731-3A-200G 2 12 40 82.3 89.8 89.8 3 ISRAEL AIRCRAFT 1125 ASTRA 24.70 20.70 TFE731-3A-200G 2 12 40 84.1 89.7 89.8 3 ISRAEL AIRCRAFT 1125 ASTRA SPX 24.65 20.70 TFE731-40R 2 0 40 79.9 89.9 92.3 3 ISRAEL AIRCRAFT Galaxy 34.85 28.00 PW306A 2 6.04 4.50 0 40 81.4 85.8 92.7 3 LEARJET 31 16.50 15.30 TFE731-2-3B 2 3.50 8 40 81.0 87.0 92.6 3 * LEARJET 31 15.50 15.30 TFE731-2-3B 2 3.50 8 40 79.6 87.2 92.6 3 * LEARJET 31A 17.00 15.30 TFE731-2-3B 2 3.50 8 40 81.9 86.9 92.8 3 LEARJET 31A 17.00 16.00 TFE731-2-3B 2 3.50 8 40 82.9 86.8 93.1 3 LEARJET 35/36 18.00 14.30 TFE731-2-2B 2 3.50 2.64 20 40 84.5 87.9 92.2 3 * LEARJET 35/36 17.00 14.30 TFE731-2-2B 2 3.50 2.64 20 40 84.0 86.9 92.2 3 * LEARJET 35A 18.00 14.30 TFE731-2-2B 2 3.50 2.64 8 40 83.6 87.4 91.3 3 * LEARJET 35A/36A 18.00 14.30 TFE731-2-2B 2 3.50 2.64 8 40 78.7 87.4 91.3 3 LEARJET 35A/36A 18.30 15.30 TFE731-2-2B 2 3.50 2.64 8 40 79.2 86.7 91.4 3 LEARJET 36A 18.30 15.30 TFE731-2-2B 2 3.50 2.64 20 40 83.9 87.8 91.4 3 * LEARJET 20.50 19.20 TFE731-20R-1B or (-20AR­ 2 8 40 74.4 85.2 93.4 3 1B) Page 32 45 ### Page 229 **APPENDIX 3** **MANUFACTURER** LEARJET MODEL 55 1000# MTOW 21.00 ***STAGE 3*** TURBOJET POWERED AIRPLANES 1000# ENGINE MODEL NO. MLW 17.00 TFE731-3A-2B 2 THRUST 1000# BPR **3.70 TO AP FLAPS 8 40** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) 85.5 90.7 90.6 3 * LEARJET 55 19.50 17.00 TFE731-3A-2B 2 3.70 8 40 84.2 90.9 90.6 3 * LEARJET 55B 21.50 18.00 TFE731-3A-2B 2 3.70 20 40 86.3 90.7 91.0 3 * LEARJET 55C 21.50 17.00 TFE731-3AR-3B 2 3.90 2.90 20 40 87.0 91.4 92.4 3 * LEARJET 55C 21.00 17.00 TFE731-3AR-3B 2 3.90 2.90 20 40 86.7 91.5 92.4 3 * LEARJET 55C 21.50 18.00 TFE731-3AR-2B 2 3.90 2.90 20 40 86.7 90.9 92.4 3 * LEARJET 55C 21.00 18.00 TFE731-3AR-2B 2 3.90 2.90 20 40 86.2 91.0 92.4 3 * LEARJET 60 23.50 19.50 PW305A 2 4.67 8 40 70.8 83.2 87.7 3 LEARJET 60 23.10 19.50 PW305A 2 4.67 8 40 70.8 83.1 87.7 3 **LOCKHEED** **LOCKHEED** LOCKHEED 1329-23A/D/E (STAR 3 STC ST00258SE) 1329-25 (STAR 3 STC# ST00259SE) L-1011 44.25 36.00 44.50 36.00 **430.00 358.00 TFE731-3-1R TFE731-3-1R RB211-22B 4 4 3** 3.70 3.70 41.00 2.80 2.80 4.70 20 20 14 59 59 42 85.2 85.4 95.9 90.7 90.7 95.1 96.9 96.9 102.8 3 3 3 5 * LOCKHEED L-1011-1 430.00 358.00 RB211-22B 3 41.00 4.70 10 42 96.0 95.0 102.8 3 5 * LOCKHEED L-1011-100 466.00 368.00 RB211-22B 3 41.00 4.70 10 42 98.5 94.9 102.8 3 5 * LOCKHEED L-1011-200 466.00 368.00 RB211-524B 3 50.00 4.50 10 33 98.1 97.9 101.4 3 5 * LOCKHEED L1011-385-1-14/15 474.00 368.00 RB211-22B 3 41.00 4.70 4 42 98.6 94.1 102.8 3 LOCKHEED L1011-385-1-14/15 466.00 368.00 RB211-524B4 3 50.00 4.50 10 42 97.9 95.9 103.3 3 * LOCKHEED L-1011-500 496.00 368.00 RB211-524B 3 50.00 4.50 14 33 98.4 97.8 101.5 3 5 * Page 33 ### Page 230 APPENDIX 3 ***STAGE 3*** **TURBOJET POWERED AIRPLANES** **MANUFACTURER** LOCKHEED MODEL L-1011-500 1000# MTOW 496.00 1000# MLW 368.00 **ENGINE MODEL RB211-524B3 NO.** 3 THRUST 1000# BPR **50.00 4.50 TO AP FLAPS 14 33** TO SL AP STAGE NOTES NOISE LEVEL (EPNdB) 97.4 96.7 100.3 3 5 * LOCKHEED L-1011-500 504.00 368.00 RB211-524B3 3 50.00 4.50 22 33 98.0 96.9 100.2 3 5 * LOCKHEED L-1011-500 510.00 368.00 RB211-524B4 3 50.00 4.50 10 33 99.3 96.4 102.0 3 * **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS** MCDONNELL DOUGLAS DC-08-61 (BAC II STC: SA4892NM) DC-08-62 (BAC II STC: SA4892NM or SA5455NM) DC-08-62 (BAC II STC: SA4892NM) DC-08-62 (BAC II STC: SA4892NM) DC-08-62 (BAC II STC: SA5455NM) DC-08-63 (BAC II STC: SA4892NM or SA5455NM) DC-08-63 (BAC II STC: SA4892NM or SA5455NM) DC-08-71 325.00 335.00 348.00 335.00 350.00 353.00 353.00 325.00 240.00 250.00 240.00 250.00 240.00 258.00 267.00 **240.00 JT3D-3B JT3D-7 JT3D-3B JT3D-3B JT3D-3B JT3D-7 JT3D-7 CFM56-2-C1 4 4 4 4 4 4 4 4** 18.00 19.00 18.00 18.00 18.00 19.00 19.00 22.00 1.40 1.40 1.40 1.40 1.40 1.40 1.40 6.00 15 12 12 12 12 12 12 15 35 35 35 35 35 35 35 50 99.8 97.8 100.5 99.7 100.5 98.9 98.9 94.3 101.0 101.3 101.2 101.3 101.2 101.4 101.4 92.9 101.6 102.2 100.7 101.0 100.2 102.4 102.7 98.3 3 3 3 3 3 3 3 3 12 12 12 12 12 12 12 * MCDONNELL DOUGLAS DC-08-71 325.00 240.00 CFM-56-2C5 4 22.00 6.00 94.3 92.9 98.3 3 * MCDONNELL DOUGLAS DC-08-71 328.00 258.00 CFM56-2-C1 4 22.00 6.00 15 50 94.5 92.9 98.6 3 * MCDONNELL DOUGLAS DC-08-72 335.00 240.00 CFM56-2-C1 4 22.00 6.00 12 50 94.4 92.9 98.1 3 * MCDONNELL DOUGLAS DC-08-72 350.00 250.00 CFM56-2-C1 4 22.00 6.00 12 50 95.2 92.8 98.2 3 * MCDONNELL DOUGLAS DC-08-73 355.00 258.00 CFM56-2-C1 4 22.00 6.00 12 50 95.7 92.8 98.3 3 * MCDONNELL DOUGLAS DC-08-73 355.00 275.00 CFM56-2-C1 4 22.00 6.00 12 50 95.7 92.8 98.5 3 * MCDONNELL DOUGLAS DC-09-10 (ABS) 90.70 81.70 JT8D-7/7A/7B 2 14.00 1.40 10 40 87.2 96.4 95.0 3 6 Page 34 ### Page 231 APPENDIX 3 ***STAGE 3*** **TURBOJET POWERED AIRPLANES** **MANUFACTURER** **MCDONNELL DOUGLAS** MCDONNELL DOUGLAS MODEL DC-09-10 (AIRWELD STC ST00934LA) DC-09-20 (ABS;STC SA1613GL) 1000# MTOW 108.00 100.00 1000# MLW 99.00 93.40 **ENGINE MODEL JT8D-9A JT8D-9/9A NO.** 2 2 THRUST 1000# 14.50 **14.50 BPR** 1.03 **1.03 TO AP FLAPS 0 40 0 40** TO SL AP NOISE LEVEL (EPNdB) 90.6 96.7 95.6 88.8 96.9 95.7 STAGE NOTES 3 12 3 MCDONNELL DOUGLAS DC-09-30 (ABS/SA16136L) 103.00 99.00 JT8D-9/9A 2 14.50 1.03 0 40 89.7 96.8 96.0 3 12 MCDONNELL DOUGLAS DC-09-30 (ABS;STC SA1613GL) 107.00 101.00 JT8D-9/9A 2 14.50 1.03 0 40 90.1 97.1 96.0 3 MCDONNELL DOUGLAS DC-09-30(ABS/SA1613GL) 103.00 99.00 JT8D-7/7A/7B 2 14.00 1.40 0 40 90.3 95.9 96.0 3 MCDONNELL DOUGLAS DC-09-30(ABS/SA1613GL) 105.00 101.00 JT8D-7/7A/7B 2 14.00 1.40 0 40 91.0 95.8 96.0 3 MCDONNELL DOUGLAS DC-09-30(ABS/SA1613GL) 105.00 101.00 JT8D-9/9A 2 14.50 1.03 0 40 90.3 96.7 96.1 3 MCDONNELL DOUGLAS DC-09-30(ABS/SA1785GL) 103.00 99.00 JT8D-7/7A/7B 2 14.00 1.40 0 40 90.4 95.9 96.0 3 MCDONNELL DOUGLAS DC-09-30(ABS/SA1785GL) 103.00 99.00 JT8D-9/9A 2 14.50 1.03 0 40 89.7 96.8 96.0 3 MCDONNELL DOUGLAS DC-09-30(ABS/SA1785GL) 107.00 101.00 JT8D-7/7A/7B 2 14.00 1.40 0 40 91.0 96.2 96.0 3 MCDONNELL DOUGLAS DC-09-30(ABS/SA1785GL) 107.00 101.00 JT8D-9/9A 2 14.50 1.03 0 40 90.1 97.1 96.0 3 **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS** MCDONNELL DOUGLAS DC-09-31/32/32F/33F(ABS;STC SA1613GL) DC-09-31/32/32F/33F(ABS;STC SA1613GL) DC-10-10 103.00 107.00 410.00 99.00 101.00 347.80 JT8D-7/7A/7B JT8D-7/7A/7B CF6-6D 2 2 3 14.00 14.00 39.30 1.40 1.40 5.90 0 0 14 40 40 50 90.3 91.0 97.4 95.9 96.2 97.0 96.0 96.0 104.9 3 3 3 * MCDONNELL DOUGLAS DC-10-10 410.00 347.80 CF6-6K 3 39.30 5.90 14 50 96.8 96.3 103.3 3 * MCDONNELL DOUGLAS DC-10-10 430.00 347.80 CF6-6K2 3 40.90 5.90 11 50 97.4 96.5 103.3 3 * MCDONNELL DOUGLAS DC-10-10 455.00 363.50 CF6-6D 3 39.30 5.90 0 50 101.8 96.0 105.5 3 * MCDONNELL DOUGLAS DC-10-10 455.00 363.50 CF6-6D1 3 40.30 5.80 4 50 100.2 96.6 105.5 3 * Page 35 ### Page 232 APPENDIX 3 ***STAGE 3*** TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES MCDONNELL DOUGLAS DC-10-10 430.00 363.50 CF6-6D1 3 40.30 5.80 11 50 98.1 97.0 105.5 3 * MCDONNELL DOUGLAS DC-10-10 430.00 363.50 CF6-6D1A 3 40.90 5.80 11 50 98.1 97.0 105.5 3 * MCDONNELL DOUGLAS DC-10-10 455.00 363.50 CF6-6D1A 3 40.90 5.80 4 50 100.2 96.6 105.5 3 * MCDONNELL DOUGLAS DC-10-10 455.00 363.50 CF6-6K 3 39.30 5.90 0 50 100.9 95.5 103.8 3 * MCDONNELL DOUGLAS DC-10-10 455.00 363.50 CF6-6K2 3 40.90 5.90 4 50 99.3 96.1 103.8 3 * MCDONNELL DOUGLAS DC-10-15 455.00 363.50 CF6-50C2-F 3 45.60 4.60 5 50 93.8 95.6 103.1 3 MCDONNELL DOUGLAS DC-10-30 555.00 403.00 CF6-50A 3 48.40 4.30 5 50 101.8 96.9 106.3 3 * MCDONNELL DOUGLAS DC-10-30 555.00 403.00 CF6-50C/H 3 50.40 4.30 10 50 101.6 97.5 106.3 3 MCDONNELL DOUGLAS DC-10-30 572.00 403.00 CF6-50C1 3 51.80 4.20 10 50 102.1 98.3 106.3 3 MCDONNELL DOUGLAS DC-10-30 555.00 403.00 CF6-50C2 3 51.80 4.30 5 50 96.8 97.8 105.0 3 MCDONNELL DOUGLAS DC-10-30 555.00 403.00 CF6-50C2-B 3 53.20 4.30 5 50 96.1 98.4 105.0 3 MCDONNELL DOUGLAS DC-10-30 555.00 403.00 CF6-50C2-R 3 50.40 4.40 10 50 97.5 97.2 105.0 3 MCDONNELL DOUGLAS DC-10-30 565.00 411.00 CF6-50A 3 48.40 4.30 5 50 102.7 96.8 106.6 3 * MCDONNELL DOUGLAS DC-10-30 572.00 411.00 CF6-50C/H 3 50.40 4.30 10 50 102.3 97.5 106.6 3 MCDONNELL DOUGLAS DC-10-30 590.00 411.00 CF6-50C1 3 51.80 4.20 10 50 103.0 98.0 106.6 3 MCDONNELL DOUGLAS DC-10-30 590.00 411.00 CF6-50C2 3 51.80 4.30 15 50 99.0 97.9 105.3 3 MCDONNELL DOUGLAS DC-10-30 590.00 411.00 CF6-50C2-B 3 53.20 4.30 15 50 98.7 98.5 105.3 3 MCDONNELL DOUGLAS DC-10-30 572.00 421.00 CF6-50C2-R 3 50.40 4.40 10 50 98.4 97.3 105.8 3 Page 36 ### Page 233 APPENDIX 3 ***STAGE 3*** TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES MCDONNELL DOUGLAS DC-10-30 555.00 424.00 CF6-50C2 3 51.80 4.30 5 50 96.8 97.8 106.0 3 15 MCDONNELL DOUGLAS DC-10-30 572.00 424.00 CF6-50C2-B 3 53.20 4.30 10 50 97.4 98.5 106.0 3 15 MCDONNELL DOUGLAS DC-10-30 555.00 424.00 CF6-50C2-B 3 53.20 4.30 5 50 96.1 98.4 106.0 3 15 MCDONNELL DOUGLAS DC-10-30 590.00 436.00 CF6-50C2 3 51.80 4.30 15 50 99.0 97.7 106.4 3 15 MCDONNELL DOUGLAS DC-10-40 530.00 403.00 JT9D-20D 3 44.50 5.00 10 50 100.8 95.2 105.7 3 * MCDONNELL DOUGLAS DC-10-40 555.00 403.00 JT9D-59A 3 51.70 4.90 10 50 101.4 98.0 106.4 3 * MCDONNELL DOUGLAS MD-10-10 440.00 375.00 CF6-6K 3 39.30 5.90 5 50 99.2 96.2 104.4 3 56 MCDONNELL DOUGLAS MD-10-10 440.00 375.00 CF6-6K W/ FSMS 3 39.30 5.90 5 50 99.2 95.9 104.4 3 56 MCDONNELL DOUGLAS MD-10-30 565.00 424.00 CF6-50C2 3 51.80 4.30 10 50 96.9 97.4 106.0 3 57 MCDONNELL DOUGLAS MD-10-30 580.00 436.00 CF6-50C2 3 51.80 4.30 15 50 97.9 97.4 106.3 3 57 MCDONNELL DOUGLAS MD-11 602.50 430.00 CF6-80C2 3 61.50 5.30 10 50 92.8 96.3 103.6 3 MCDONNELL DOUGLAS MD-11 602.50 430.00 CF6-80C2D1F 3 61.50 5.30 10 50 92.8 96.3 103.6 3 MCDONNELL DOUGLAS MD-11 602.50 430.00 PW4460 3 60.00 5.00 10 50 93.7 96.3 103.8 3 MCDONNELL DOUGLAS MD-11 602.50 430.00 PW4462 3 62.00 5.00 10 50 93.1 96.6 103.8 3 MCDONNELL DOUGLAS MD-11 618.00 471.50 CF6-80C2 3 61.50 5.30 10 50 93.9 96.3 104.3 3 MCDONNELL DOUGLAS MD-11 630.50 481.50 PW4460 3 60.00 5.00 10 50 95.8 96.1 104.4 3 MCDONNELL DOUGLAS MD-11 630.50 481.50 PW4462 3 62.00 5.00 10 50 95.0 96.5 104.4 3 MCDONNELL DOUGLAS MD-11 A-1 602.50 430.00 CF6-80C2D1F 3 61.50 5.30 10 50 92.8 96.4 103.6 3 Page 37 ### Page 234 APPENDIX 3 ***STAGE 3*** TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES MCDONNELL DOUGLAS MD-11 A-1 602.50 430.00 PW4460 (-3) 3 60.00 5.00 10 50 93.9 96.3 103.4 3 MCDONNELL DOUGLAS MD-11 A-1 602.50 430.00 PW4462 (-3) 3 62.00 5.00 10 50 93.3 96.6 103.4 3 MCDONNELL DOUGLAS MD-11 A-1 630.50 481.50 CF6-80C2D1F 3 61.50 5.30 10 50 94.6 96.4 104.5 3 MCDONNELL DOUGLAS MD-11 A-1 630.50 481.50 PW4460 (-3) 3 60.00 5.00 10 50 95.7 96.1 104.4 3 MCDONNELL DOUGLAS MD-11 A-1 630.50 481.50 PW4462 (-3) 3 62.00 5.00 10 50 95.0 96.5 104.4 3 MCDONNELL DOUGLAS MD-80 140.00 128.00 JT8D-209 2 19.25 1.83 0 40 88.9 94.7 92.8 3 10 MCDONNELL DOUGLAS MD-80 140.00 128.00 JT8D-219 2 21.70 1.70 0 40 86.7 97.3 92.8 3 10 MCDONNELL DOUGLAS MD-80 149.50 130.00 JT8D-209 2 19.25 1.83 0 40 91.1 94.5 92.9 3 10 MCDONNELL DOUGLAS MD-80 142.00 130.00 JT8D-217 2 20.85 1.80 0 40 88.2 96.1 92.9 3 10 MCDONNELL DOUGLAS MD-80 149.50 130.00 JT8D-217 2 20.85 1.80 0 40 89.7 95.8 92.9 3 10 MCDONNELL DOUGLAS MD-80 149.50 130.00 JT8D-219 2 21.70 1.70 0 40 88.6 97.1 92.9 3 10 MCDONNELL DOUGLAS MD-80 160.00 150.00 JT8D-217A 2 20.85 1.80 2 40 92.0 95.9 93.7 3 10 MCDONNELL DOUGLAS MD-80 160.00 150.00 JT8D-217C 2 20.85 1.70 2 40 91.5 96.3 93.7 3 10 MCDONNELL DOUGLAS MD-80 160.00 150.00 JT8D-219 2 21.70 1.70 2 40 90.8 97.2 93.7 3 10 MCDONNELL DOUGLAS MD-87 125.00 120.00 JT8D-217A 2 20.85 1.80 0 40 84.3 96.4 92.9 3 10 MCDONNELL DOUGLAS MD-87 125.00 120.00 JT8D-217C 2 20.85 1.70 0 40 84.1 96.5 92.9 3 10 MCDONNELL DOUGLAS MD-87 140.00 128.00 JT8D-219 2 21.70 1.70 0 40 86.5 97.1 93.3 3 10 MCDONNELL DOUGLAS MD-87 149.50 130.00 JT8D-217A 2 20.85 1.80 1 40 89.7 95.9 93.3 3 10 Page 38 ### Page 235 APPENDIX 3 ***STAGE 3*** TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES MCDONNELL DOUGLAS MD-87 149.50 130.00 JT8D-217C 2 20.85 1.70 1 40 89.2 96.2 93.3 3 10 MCDONNELL DOUGLAS MD-87 149.50 130.00 JT8D-219 2 21.70 1.70 1 40 88.5 97.1 93.3 3 10 MCDONNELL DOUGLAS MD-90-30 135.00 130.00 V2525-D5 2 25.00 4.80 5 40 78.3 89.2 91.7 3 MCDONNELL DOUGLAS MD-90-30 135.00 130.00 V2528-D5 2 28.00 4.80 5 40 77.2 91.4 91.7 3 MCDONNELL DOUGLAS MD-90-30 166.00 142.00 V2525-D5 2 25.00 4.80 5 40 84.2 88.8 91.9 3 MCDONNELL DOUGLAS MD-90-30 166.00 142.00 V2528-D5 2 28.00 4.80 5 40 82.6 91.0 91.9 3 MITSUBISHI MU-300 (DIAMOND I) 14.10 13.20 JT15D-4 2 2.50 2.68 10 30 86.3 88.0 85.8 3 * MITSUBISHI MU-300 (DIAMOND I) 15.50 13.20 JT15D-4D 2 2.50 2.68 0 30 81.2 88.4 85.8 3 MITSUBISHI MU-300-10 (DIAM. II) 15.78 14.22 JT15D-5 2 2.90 2.10 10 30 88.6 93.7 91.4 3 * RAYTHEON 390 PREMIER 12.50 11.60 FJ44-2A 2 2.30 0 30 76.6 87.9 92.0 3 RAYTHEON C-29A 28.00 23.35 TFE731-5R-1H 2 4.30 3.30 0 45 81.4 87.3 95.8 3 RAYTHEON HAWKER 125- 1A 21.70 19.60 TFE731-3-1H 2 3.70 2.70 0 45 84.2 90.0 96.0 3 RAYTHEON HAWKER 125- 1A 21.20 19.60 TFE731-3-1H 2 3.70 2.70 0 45 83.4 90.1 96.0 3 RAYTHEON HAWKER 125- 3A 21.70 20.00 TFE731-3-1H 2 3.70 2.70 0 45 84.2 90.0 96.3 3 RAYTHEON HAWKER 125- 3A/RA 23.60 20.00 TFE731-3-1H 2 3.70 2.70 0 45 85.5 89.8 95.7 3 RAYTHEON HAWKER 125- 400A 23.60 20.00 TFE731-3-1H 2 3.70 2.70 0 45 85.5 89.8 95.7 3 RAYTHEON HAWKER 125- 600A 25.50 22.00 TFE731-3-1H 2 3.70 2.70 0 45 88.0 89.2 96.3 3 RAYTHEON HAWKER 125- 700A 25.50 22.00 TFE731-3-1H 2 3.70 2.70 0 45 88.0 89.2 96.3 3 33 Page 39 ### Page 236 APPENDIX 3 ***STAGE 3*** TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES RAYTHEON HAWKER 125- 800 27.40 23.35 TFE731-5R-1H 2 4.30 3.30 0 45 80.9 87.2 96.5 3 RAYTHEON HAWKER 125- 800A 27.40 23.35 TFE731-5R-1H 2 4.30 3.30 0 45 80.9 89.6 96.5 3 25 RAYTHEON HAWKER 125-1000 31.00 25.00 PW305 2 5.20 4.50 0 25 81.8 85.9 91.6 3 RAYTHEON HAWKER 125-1000 35.50 28.50 PW305 2 5.20 4.50 0 25 85.7 85.3 92.0 3 SABRELINER SABRELINER 65 22.70 21.80 TFE731-3R 2 3.70 2.80 0 36 82.3 93.1 90.6 3 * SABRELINER SABRELINER 65 24.00 21.80 TFE731-3R 2 3.70 2.80 84.0 93.0 90.6 3 * Refer to Appendix 1 for Note Explanations Page 40 ### Page 237 11/15/01 MANUFACTURER BOEING BOEING BOEING BOEING BOEING BOEING BOEING BOEING BOEING BOEING BOEING BOEING BOEING BOEING BOEING BOEING MCDONNELL DOUGLAS AC 36-1H APPENDIX 4 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***TAKEOFF*** MODEL MTOW 1000# MLW 1000# ENGINE MODEL TO FLAPS TO NOISE LEVEL (EPNdB) NOTES B-747-200 767.00 564.00 JT9D-3A 10 110.0 * ** B-747-200 800.00 630.00 JT9D-7F 10 109.7 * ** B-747-200 812.00 630.00 JT9D-7FW/-7J 10 109.7 * ** B-747-100 734.00 564.00 JT9D-3A 10 109.4 * ** B-747-200 805.00 630.00 JT9D-7FW 10 109.4 * ** B-747-200 785.00 630.00 JT9D-7A 10 109.3 * ** B-747-200 800.00 630.00 JT9D-7J 10 109.3 * ** B-747-200 773.00 585.00 JT9D-3AWET 10 109.1 * ** B-747-200 770.00 564.00 JT9D-7 10 108.9 * ** B-747-200 785.00 630.00 JT9D-7WET 10 108.7 * ** B-747-100 710.00 564.00 JT9D-7 10 108.0 * ** B-747-100 750.00 585.00 JT9D-7A 10 107.8 * ** B-747-100 750.00 585.00 JT9D-7F 10 107.7 * ** B-747-100 750.00 585.00 JT9D-7FW 10 107.6 * ** B-747-100 750.00 585.00 JT9D-7WET 10 107.4 * ** B-747-200 833.00 585.00 RB211-524C2 10 106.5 * DC-08-55 (QNC PLS QN) 320.30 217.00 JT3D-3B 105.5 6,26,** Page 1 ### Page 238 APPENDIX 4 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***TAKEOFF*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL TO FLAPS TO NOISE LEVEL (EPNdB) NOTES MCDONNELL DOUGLAS DC-08-61 (QNC PLS QN) 320.30 240.00 JT3D-3B 105.5 6,** BOEING B-707-300B ADV/C ( SHN) 322.30 247.00 JT3D-1-3B(IC) 14 105.5 6,21,** BOEING B-747-200 820.00 630.00 RB211-524B/B2 10 105.5 ** BOEING B-747-300 820.00 630.00 RB211-524B2 10 105.5 ** BOEING B-747-100 710.00 540.00 JT9D-3A 10 105.4 29 MCDONNELL DOUGLAS DC-08-55/F54 (BAC STC: 313.70 217.00 JT3D-3B 15 105.3 6,26,** SA3915NM) MCDONNELL DOUGLAS DC-08F-54/55 (BAC STC: 313.70 240.00 JT3D-3B 15 105.3 6,26,** SA3915NM) MCDONNELL DOUGLAS DC-08-53 (QNC PLS QN) 318.00 207.00 JT3D-3B 105.3 6,26,** MCDONNELL DOUGLAS DC-08-53 (QNC QN) 306.80 207.00 JT3D 15 105.2 6,** MCDONNELL DOUGLAS DC-08-53 (QNC QN) 309.80 207.00 JT3D-3B 15 105.2 6,26,** MCDONNELL DOUGLAS DC-08-55 (QNC QN) 309.80 217.00 JT3D-3B 15 105.2 6,26,** MCDONNELL DOUGLAS DC-08-61 (QNC QN) 309.80 240.00 JT3D-3B 15 105.2 6,26,** MCDONNELL DOUGLAS DC-08F-54 (QNC QN) 309.80 240.00 JT3D-3B 15 105.2 6,26,** MCDONNELL DOUGLAS DC-08F-55 (QNC QN) 309.80 240.00 JT3D-3B 15 105.2 6,26,** MCDONNELL DOUGLAS DC-08-61F (QNC QN) 309.80 248.00 JT3D-3B 15 105.2 6,26,** MCDONNELL DOUGLAS DC-08F-54 (QNC PLS QN) 315.00 217.00 JT3D-3B 105.2 6,** MCDONNELL DOUGLAS DC-08F-55 (QNC PLS QN) 317.80 240.00 JT3D-3B 105.2 6,26,** BOEING B-747-100 734.00 540.00 JT9D-7 10 105.1 29 Page 2 ### Page 239 APPENDIX 4 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***TAKEOFF*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL TO FLAPS TO NOISE LEVEL (EPNdB) NOTES MCDONNELL DOUGLAS DC-08-53 (QNC QN) 315.00 207.00 JT3D-3B 104.9 6,** MCDONNELL DOUGLAS DC-08F-54 (QNC PLS QN) 315.00 240.00 JT3D-3B 104.9 6,26,** MCDONNELL DOUGLAS DC-08-63 (ADC QN) 355.00 275.00 JT3D-3B 12 104.8 6,** BOEING B-707-300B ADV/C (SHN) 330.00 201.00 JT3D-7 104.7 6,** BOEING B-707-300B ADV/C (SHN) 321.00 240.00 JT3D-3B 104.5 6,** BOEING B-747-100 750.00 520.00 JT9D-7F 10 104.5 29 BOEING B-747-100 750.00 585.00 RB211-524C2 10 104.5 * ** BOEING B-707-300B ADV/C (QNC) 335.00 247.50 JT3D-3B 104.4 6,** BOEING B-747-200 710.00 630.00 JT9D-3A 10 104.4 30 MCDONNELL DOUGLAS DC-08-62 (ADC QN) 350.00 250.00 JT3D-3B 12 104.3 6,** BOEING B-747-100 734.00 630.00 JT9D-7A 10 104.3 29 MCDONNELL DOUGLAS DC-08-52 (QNC QN) 300.00 202.00 JT3D-3B 15 104.2 6,** BOEING B-747-200 734.00 630.00 JT9D-7 10 104.2 30 MCDONNELL DOUGLAS DC-08-63 (ADC QN) 355.00 275.00 JT3D-7 12 104.1 6,** MCDONNELL DOUGLAS DC-08-62 (TNC QN) 350.00 250.00 JT3D-3B 12 103.9 6,** MCDONNELL DOUGLAS DC-08-63 (TNC QN) 350.00 250.00 JT3D-3B 12 103.9 6,** BOEING B-747-200 833.00 630.00 RB211-524D4 10 103.9 BOEING B-747-300 833.00 630.00 RB211-524D4 10 103.9 ** Page 3 ### Page 240 APPENDIX 4 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***TAKEOFF*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL TO FLAPS TO NOISE LEVEL (EPNdB) NOTES BOEING B-707-100B (QNC) 258.00 190.00 JT3D-3B 103.8 6,** MCDONNELL DOUGLAS DC-08-63 (TNC QN) 355.00 275.00 JT3D-7 12 103.8 6,** MCDONNELL DOUGLAS DC-08-52 (QNC QN) 300.00 202.00 JT3D-3B 15 103.7 6,26,** MCDONNELL DOUGLAS DC-08-55 (BAC STC: 325.00 217.00 JT3D-3B 15 103.7 6,26,** SA3915NM) MCDONNELL DOUGLAS DC-08-55 (BAC STC: 325.00 240.00 JT3D-3B 15 103.7 6,26,** SA3915NM) MCDONNELL DOUGLAS DC-08-61 (BAC STC: 325.00 240.00 JT3D-3B 15 103.7 6,26,** SA3915NM) BOEING B-747-200 770.00 630.00 JT9D-7J 10 103.6 30 BOEING B-707-120B (SHANNON) 258.00 190.00 JT3D-1 103.5 21,** BOEING B-747-200 734.00 630.00 JT9D-7A 10 103.5 30 BOEING B-747-200 750.00 630.00 JT9D-7F 10 103.5 30 BOEING B-707-100B (QNC) 241.30 190.00 JT3D-1 103.4 6,** MCDONNELL DOUGLAS DC-08-62 (ADC QN) 350.00 250.00 JT3D-7 12 103.4 6,** BOEING B-707-138B (SHANNON) 258.00 190.00 JT3D-1 103.2 21,** MCDONNELL DOUGLAS DC-08-52 (QNC PLS QN) 300.00 202.00 JT3D-3B 103.2 6,** BOEING B-747-200 833.00 630.00 JT9D-7Q 10 103.2 MCDONNELL DOUGLAS DC-10-30 590.00 411.00 CF6-50C1 10 103.0 MCDONNELL DOUGLAS DC-08-52 (QNC PLS QN) 300.00 202.00 JT3D-3B 102.9 6,26,** MCDONNELL DOUGLAS DC-08-62 (TNC QN) 355.00 275.00 JT3D-7 12 102.7 6,** Page 4 ### Page 241 APPENDIX 4 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***TAKEOFF*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL TO FLAPS TO NOISE LEVEL (EPNdB) NOTES 565.00 411.00MCDONNELL DOUGLAS DC-10-30 CF6-50A 5 102.7 * 833.00 630.00BOEING B-747-200 CF6-50E2 10 102.6 BOEING B-747-200 820.00 630.00 CF6-50E 10 102.5 **BOEING B-727-200 208.00 142.50 JT8D-17RQN 5 102.4 2,20** BOEING B-747-200 833.00 630.00 JT9D-7R4G2 10 102.4 ** **BOEING B-747-300 833.00 630.00 JT9D-7R4G2 10 102.4** BOEING B-720B (QNC) 234.00 175.00 JT3D-1 102.3 6,** MCDONNELL DOUGLAS DC-08-53 (BAC STC: 315.00 203.30 JT3D-3B 15 102.3 6,26,** SA3915NM) MCDONNELL DOUGLAS DC-08F-54 (BAC STC: 315.00 240.00 JT3D-3B 15 102.3 6,26,** SA3915NM) MCDONNELL DOUGLAS DC-10-30 572.00 411.00 CF6-50C/H 10 102.3 BOEING B-727-200 203.10 158.00 JT8D-17QN 5 102.0 2,19 BOEING B-747-SP JT9D-7A 10 102.0701.00 465.00 MCDONNELL DOUGLAS DC-08-51 (QNC PLS QN) 276.00 199.50 JT3D-1 101.9 6,** MCDONNELL DOUGLAS DC-10-10 CF6-6D 0 101.8 *455.00 363.50 610.00 564.00BOEING B-747-SR JT9D-7A 10 101.8 * **875.00 652.00BOEING B-747-400 PW4056 10 101.6** 800.00 630.00BOEING B-747-300 CF6-50E2 10 101.6 BOEING B-727-200 184.80 142.50 JT8D-9QN 15 101.5 2,17 Page 5 ### Page 242 APPENDIX 4 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***TAKEOFF*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL TO FLAPS TO NOISE LEVEL (EPNdB) NOTES 555.00 403.00MCDONNELL DOUGLAS DC-10-40 JT9D-59A 10 101.4 * MCDONNELL DOUGLAS DC-08-51 (QNC QN) 286.00 207.00 JT3D-3B 15 101.3 6,26,** MCDONNELL DOUGLAS DC-08-51 (BAC STC: 276.00 199.50 JT3D-1 15 101.2 6,** SA3915NM) BOEING B-747-200 820.00 630.00 JT9D-70A 10 101.1 MCDONNELL DOUGLAS DC-08-52 (BAC STC: 305.00 201.90 JT3D-3B 15 100.9 6,26,** SA3915NM) MCDONNELL DOUGLAS DC-10-10 455.00 363.50 CF6-6K 0 100.9 * MCDONNELL DOUGLAS DC-10-40 530.00 403.00 JT9D-20D 10 100.8 * BOEING B-727-200 178.00 150.00 JT8D-9FCD 5 100.7 3,17 MCDONNELL DOUGLAS DC-08-51 (QNC PLS QN) 286.00 207.00 JT3D-3B 100.7 6,26,** MCDONNELL DOUGLAS DC-08-62 (BAC II STC: 348.00 240.00 JT3D-3B 12 100.5 12 SA4892NM) MCDONNELL DOUGLAS DC-08-62 (BAC II STC: 350.00 240.00 JT3D-3B 12 100.5 12 SA5455NM) MCDONNELL DOUGLAS DC-10-10 CF6-6D1A 4 100.2 *455.00 363.50 455.00 363.50MCDONNELL DOUGLAS DC-10-10 CF6-6D1 4 100.2 * 820.00 630.00BOEING B-747-300 JT9D-70A 10 100.2 ** MCDONNELL DOUGLAS MD-10-10 440.00 373.50 CF6-6D W/ FSMS 5 100.1 56 BOEING B-747-SP JT9D-7J 10 100.1702.00 475.00 BOEING B-727-200 172.50 142.50 JT8D-7QN 15 100.0 2,16 BOEING B-727-200 190.50 142.50 JT8D-15QN 5 100.0 2,18 Page 6 ### Page 243 APPENDIX 4 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***TAKEOFF*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL TO FLAPS TO NOISE LEVEL (EPNdB) NOTES 440.00 373.50MCDONNELL DOUGLAS MD-10-10 CF6-6D 5 100.0 56 MCDONNELL DOUGLAS DC-08-51 (QNC QN) 276.00 199.50 JT3D-3B 15 99.9 6,** BOEING B-747-400 875.00 652.00 CF6-80C2B1F W/N1 MOD 10 99.9 BOEING B-727-200 177.60 142.50 JT8D-7FCD 5 99.8 3,16 MCDONNELL DOUGLAS DC-08-61 (BAC II STC: 325.00 240.00 JT3D-3B 15 99.8 12 SA4892NM) BOEING B-747-400 875.00 652.00 CF6-80C2B1F 10 99.8 BOEING B-747-400 870.00 652.00 CF6-80C2B1F 99.7 BOEING B-747-400 875.00 652.00 PW4056 PH3 (FB2B) 10 99.7 MCDONNELL DOUGLAS DC-08-51 (BAC STC: 276.00 199.50 JT3D-1 15 99.5 6,26,** SA3915NM) MCDONNELL DOUGLAS DC-08-51 (QNC PLS QN) 276.00 199.50 JT3D-3B 99.5 6,** BOEING B-707-300B/C (QSI STC: 336.00 247.00 JT3D-3B 14 99.5 12 ST00702LA) BOEING B-747-SP RB211-524B2 10 99.5696.00 450.00 BOEING B-720B (QNC) 234.00 175.00 JT3D-3B 99.3 6,** MCDONNELL DOUGLAS DC-08-51 (QNC QN) 276.00 199.50 JT3D-3B 15 99.3 6,26,** MCDONNELL DOUGLAS DC-10-10 CF6-6K2 4 99.3 *455.00 363.50 510.00 368.00LOCKHEED L-1011-500 RB211-524B4 10 99.3 * BOEING B-747-400 875.00 652.00 PW4056 PKG B/PHASE I 10 99.3 MCDONNELL DOUGLAS MD-10-10 CF6-6K 5 99.2 56440.00 375.00 Page 7 ### Page 244 APPENDIX 4 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***TAKEOFF*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL TO FLAPS TO NOISE LEVEL (EPNdB) NOTES MCDONNELL DOUGLAS MD-10-10 440.00 375.00 CF6-6K W/ FSMS 5 99.2 56 BOEING B-747-SP 702.00 410.00 RB211-524D4 10 99.2 BOEING B-747-400 875.00 652.00 RB211-524G 10 99.2 MCDONNELL DOUGLAS DC-08-51 (QNC PLS QN) 276.00 199.50 JT3D-3B 99.1 6,26,** MCDONNELL DOUGLAS DC-10-30 590.00 411.00 CF6-50C2 15 99.0 MCDONNELL DOUGLAS DC-10-30 590.00 436.00 CF6-50C2 15 99.0 15 BOEING B-747-300 833.00 666.00 CF6-80C2B1 10 99.0 BOEING B-720B (SHANNON) 234.00 175.00 JT3D-1 98.9 6,** MCDONNELL DOUGLAS DC-08-63 (BAC II STC: 353.00 267.00 JT3D-7 12 98.9 12 SA4892NM or SA5455NM) MCDONNELL DOUGLAS DC-08-63 (BAC II STC: 353.00 275.00 JT3D-7 12 98.9 6,26,** SA4892NM) MCDONNELL DOUGLAS DC-10-30 590.00 411.00 CF6-50C2-B 15 98.7 BOEING B-747-SP 660.00 475.00 JT9D-7F 10 98.7 BOEING B-747-400 875.00 652.00 PW4056 PH3 (FB2C) 10 98.6 MCDONNELL DOUGLAS DC-08-61 (QNC PLS QN) 270.00 240.00 JT3D-3B 98.6 6,26,** MCDONNELL DOUGLAS DC-08-51 (BAC STC: 276.00 199.50 JT3D-3B 15 98.6 6,** SA3915NM) MCDONNELL DOUGLAS DC-08-62 (BAC II STC: 350.00 240.00 JT3D-7 12 98.6 12 SA4892NM) LOCKHEED L1011-385-1-14/15 474.00 368.00 RB211-22B 4 98.6 BOEING B-727-100 169.50 137.50 JT8D-1FCD 5 98.5 3 Page 8 ### Page 245 APPENDIX 4 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***TAKEOFF*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL TO FLAPS TO NOISE LEVEL (EPNdB) NOTES BOEING B-707-300B/C (QSI STC: 336.00 247.00 JT3D-7 14 98.5 12 ST00702LA) LOCKHEED L-1011-100 466.00 368.00 RB211-22B 10 98.5 5 * MCDONNELL DOUGLAS DC-08-51 (BAC STC: 286.00 199.50 JT3D-3B 15 98.4 6,26,** SA3915NM) LOCKHEED L-1011-500 496.00 368.00 RB211-524B 14 98.4 5 * BOEING B-747-SR 571.00 564.00 CF6-45A2 10 98.4 MCDONNELL DOUGLAS DC-10-30 572.00 421.00 CF6-50C2-R 10 98.4 BOEING B-727-100 169.50 137.50 JT8D-9FCD 5 98.3 3,17 MCDONNELL DOUGLAS DC-09-50 121.00 110.00 JT8D-17 0 98.1 1 LOCKHEED L-1011-200 466.00 368.00 RB211-524B 10 98.1 5 * MCDONNELL DOUGLAS DC-09-34 121.00 110.00 JT8D-17 0 98.0 1 LOCKHEED L-1011-500 504.00 368.00 RB211-524B3 22 98.0 5 * BOEING B-747-400 875.00 652.00 RB211-524H2 10 98.0 BOEING B-727-100 169.50 137.50 JT8D-7FCD 5 97.9 3,16 LOCKHEED L1011-385-1-14/15 466.00 368.00 RB211-524B4 10 97.9 * MCDONNELL DOUGLAS MD-10-30 580.00 436.00 CF6-50C2 15 97.9 57 MCDONNELL DOUGLAS DC-09-34 121.00 110.00 JT8D-15 0 97.8 1 MCDONNELL DOUGLAS DC-09-50 121.00 110.00 JT8D-15 0 97.8 1 MCDONNELL DOUGLAS DC-08-62 (BAC II STC: 335.00 250.00 JT3D-7 12 97.8 12 SA4892NM or SA5455NM) Page 9 ### Page 246 APPENDIX 4 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***TAKEOFF*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL TO FLAPS TO NOISE LEVEL (EPNdB) NOTES BOEING B-747-400 870.00 652.00 RB211-524H 10 97.8 BOEING B-737-200 ADV. 128.10 88.00 JT8D-15QN 1 97.7 2,18 BOEING B727-200 (FED EX; STC 201.00 166.00 JT8D-15 w/BURBANK 5 97.7 27 SA5839NM) INLET+ FAN CSD BOEING B727-200 (FED EX; STC 204.50 159.00 JT8D-17 w/BURBANK 5 97.7 27 SA5839NM) INLET+CHIN OR FAN CSD BOEING B727-200 (FED EX; STC 199.05 166.00 JT8D-15 w/BOEING 5 97.6 27 SA5839NM) INLET+FAN CSD BOEING B727-200 (FED EX; STC 199.05 166.00 JT8D-15 w/BOEING 5 97.6 27 SA5839NM) INLET+CHIN CSD MCDONNELL DOUGLAS DC-09-30 110.00 101.00 JT8D-7 0 97.5 16,24 BOEING B727-200 (FED EX; STC 196.00 166.00 JT8D-9 w/BOEING 5 97.5 27 SA5839NM) INLET+FAN CSD BOEING B727-200 (FED EX; STC 196.00 166.00 JT8D-9 w/BOEING 5 97.5 27 SA5839NM) INLET+CHIN CSD BOEING B-747-400 875.00 652.00 CF6-80C2B5F 10 97.5 BOEING B727-200 (FED EX; STC 191.20 160.00 JT8D-9 w/BURBANK 5 97.4 27 SA5839NM) INLET+CHIN CSD BOEING B727-200 (FED EX; STC 191.20 160.00 JT8D-9 w/BURBANK 5 97.4 27 SA5839NM) INLET+ FAN CSD BOEING B727-200 (RAISBECK STC 193.00 161.00 JT8D-15 5 97.4 45 ST00685SE) MCDONNELL DOUGLAS DC-10-30 572.00 424.00 CF6-50C2-B 10 97.4 15 BOEING B-747-400 875.00 652.00 PW4056 PH3 (FB2C) NR 10 97.4 BOEING B-720B (SHANNON) 234.00 175.00 JT3D-3B 97.3 6,** MCDONNELL DOUGLAS DC-09-30 114.00 102.00 JT8D-9 0 97.1 1 MCDONNELL DOUGLAS DC-09-30 110.00 101.00 JT8D-9 0 97.0 24 Page 10 ### Page 247 APPENDIX 4 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***TAKEOFF*** **MANUFACTURER BOEING MODEL B-737-200 ADV.** MTOW 1000# 128.10 MLW 1000# 79.10 **ENGINE MODEL JT8D-17QN** TO FLAPS 1 TO NOISE LEVEL (EPNdB) 97.0 NOTES 2,19 BOEING BOEING BOEING B727-200 (FED EX; STC SA4833NM) B727-200 (RAISBECK STC ST00555SE) B727-200 (DUGAN AIR STC) 178.42 179.70 209.41 154.50 166.00 164.00 JT8D-7 w/BURBANK INLET+CHIN CSD JT8D-9 JT8D-15 5 5 4 97.0 97.0 97.0 35 34,44 MCDONNELL DOUGLAS BOEING DC-08-51 (BAC STC: **SA3915NM) B-737-200 ADV.** 276.00 122.50 199.50 105.00 JT3D-3B JT8D-9QN 15 1 97.0 96.9 6,26,** 2,17 BOEING BOEING MCDONNELL DOUGLAS B727-200 (FED EX; STC SA4833NM) B727-200 (FED EX; STC SA5839NM) DC-09-40 178.00 197.50 114.00 161.00 161.00 102.00 JT8D-7 w/BURBANK INLET+ FAN CSD JT8D-17R w/BURBANK INLET+CHIN OR FAN CSD JT8D-11 5 5 0 96.9 96.9 96.8 35 27 1 BOEING BOEING BOEING BOEING BOEING BOEING B727-200 (FED EX; STC SA5839NM) B727-100 (RAISBECK STC ST00448SE) B727-100 (FED EX; STC SA3993NM) B727-200 (RAISBECK STC ST00399SE) B727-100 (FED EX; STC SA3993NM) B-767-200 203.10 172.60 175.50 166.40 175.50 360.00 166.00 142.50 154.50 153.30 154.50 300.00 JT8D-17 w/BOEING INLET+CHIN OR FAN CSD JT8D-7 JT8D-7 w/BOEING INLET+CHIN CSD JT8D-9 JT8D-7 w/BURBANK INLET+CHIN CSD JT9D-7R4D(B) 5 5 5 5 5 1 96.8 96.6 96.6 96.5 96.3 96.2 27 16,43 35 17,34,43 35 AIRBUS A340-312 595.24 440.92 CFM56-5C3 17 96.2 BOEING B-777-300 660.00 524.00 RR TRENT 884 5 96.2 MCDONNELL DOUGLAS DC-09-34 110.00 101.00 JT8D-9 0 96.1 1 Page 11 ### Page 248 APPENDIX 4 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***TAKEOFF*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL TO FLAPS TO NOISE LEVEL (EPNdB) NOTES AIRBUS A340-212 595.25 440.92 CFM56-5C3 17 96.1 BOEING B727-200 (FED EX; STC 197.00 154.50 JT8D-17R w/BOEING 5 96.0 27 SA5839NM) INLET+CHIN OR FAN CSD LOCKHEED L-1011-1 430.00 358.00 RB211-22B 10 96.0 5 * MCDONNELL DOUGLAS DC-09-30 110.00 101.00 JT8D-7 0 95.9 1 BOEING B727-100 (DUGAN AIR STC) 174.50 142.50 JT8D-7 4 95.9 LOCKHEED L-1011 430.00 358.00 RB211-22B 14 95.9 5 * MCDONNELL DOUGLAS MD-11 630.50 481.50 PW4460 10 95.8 MCDONNELL DOUGLAS DC-09-30 114.00 102.00 JT8D-15 0 95.8 1 MCDONNELL DOUGLAS DC-09-40 114.00 102.00 JT8D-15 0 95.8 1 MCDONNELL DOUGLAS DC-08-73 355.00 275.00 CFM56-2-C1 12 95.7 * AIRBUS UK 1-11 400 89.50 79.00 SPEY511-14/14W 0 95.7 12 MCDONNELL DOUGLAS MD-11 A-1 630.50 481.50 PW4460 (-3) 10 95.7 AIRBUS A330-321 507.06 418.88 PW4164 8 95.6 BOEING B-737-200 NON-ADV. 117.00 101.70 JT8D-9QN 1 95.5 2,17 BOEING B-707-100B (BAC II STC: 200.00 160.00 JT3D-1 20 95.5 12 ST00956LA) BOEING B-767-200 360.00 300.00 JT9D-7R4E 1 95.4 BOEING B-727-200 RE (ROHR STC 209.42 164.00 JT8D-217C/JT8D-15 5 95.3 23,61 SA4363NM) BOEING B727-200 (FED EX; STC 177.60 154.50 JT8D-7 w/BOEING 5 95.2 35 SA4833NM) INLET+FAN CSD Page 12 ### Page 249 APPENDIX 4 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***TAKEOFF*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL TO FLAPS TO NOISE LEVEL (EPNdB) NOTES BOEING B727-200 (FED EX; STC 177.60 154.50 JT8D-7 w/BOEING 5 95.2 35 SA4833NM) INLET+CHIN CSD BOEING B-727-200 RE (ROHR STC 209.50 162.00 JT8D-217C/JT8D-17 5 95.2 23,62 SA4363NM) MCDONNELL DOUGLAS DC-08-72 350.00 250.00 CFM56-2-C1 12 95.2 * MCDONNELL DOUGLAS DC-09-30 108.00 99.00 JT8D-7A 0 95.1 1 BOEING B-767-200 351.00 300.00 JT9D-7R4D(A) 1 95.1 MCDONNELL DOUGLAS MD-11 630.50 481.50 PW4462 10 95.0 MCDONNELL DOUGLAS MD-11 A-1 630.50 481.50 PW4462 (-3) 10 95.0 BOEING B727-200 (DUGAN AIR STC) 190.50 164.00 JT8D-9 4 95.0 SABRELINER SABRELINER 60 20.20 JT12A-8 95.0 * BOEING B-767-300 351.00 320.00 JT9D-7R4E 5 95.0 BOEING B727-100 (FED EX; STC 174.50 142.50 JT8D-9 w/BURBANK 5 94.9 35 SA3993NM) INLET+CHIN CSD AIRBUS UK 1-11 400 87.00 77.20 SPEY511-14/14W 0 94.8 12 BOEING B-737-200 NON-ADV. 109.00 98.00 JT8D-7QN 1 94.7 2,16 BOEING B727-200 (FED EX; STC 177.60 154.50 JT8D-9 w/BOEING 5 94.7 35 SA4833NM) INLET+CHIN CSD BOEING B727-200 (FED EX; STC 177.60 154.50 JT8D-9 w/BOEING 5 94.7 35 SA4833NM) INLET+FAN CSD MCDONNELL DOUGLAS MD-11 A-1 630.50 481.50 CF6-80C2D1F 10 94.6 BOEING B727-100 (FED EX; STC 169.50 142.50 JT8D-7 w/BOEING 5 94.5 35 SA3993NM) INLET+FAN CSD SABRELINER SABRELINER 40 20.20 17.50 JT12A-8 0 94.5 Page 13 ### Page 250 APPENDIX 4 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***TAKEOFF*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL TO FLAPS TO NOISE LEVEL (EPNdB) NOTES 328.00 258.00MCDONNELL DOUGLAS DC-08-71 CFM56-2-C1 15 94.5 * SABRELINER SABRELINER 60A/60SC 22.70 20.60 JT12A-8 0 94.4 BOEING B-777-300 660.00 524.00 PW4090 5 94.4 55 MCDONNELL DOUGLAS DC-09-30 108.00 98.10 JT8D-17 0 94.3 1 MCDONNELL DOUGLAS DC-08-71 325.00 240.00 CFM-56-2C5 94.3 * AIRBUS A330-322 507.06 418.88 PW4168 8 94.3 BOEING B-777-200 632.50 470.00 RR TRENT 884 5 94.3 BOEING B-767-300 407.00 320.00 PW 4056 5 94.2 AIRBUS A330-301 507.06 418.88 CF6-80E1A2 14 94.2 660.00 524.00BOEING B-777-300 RR TRENT 892 5 94.2 BOEING B727-100 (FED EX; STC 169.50 142.50 JT8D-7 w/BURBANK 5 94.1 35 SA3993NM) INLET+ FAN CSD BOEING B727-100 (FED EX; STC 174.50 142.50 JT8D-9 w/BOEING 5 94.1 35 SA3993NM) INLET+CHIN CSD BOEING B727-200 (FED EX; STC 177.60 154.50 JT8D-9 w/BURBANK 5 94.1 35 SA4833NM) INLET+ FAN CSD BOEING B727-200 (FED EX; STC 177.60 154.50 JT8D-9 w/BURBANK 5 94.1 35 SA4833NM) INLET+CHIN CSD LEARJET 25C CJ610-6 20 94.0 1315.00 13.30 **15.00 13.30LEARJET 25D CJ610-6 20 94.0 14** **363.70 299.83AIRBUS A300B4-203 CF6-50-C2 0 94.0 31** 656.00 470.00BOEING B-777-200 RR TRENT 892 5 94.0 Page 14 ### Page 251 APPENDIX 4 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***TAKEOFF*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL TO FLAPS TO NOISE LEVEL (EPNdB) NOTES BOEING B727-100 (FED EX; STC 169.50 142.50 JT8D-9 w/BOEING 5 93.9 35 SA3993NM) INLET+FAN CSD MCDONNELL DOUGLAS MD-11 618.00 471.50 CF6-80C2 10 93.9 BOEING B-777-200 656.00 470.00 PW4090 5 93.9 55 BOEING B-767-300 407.00 320.00 RB211-524G 5 93.8 MCDONNELL DOUGLAS DC-10-15 455.00 363.50 CF6-50C2-F 5 93.8 BOEING B-727-200 RE (ROHR STC 198.50 162.00 JT8D-217C/JT8D-9 5 93.7 23,60 SA4363NM) BOEING B-767-200 400.00 300.00 PW 4056 1 93.7 AIRBUS A300B4-103 347.20 295.40 CF6-50-C2 16 93.6 LEARJET 25 16.00 13.30 CJ610-6 10 93.5 LEARJET 25B/C/D/F XR Dee Hwd 16.30 13.30 CJ610-6/8A 10 93.5 BOEING B-727-200 RE (ROHR STC 203.10 164.00 JT8D-217C/JT8D-17A 5 93.4 23 SA4363NM) BOEING B-777-200 656.00 470.00 RR TRENT 895 5 93.4 AIRBUS UK 1-11 200 80.00 71.00 SPEY 506-14 3 93.3 12 BOEING B-767-300 407.00 320.00 PW 4060 5 93.2 LOCKHEED 1329-25 (AIRESEARCH) 44.50 36.00 TFE731-3 93.1 * ** BOEING B-777-300 660.00 524.00 PW4098 5 93.1 BOEING B-727-200 RE (ROHR STC 198.70 162.00 JT8D-219/JT8D-9 5 93.0 23,60 SA4363NM) AIRBUS A310-304 352.74 286.60 CF6-80C2A2 0 92.9 Page 15 ### Page 252 APPENDIX 4 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***TAKEOFF*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL TO FLAPS TO NOISE LEVEL (EPNdB) NOTES BOEING B-767-300 407.00 320.00 RB211-524H 5 92.9 FOKKER F28 MK4000 73.00 69.50 SPEY MK555-15P 6 92.9 MCDONNELL DOUGLAS MD-11 602.50 430.00 CF6-80C2D1F 10 92.8 BOEING B-727-200 RE (ROHR STC 198.70 162.00 JT8D-219/JT8D-17 5 92.8 23 SA4363NM) BOEING B-767-200 360.00 300.00 CF6-80A 1 92.8 BOEING B-727-200 RE (ROHR STC 198.70 162.00 JT8D-219/JT8D-15 5 92.7 7,23,64 SA4363NM) BOEING B-727-200 RE (ROHR STC 198.70 162.00 JT8D-219/JT8D-9 5 92.7 7,23,63 SA4363NM) LOCKHEED 1329-23 (AIRESEARCH) 43.80 TFE731-3-1E 20 92.7 * ** GULFSTREAM G-II GULFSTREAM 65.50 58.50 SPEY 511-8 10 92.5 12 RAYTHEON HAWKER 125- 600A 25.50 22.00 VIPER 601-22 0 92.3 12 BOEING B-767-300/300ER 412.00 320.00 PW4062 (FB2B) 5 92.2 BOEING B-737-200 (AVAERO;STC 128.10 93.00 JT8D-15 1 92.1 27,42 ST223CH) BOEING B-737-200 ADV(AVAERO;STC 128.10 98.00 JT8D-15 1 92.1 27,42 ST223CH) BOEING B-737-200 ADV(AVAERO;STC 128.10 107.00 JT8D-15 1 92.1 27,42 ST223CH) BOEING B-727-100 (Dee Howard) 169.50 137.50 TAY 651-54 5 92.1 BOEING B-767-300 407.00 320.00 CF6-80C2-B4 5 92.1 MCDONNELL DOUGLAS MD-80 160.00 150.00 JT8D-217A 2 92.0 10 BOEING B-767-300 351.00 320.00 CF6-80A 5 92.0 Page 16 ### Page 253 APPENDIX 4 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***TAKEOFF*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL TO FLAPS TO NOISE LEVEL (EPNdB) NOTES BOEING B-777-200 545.00 470.00 RR TRENT 875 5 92.0 BOEING B-777-200 632.50 470.00 GE90-85B (BLK IV) 5 92.0 54 BOEING B-737-200 ADV (NORDAM; 124.50 107.00 JT8D-9 1 91.9 27,41 STC SA5730NM) LEARJET 24D 13.50 11.90 CJ610-6 20 91.9 FOKKER F28 MK4000 73.00 65.80 SPEY MK555-15H 6 91.9 BOEING B-737-200 ADV (NORDAM; 122.90 107.00 JT8D-9 w/LGW-L 1 91.8 36 STC ST00131SE) HUSHKIT BOEING B-737-200 ADV(AVAERO;STC 124.50 107.00 JT8D-15 1 91.8 35,42 ST223CH) BOEING B-737-200 ADV (NORDAM; 125.90 107.00 JT8D-15 w/LGW-L 1 91.8 37 STC ST00131SE) HUSHKIT LEARJET 24/24D 13.50 11.90 CJ610-6 20 91.8 13 LEARJET 24D 13.50 11.90 CJ610-6 20 91.8 14 AIRBUS A300B2-1C 313.00 286.60 CF6-50C2-R 0 91.8 BOEING B-737-200 ADV(AVAERO;STC 119.50 95.00 JT8D-9 1 91.7 35,41 ST223CH) BOEING B-737-200 ADV(AVAERO;STC 119.50 107.00 JT8D-9 1 91.7 35,41 ST223CH) BOEING B-737-200 ADV (NORDAM; 121.60 107.00 JT8D-15 w/LGW HUSHKIT 1 91.7 37 STC ST00131SE) BOEING B-767-200 360.00 300.00 CF6-80A2 1 91.7 BOEING B-777-200 555.00 470.00 RR TRENT 877 5 91.7 BOEING B-767-200/200ER 387.00 300.00 PW4060 1 91.6 BOEING B-737-200 ADV (NORDAM; 117.00 107.00 JT8D-7 w/LGW-N 1 91.6 40 STC ST00131SE) HUSHKIT Page 17 ### Page 254 APPENDIX 4 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***TAKEOFF*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL TO FLAPS TO NOISE LEVEL (EPNdB) NOTES BOEING B-737-200 ADV (NORDAM; 118.50 107.00 JT8D-9 w/LGW-N 1 91.6 36 STC ST00131SE) HUSHKIT BOEING B-737-200 ADV (NORDAM; 118.70 107.00 JT8D-9 w/LGW HUSHKIT 1 91.6 36 STC ST00131SE) RAYTHEON HAWKER 125- 700A 25.50 22.00 TFE731-3-1H 0 91.6 25,33 BOEING B-737-200 (AVAERO;STC 118.50 107.00 JT8D-9 1 91.5 35,41 ST223CH) BOEING B-737-200 (AVAERO;STC 121.50 107.00 JT8D-9 1 91.5 27,41 ST223CH) BOEING B-737-200 ADV(AVAERO;STC 121.50 107.00 JT8D-9 1 91.5 27,41 ST223CH) MCDONNELL DOUGLAS MD-80 160.00 150.00 JT8D-217C 2 91.5 10 AIRBUS A300 B4-605R 385.46 319.38 CF6-80C2A5F 0 91.5 BOEING B-777-200 656.00 470.00 GE90-90B (BLK IV) 5 91.5 54 BOEING B-737-200 (AVAERO;STC 128.10 88.00 JT8D-17 1 91.4 27 ST223CH) BOEING B-737-200 (AVAERO;STC 128.10 107.00 JT8D-17 1 91.4 27 ST223CH) BOEING B-757-200 255.50 210.00 PW 2037 5 91.4 MCDONNELL DOUGLAS DC-09-10 90.70 81.70 JT8D-7 10 91.4 24 MCDONNELL DOUGLAS DC-09-10 90.70 81.70 JT8D-7/-7A 10 91.4 1 BOEING B-777-200 632.50 460.00 GE90-85B 5 91.3 53 BOEING B-777-200 656.00 460.00 GE90-90B 5 91.3 53 BOEING B-737-200 ADV(AVAERO;STC 128.10 107.00 JT8D-17 1 91.2 27 ST223CH) SABRELINER SABRELINER 80A/80SC 25.50 22.00 CF700-2D-2 0 91.2 * Page 18 ### Page 255 APPENDIX 4 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***TAKEOFF*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL TO FLAPS TO NOISE LEVEL (EPNdB) NOTES BOEING B-767-300 351.00 320.00 CF6-80A2 5 91.2 BOEING B-767-400 450.00 350.00 CF6-80C2B8F 5 91.2 BOEING B-737-200 (NORDAM;STC 119.50 103.00 JT8D-15 w/LGW HUSHKIT 1 91.1 37 ST00131SE) MCDONNELL DOUGLAS MD-80 149.50 130.00 JT8D-209 0 91.1 10 AIRBUS A300B2-203 313.10 286.60 CF6-50-C2 16 91.1 BOEING B-767-300 407.00 320.00 CF6-80C2-B6 5 91.1 BOEING B-777-200 656.00 470.00 GE90-94B BLK IV) 5 91.1 54 GULFSTREAM G-IIB/G-III 69.70 58.50 SPEY 511-8 10 91.1 12 MCDONNELL DOUGLAS DC-09-30(ABS/SA1613GL) 105.00 101.00 JT8D-7/7A/7B 0 91.0 MCDONNELL DOUGLAS DC-09-30(ABS/SA1785GL) 107.00 101.00 JT8D-7/7A/7B 0 91.0 MCDONNELL DOUGLAS DC-09-31/32/32F/33F(ABS;STC 107.00 101.00 JT8D-7/7A/7B 0 91.0 SA1613GL) BOEING B-737-200 ADV (NORDAM; 126.70 107.00 JT8D-15 1 91.0 27,42 STC SA5730NM) LEARJET 25/25B/C Raisb MK II 15.00 13.30 CJ610 10 91.0 BOEING B-767-300/300ER 412.00 320.00 PW4056 PH3 (FB2C) NRI 5 91.0 FOKKER F28 MK3000 71.00 64.00 SPEY MK555-15H 6 91.0 BOEING B-767-200 351.00 285.00 PW4052 1 90.9 BOEING B-767-300 407.00 320.00 CF6-80C2B6F 5 90.9 BOEING B-777-200 535.00 445.00 PW4074 5 90.9 Page 19 ### Page 256 APPENDIX 4 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***TAKEOFF*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL TO FLAPS TO NOISE LEVEL (EPNdB) NOTES BOEING B-737-200 ADV (NORDAM; 120.50 107.00 JT8D-17/-17A w/LGW 1 90.8 STC ST00131SE) HUSHKIT MCDONNELL DOUGLAS MD-80 160.00 150.00 JT8D-219 2 90.8 10 BOEING B-777-200 535.00 445.00 PW4090 at PW4074 rating 5 90.8 55 SABRELINER SABRELINER 75A 23.00 CF700-2D-2 15 90.7 * SABRELINER SABRELINER 80 23.30 22.00 CF700-2D-2 90.7 * BOEING B-777-200 545.00 460.00 PW4077 5 90.7 BOEING B-767-200/200ER 387.00 300.00 CF6-80C2B4F W/N1 MOD 1 90.6 MCDONNELL DOUGLAS DC-09-10 (AIRWELD STC 108.00 99.00 JT8D-9A 0 90.6 12 ST00934LA) AIRBUS A310-324 330.69 271.16 PW-4152 15 90.6 BOEING B-767-200 387.00 300.00 CF6-80C2-B4 1 90.6 BOEING B-777-200 545.00 445.00 PW4090 at PW4077 rating 5 90.6 55 AIRBUS A310-221 305.60 267.90 JT9D-7R4D1 15 90.5 BOEING B-767-200/200ER 400.00 300.00 CF6-80C2B6F W/N1 MOD 1 90.5 MCDONNELL DOUGLAS DC-09-30(ABS/SA1613GL) 105.00 101.00 JT8D-9/9A 0 90.3 MCDONNELL DOUGLAS DC-09-30 (ABS) 111.00 101.00 JT8D-11 0 90.3 MCDONNELL DOUGLAS DC-09-30(ABS) 111.00 101.00 JT8D-11 0 90.3 12 BOEING B-737-200 ADV(AVAERO;STC 119.50 88.00 JT8D-15 1 90.3 35,42 ST223CH) BOEING B-767-300/300ER 412.00 320.00 PW4060 PH3 (FB2C) NRI 5 90.3 Page 20 ### Page 257 APPENDIX 4 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***TAKEOFF*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL TO FLAPS TO NOISE LEVEL (EPNdB) NOTES BOEING B-737-200 (NORDAM;STC 119.50 103.00 JT8D-15 w/LGW-L 1 90.2 37 ST00131SE) HUSHKIT BOEING B-737-200 ADV(AVAERO;STC 125.00 107.00 JT8D-17 1 90.2 27 ST223CH) BOEING B-767-200/200ER 360.00 300.00 CF6-80C2B2F 1 90.2 MCDONNELL DOUGLAS DC-09-30 (ABS;STC SA1613GL) 107.00 101.00 JT8D-9/9A 0 90.1 MCDONNELL DOUGLAS DC-09-30(ABS/SA1785GL) 107.00 101.00 JT8D-9/9A 0 90.1 LEARJET 25D/25F 15.00 13.30 CJ610-6/8A 8 90.1 BOEING B-737-200 ADV (NORDAM; 126.50 107.00 JT8D-17 1 90.0 27 STC SA5730NM) DASSAULT FALCON 20-Basic/D/E 28.66 27.32 CF700-2D-2 15 90.0 DASSAULT FALCON 20-F (M1400) 28.66 27.32 CF700-2D-2 10 90.0 FOKKER F28 MK2000 65.00 SPEY MK555-15 6 90.0 * FOKKER F28 MK1000 65.00 59.00 SPEY MK555-15 6 90.0 AIRBUS UK 1-11 400 (QTV STC: ST02167AT) 81.90 78.00 SPEY511-14/14W 90.0 BOEING B-767-300/300ER 412.00 320.00 PW4062 PH3 (FB2C) NRI 5 89.9 AIRBUS A321-211 205.02 171.51 CFM56-5B3/P; Mod. No. 89.8 27772 BOEING B-757-300 275.00 224.00 RB211-535-E4 5 89.8 58 BOEING B-767-200/200ER 395.00 300.00 PW4056 PH3 (FB2C) NRI 1 89.8 BOEING B-737-200 (AVAERO;STC 117.00 90.00 JT8D-15 1 89.7 35,42 ST223CH) MCDONNELL DOUGLAS MD-80 149.50 130.00 JT8D-217 0 89.7 10 Page 21 ### Page 258 APPENDIX 4 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***TAKEOFF*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL TO FLAPS TO NOISE LEVEL (EPNdB) NOTES MCDONNELL DOUGLAS MD-87 149.50 130.00 JT8D-217A 1 89.7 10 BOEING B-757-200 255.50 210.00 PW 2040 5 89.7 BOEING B-757-200 255.50 210.00 PW 2037QFC 5 89.7 59 BOEING B-767-200 351.00 300.00 CF6-80C2-B2 1 89.5 BOEING B-777-200 545.00 460.00 GE90-76B (BLK IV) 5 89.5 54 BOEING B-747-400 600.00 564.00 PW4056 10 89.5 BOEING B727-100 RE (ROHR STC 174.50 142.50 JT8D-217C/JT8D-9 5 89.4 23 SA4363NM) BOEING B-777-200 545.00 460.00 GE90-77B (BLK IV) 5 89.4 54 CESSNA 552 15.50 14.30 JT15D-5 20 89.3 * MCDONNELL DOUGLAS MD-87 149.50 130.00 JT8D-217C 1 89.2 10 LEARJET 24 Raisbeck MK II 13.00 11.90 CJ610-1/-4 10 89.0 BOEING B727-100 RE (ROHR STC 174.50 142.50 JT8D-219/JT8D-7B 5 89.0 23 SA4363NM) BOEING B-767-200/200ER 395.00 300.00 PW4060 PH3 (FB2C) NRI 1 89.0 BOEING B-737-400 142.50 121.00 CFM56-3-B1 5 88.9 MCDONNELL DOUGLAS DC-09-20 (ABS;STC SA1613GL) 100.00 93.40 JT8D-9/9A 0 88.8 BOEING B727-100 RE (ROHR STC 174.50 142.50 JT8D-219/JT8D-9 5 88.8 23 SA4363NM) BOEING B-777-200 545.00 460.00 GE90-77B 5 88.8 53 BOEING B-777-200 545.00 460.00 GE90-76B 5 88.8 53 Page 22 ### Page 259 APPENDIX 4 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***TAKEOFF*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL TO FLAPS TO NOISE LEVEL (EPNdB) NOTES BEECH BEECHJET 400 15.78 14.22 JT15D-5 10 88.6 * MITSUBISHI MU-300-10 (DIAM. II) 15.78 14.22 JT15D-5 10 88.6 * BOEING B-737-700 IGW/-700C 171.00 134.00 CFM56-7B24 1 88.6 51 BOEING B-737-800 174.20 146.30 CFM56-7B24 1 88.6 MCDONNELL DOUGLAS MD-87 149.50 130.00 JT8D-219 1 88.5 10 BOEING B-767-200/200ER 360.00 300.00 CF6-80C2B4F 1 88.5 BOEING B-737-900 174.20 147.30 CFM56-7B24 1 88.4 BOEING B-757-300 275.00 224.00 RB211-535E4-B 5 88.4 58 BOEING B-757-300 275.00 224.00 RB211-535E4-C 5 88.4 58 AIRBUS A321-231 205.02 171.51 V2533A5 88.2 BOEING B-757-200 240.00 210.00 RB211-535C 5 88.1 BOEING B-757-200 255.50 210.00 PW 2040QFC 5 88.1 59 LEARJET 23 Raisbeck MK II 12.50 11.90 CJ610-1/-4 10 88.0 AIRBUS A320-214 182.80 150.00 CFM56-5B4/P 10 88.0 RAYTHEON HAWKER 125- 600A 25.50 22.00 TFE731-3-1H 0 88.0 RAYTHEON HAWKER 125- 700A 25.50 22.00 TFE731-3-1H 0 88.0 33 AIRBUS A300B4-622R 330.00 275.00 PW-4158 0 88.0 AIRBUS A320-211 162.00 142.20 CFM56-5A1 10 87.8 Page 23 ### Page 260 APPENDIX 4 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***TAKEOFF*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL TO FLAPS TO NOISE LEVEL (EPNdB) NOTES BOEING B-737-800 174.20 146.30 CFM56-7B24/2 DAC 1 87.8 50 BOEING B-737-500 132.80 114.00 CFM56-3-B1(R) 5 87.7 BOEING B-737-400 150.00 124.00 CFM56-3B-2 5 87.7 LEARJET 24B/D Raisbeck MK II 13.50 11.88 CJ610 10 87.6 BOEING B-737-300 139.50 121.00 CFM56-3-B1 1 87.5 AIRBUS A319-113 158.73 149.91 CFM56-5A4 10 87.5 BOEING B-737-800W 174.20 146.30 CFM56-7B24 1 87.5 52 DASSAULT FALCON 20-G (M2500) 32.00 27.56 ATF3-6-2C 10 87.5 BOEING B-737-800/BBJ 2 174.20 146.30 CFM56-7B26; -7B26/B1 1 87.4 BOEING B-737-500 139.00 114.00 CFM56-3-B1 5 87.3 BOEING B-757-200 255.50 210.00 RB211-535-E4 5 87.3 58 BOEING B-737-900 174.20 147.30 CFM56-7B26 1 87.2 MCDONNELL DOUGLAS DC-09-10 (ABS) 90.70 81.70 JT8D-7/7A/7B 10 87.2 6 BOEING B-737-400 150.00 124.00 CFM56-3C-1 5 87.1 BOEING B-737-700 154.50 129.20 CFM56-7B20 1 87.1 BOEING B-737-700 IGW/-700C/BBJ 171.00 134.00 CFM56-7B26; -7B26/B1 1 87.1 51 LEARJET 28/29 15.00 14.30 CJ610-8A 8 87.0 BOEING B-737-800/BBJ 2 174.20 146.30 CFM56-7B27; -7B27/B3 1 87.0 Page 24 ### Page 261 APPENDIX 4 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***TAKEOFF*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL TO FLAPS TO NOISE LEVEL (EPNdB) NOTES LEARJET 55C 21.50 17.00 TFE731-3AR-3B 20 87.0 * BOEING B-737-400 142.50 124.00 CFM56-3 w/HWFAP 5 86.9 38 BOEING B-737-400 142.50 124.00 CFM56-3 w/HWFAP 5 86.9 BOEING B-737-800W 174.20 146.30 CFM56-7B24/2 DAC 1 86.9 50,52 AIRBUS A319-114 163.14 149.91 CFM56-5A5 10 86.8 BOEING B-737-800/BBJ 2 174.20 146.30 CFM56-7B27/B1; -7B27/B2 1 86.8 BOEING B-757-200 255.50 210.00 RB211-535-E4 5 86.8 BOEING B-737-800 174.20 146.30 CFM56-7B26/2 DAC 1 86.7 50 BOEING B-737-900 174.20 147.30 CFM56-7B27 1 86.7 LEARJET 55C 21.50 18.00 TFE731-3AR-2B 20 86.7 * AIRBUS A320-231 162.00 142.20 V2500.A1 10 86.6 BOEING B-737-700 IGW/BBJ 171.00 134.00 CFM56-7B27/B3 1 86.6 51 BOEING B-737-900 174.20 147.30 CFM56-7B27/B1 1 86.6 BAE SYSTEMS (BAe) 146-300A 97.50 84.50 ALF502R-5 18 86.5 BOEING B-737-700 154.50 129.20 CFM56-7B20/2 DAC 1 86.4 50 BOEING B-737-800W/BBJ 2 174.20 146.30 CFM56-7B26; -7B26/B1 1 86.4 52 BAE SYSTEMS (BAe) 146-300 101.50 88.50 LF 507-1H/-1F 18 86.3 MITSUBISHI MU-300 (DIAMOND I) 14.10 13.20 JT15D-4 10 86.3 * Page 25 ### Page 262 APPENDIX 4 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***TAKEOFF*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL TO FLAPS TO NOISE LEVEL (EPNdB) NOTES BOEING B-737-400 150.00 124.00 CFM56-3 w/HWFAP 5 86.3 38 BOEING B-737-400 150.00 124.00 CFM56-3 w/HWFAP 5 86.3 BOEING B-737-700 154.50 129.20 CFM56-7B22 1 86.3 AIRBUS A319-112 166.44 149.91 CFM56-5B6/P 10 86.3 LEARJET 55B 21.50 18.00 TFE731-3A-2B 20 86.3 * BOEING B-757-200 255.50 210.00 RB211-535E4-B 5 86.2 58 BAE SYSTEMS (AVRO) 146-RJ 100 101.50 88.50 LF 507-1F 18 86.1 BOEING B-737-800 174.20 146.30 CFM56-7B27/2 DAC 1 86.1 50 BOEING B-737-800W/BBJ 2 174.20 146.30 CFM56-7B27; -7B27/B3 1 86.0 52 BOEING B-737-400 150.00 124.00 CFM56-3 w/HWFAP 5 85.9 38 BOEING B-737-400 150.00 124.00 CFM56-3 w/HWFAP 5 85.9 BOEING B-737-700 154.50 129.20 CFM56-7B24 1 85.9 BOEING B-737-800 174.20 146.30 CFM56-7B27/2B1 DAC 1 85.9 50 BAE SYSTEMS (BAe) 146-200A 89.50 77.50 ALF502R-3 18 85.9 LEARJET 24F 13.50 11.90 CJ610-6 8 85.8 BOEING B-737-800W/BBJ 2 174.20 146.30 CFM56-7B27/B1; -7B27/B2 1 85.8 52 BOEING B-737-300 139.50 121.00 CFM56-3B-2 1 85.7 BOEING B-737-600 143.50 120.50 CFM56-7B18 1 85.7 Page 26 ### Page 263 APPENDIX 4 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***TAKEOFF*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL TO FLAPS TO NOISE LEVEL (EPNdB) NOTES BOEING B-757-200 255.50 210.00 RB211-535E4-B 5 85.7 RAYTHEON HAWKER 125-1000 35.50 28.50 PW305 0 85.7 BOEING B-737-700 154.50 129.20 CFM56-7B22/2 DAC 1 85.6 50 BOEING B-737-800W 174.20 146.30 CFM56-7B26/2 DAC 1 85.6 50,52 LEARJET 55 21.00 17.00 TFE731-3A-2B 8 85.5 * RAYTHEON HAWKER 125- 3A/RA 23.60 20.00 TFE731-3-1H 0 85.5 RAYTHEON HAWKER 125- 400A 23.60 20.00 TFE731-3-1H 0 85.5 BOEING B-737-500 132.80 114.00 CFM56-3 w/HWFAP 5 85.4 38 BOEING B-737-500 132.80 114.00 CFM56-3 w/HWFAP 5 85.4 BOEING B-737-500 139.00 114.00 CFM56-3 w/HWFAP 5 85.4 38 BOEING B-737-500 139.00 114.00 CFM56-3 w/HWFAP 5 85.4 BOEING B-737-600 143.50 120.50 CFM56-7B20 1 85.4 ISRAEL AIRCRAFT 1124A WESTWIND 2 23.50 19.00 TFE731-3-1G 20 85.4 * LOCKHEED 1329-25 (STAR 3 STC# 44.50 36.00 TFE731-3-1R 20 85.4 ST00259SE) AIRBUS A319-131 158.73 149.91 V2522-A5 10 85.3 BOEING B-737-300 139.50 121.00 CFM56-3 w/HWFAP 1 85.2 BOEING B-737-300 139.50 121.00 CFM56-3 w/HWFAP 1 85.2 38 BOEING B-737-600 143.50 120.50 CFM56-7B/2 DAC (B18 1 85.2 50 derate) Page 27 ### Page 264 APPENDIX 4 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***TAKEOFF*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL TO FLAPS TO NOISE LEVEL (EPNdB) NOTES LOCKHEED 1329-23A/D/E (STAR 3 STC 44.25 36.00 TFE731-3-1R 20 85.2 ST00258SE) BAE SYSTEMS (BAe) 146-200A 93.00 81.00 ALF502R-5 18 85.2 BOEING B-737-800W 174.20 146.30 CFM56-7B27/2 DAC 1 85.1 50,52 BOEING B-737-800W 174.20 146.30 CFM56-7B27/2B1 DAC 1 85.0 50,52 BOEING B-737-600 143.50 120.50 CFM56-7B20/2 DAC 1 84.9 50 BAE SYSTEMS (BAe) 146-200A 89.50 77.50 ALF502R-3A 18 84.9 DASSAULT FALCON 50 (M1230) 40.78 35.71 TFE731-3-1C 20 84.8 BOMBARDIER CL-600 (WINGLETS) 41.25 36.00 ALF-502L/L-2/L-2C 20 84.8 BOEING B-737-700 154.50 129.20 CFM56-7B24/2 DAC 1 84.7 50 BOMBARDIER CL-600 41.25 36.00 ALF-502L/L-2/L-2C 20 84.7 * BOEING B-737-700 154.50 129.20 CFM56-7B26 1 84.6 CESSNA 560 CITATION V 16.30 15.20 JT15D-5A 7 84.6 LEARJET 35/36 18.00 14.30 TFE731-2-2B 20 84.5 * BOEING B-737-600 143.50 120.50 CFM56-7B22 1 84.4 LEARJET 24E 12.90 11.90 CJ610-6 8 84.3 BAE SYSTEMS (AVRO) 146-RJ 85 97.00 85.00 LF 507-1F 18 84.3 MCDONNELL DOUGLAS MD-90-30 166.00 142.00 V2525-D5 5 84.2 RAYTHEON HAWKER 125- 1A 21.70 19.60 TFE731-3-1H 0 84.2 Page 28 ### Page 265 APPENDIX 4 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***TAKEOFF*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL TO FLAPS TO NOISE LEVEL (EPNdB) NOTES 21.70 20.00RAYTHEON HAWKER 125- 3A TFE731-3-1H 0 84.2 BOEING B-717-200 121.00 110.00 BR700-715A1-30 (MP) 5 84.1 49 ISRAEL AIRCRAFT 1125 ASTRA 24.70 20.70 TFE731-3A-200G 12 84.1 BAE SYSTEMS (AVRO) 146-RJ 70 90.00 83.50 LF 507-1F 18 84.1 BOEING B-717-200 121.00 110.00 BR700-715A1-30 5 84.0 48 SABRELINER SABRELINER 65 24.00 21.80 TFE731-3R 84.0 * BOMBARDIER CL-600 40.40 36.00 ALF 502L/L-2/L-2C 20 84.0 * BOEING B-737-300 139.50 121.00 CFM56-3 w/HWFAP 1 83.9 BOEING B-737-300 139.50 121.00 CFM56-3 w/HWFAP 1 83.9 38 18.30 15.30LEARJET 36A TFE731-2-2B 20 83.9 * DASSAULT FALCON 200 (M5634) 32.00 28.88 ATF3-6A-4C 5 83.9 BOEING B-737-700 154.50 129.20 CFM56-7B26/2 DAC 1 83.8 50 DASSAULT FALCON 50 (M2193) 40.79 35.72 TFE731-40-1 20 83.8 BOEING B-737-600 143.50 120.50 CFM56-7B22/2 DAC 1 83.7 50 EMBRAER EMB-145EP AE3007A 9 83.7 *46.29 41.22 **12.50 11.90LEARJET 24F-A CJ610-6 8 83.6** 18.00 14.30LEARJET 35A TFE731-2-2B 8 83.6 * BAE SYSTEMS (AVRO) 146-RJ 70 95.00 83.50 LF 507-1F 18 83.6 4 Page 29 ### Page 266 APPENDIX 4 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***TAKEOFF*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL TO FLAPS TO NOISE LEVEL (EPNdB) NOTES BOEING B-767-300 288.70 280.00 CF6-80C2B2 5 83.1 DASSAULT FALCON 50 ( M1810) 40.79 35.72 TFE731-40-1 20 83.0 CESSNA 560 CITATION Ultra 16.30 15.20 JT15D-5D 7 82.9 LEARJET 31A 17.00 16.00 TFE731-2-3B 8 82.9 DASSAULT FALCON 20-C5/D5/E5 (M3500) 29.10 27.73 TFE731-5AR-2C 15 82.9 DASSAULT FALCON 20-C5/D5/E5 (M3547) 30.50 28.88 TFE731-5BR-2C 15 82.9 DASSAULT FALCON 900 (M1196) 46.50 42.00 TFE731-5AR-1C 20 82.9 BOMBARDIER CL-600-2C10 (CRJ700) 75.00 66.90 CF34-8C1 8 82.7 BOMBARDIER BD-700-1A10 (Global Express) 96.00 78.50 BR700-710-A2-20 16 82.7 MCDONNELL DOUGLAS MD-90-30 166.00 142.00 V2528-D5 5 82.6 BAE SYSTEMS (BAe) 146-100A 82.25 73.35 ALF502R-3A 18 82.3 BOEING B-717-200 121.00 110.00 BR700-715C1-30 (MP) 5 82.2 49 DASSAULT FALCON 10 19.30 17.64 TFE731-2-1C 15 82.2 CESSNA 650 CITATION VI 22.45 20.00 TFE731-3C-100S 7 82.2 BOEING B-717-200 121.00 110.00 BR700-715C1-30 5 82.1 48 DASSAULT FALCON 20-Basic/D/E/F 28.66 27.32 CF700-2D-2Q 0 81.9 (M2851) DASSAULT FALCON 20-F5 (M3547) 30.50 28.88 TFE731-5BR-2C 10 81.9 DASSAULT FALCON 900 45.50 42.00 TFE731-5AR-1C 20 81.9 Page 30 ### Page 267 APPENDIX 4 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***TAKEOFF*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL TO FLAPS TO NOISE LEVEL (EPNdB) NOTES BAE SYSTEMS (AVRO) 146-RJ 85 89.50 77.50 LF 507-1F 18 81.9 DASSAULT FALCON 20-F5 (M3500) 29.10 27.73 TFE731-5AR-2C 10 81.8 BAE SYSTEMS (BAe) 146-100A 84.00 77.50 ALF502R-5 18 81.8 FOKKER F100 98.00 88.00 TAY MK650-15 0 81.8 BOMBARDIER CL-600 36.00 33.00 ALF-502 20 81.6 * BOEING B-757-200 187.00 198.00 PW 2037 5 81.5 RAYTHEON C-29A 28.00 23.35 TFE731-5R-1H 0 81.4 GULFSTREAM G200 34.85 28.00 PW306A 25 81.4 46 GULFSTREAM G200 34.85 28.00 PW306A 25 81.4 47 ISRAEL AIRCRAFT Galaxy 34.85 28.00 PW306A 0 81.4 MITSUBISHI MU-300 (DIAMOND I) 15.50 13.20 JT15D-4D 0 81.2 ISRAEL AIRCRAFT 1124 WESTWIND 22.90 19.00 TFE731-3-1G 20 81.2 BOMBARDIER CL-604 48.20 38.00 GE CF34-3B 20 81.2 * LEARJET 31 16.50 15.30 TFE731-2-3B 8 81.0 * RAYTHEON HAWKER 125- 800 27.40 23.35 TFE731-5R-1H 0 80.9 RAYTHEON HAWKER 125- 800A 27.40 23.35 TFE731-5R-1H 0 80.9 25 DASSAULT FALCON 900B (M1200) 46.50 42.00 TFE731-5BR-1C 20 80.7 BAE SYSTEMS (BAe) 146-100A 76.00 72.35 ALF502R-3 18 80.7 Page 31 ### Page 268 APPENDIX 4 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***TAKEOFF*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL TO FLAPS TO NOISE LEVEL (EPNdB) NOTES 45.10 36.00BOMBARDIER CL-601-1A CF-34-1A 20 80.5 * DASSAULT FALCON 20-C5/D5/E5 (M3530) 29.10 27.73 TFE-731-5BR-2C 15 80.3 GULFSTREAM G-V 90.50 75.30 BR700-710A1-10 10 80.3 CESSNA 551 CITATION II 12.50 12.00 JT15D-4 15 80.1 * CESSNA 650 CITATION III 22.00 20.00 TFE731-3B-100S 7 80.1 22 FOKKER F70 92.00 81.00 TAY MK620-15 0 80.1 CESSNA S550 CITATION S/II 15.10 14.40 JT15D-4B 7 80.0 ISRAEL AIRCRAFT 1125 ASTRA SPX 24.65 20.70 TFE731-40R 0 79.9 BOMBARDIER CL-601 43.00 36.00 CF34-1A 20 79.9 * BOMBARDIER CL-601-3A 45.10 36.00 CF-34-3A/-3A2 20 79.8 * BOMBARDIER CL-601-3R CF-34-3A1 20 79.8 *45.10 36.00 DASSAULT FALCON 900EX (M3000) 49.00 44.50 TFE731-60-1 20 79.8 BOMBARDIER CL-600-2B19 (CRJ) 53.00 47.00 CF-34-3A1 20 79.8 DASSAULT FALCON 2000 CFE738-1-1B 20 79.436.50 33.00 43.10 36.00BOMBARDIER CL-601-3A CF-34-3A 20 79.4 * EMBRAER EMB-145LR 48.50 42.54 AE3007A1/1 9 79.4 DASSAULT FALCON 20-F5 (M3530) 29.10 27.73 TFE-731-5BR-2C 10 79.3 LEARJET 35A/36A 18.30 15.30 TFE731-2-2B 8 79.2 Page 32 ### Page 269 APPENDIX 4 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***TAKEOFF*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL TO FLAPS TO NOISE LEVEL (EPNdB) NOTES GULFSTREAM G100 24.65 20.70 TFE731-40R-200G 25 79.1 CESSNA 650 CITATION VII 23.00 20.00 TFE731-4R-3S 7 78.9 BOMBARDIER CL-600-2B19 (CRJ) 53.00 47.00 CF-34-3B1 20 78.7 CESSNA 500/501 CITATION I 11.80 11.30 JT15D-1/-1A 15 78.0 * EMBRAER EMB-135LR 44.09 40.78 AE3007A1/3 9 77.9 EMBRAER EMB-145ER 45.41 41.22 AE3007A 9 77.9 GULFSTREAM G-IV GULFSTREAM w/ASC 190 74.60 66.00 TAY 611-8 20 77.5 GULFSTREAM G-IV 73.20 58.50 TAY 611-8 10 76.8 RAYTHEON 390 PREMIER 12.50 11.60 FJ44-2A 0 76.6 FAIRCHILD DORNIER DORNIER 328-300 Mod 10 34.52 31.72 PW306B 12 76.5 CESSNA 500 CITATION 10.30 9.90 JT15D-1 15 76.4 * FAIRCHILD DORNIER DORNIER 328-300 33.51 31.06 PW306B 12 76.1 BOMBARDIER BD700-1A10 (Global Express) 75.00 75.00 Rolls Royce/ BR700-710­ 16 75.6 (Learjet STC: SA8184NM-D) A2-20 CESSNA 525A CITATION JET II (CJ-2) 12.37 11.50 FJ44-2C 15 74.5 LEARJET 45 20.50 19.20 TFE731-20R-1B or (-20AR­ 8 74.4 1B) AEROSPATIALE SN601 CORVETTE 14.60 13.20 JT15D-4 15 74.0 CESSNA 550 CITATION Bravo 14.80 13.50 PW530A 15 73.7 CESSNA 525 CESSNA JET 10.40 9.70 FJ44-1A 15 73.4 Page 33 ### Page 270 APPENDIX 4 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***TAKEOFF*** MANUFACTURER CESSNA MODEL 560XL EXCEL MTOW 1000# 20.00 MLW 1000# 18.70 **ENGINE MODEL PW545A** TO FLAPS 7 TO NOISE LEVEL (EPNdB) 72.4 NOTES CESSNA 750 CITATION X 35.70 31.80 AE3007C 15 72.3 CESSNA 550 CITATION II 14.10 13.50 JT15D-4 0 71.6 LEARJET 60 23.10 19.50 PW305A 8 70.8 LEARJET 60 23.50 19.50 PW305A 8 70.8 CESSNA 560 ENCORE 16.63 15.20 PW535A 7 70.3 Refer to Appendix 1 for Note Explanations Page 34 ### Page 271 11/15/01 **MANUFACTURER** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS BOEING** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS BOEING** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS BOEING** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS** MCDONNELL DOUGLAS AC 36-1H APPENDIX 5 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***APPROACH*** MODEL DC-08-63 (ADC QN) MTOW 1000# 355.00 MLW 1000# 275.00 **ENGINE MODEL JT3D-3B** AP FLAPS 50 AP NOISE LEVEL (EPNdB) 108.5 NOTES 6,** DC-08-63 (ADC QN) 355.00 275.00 JT3D-7 50 108.4 6,** B-707-300B ADV/C (SHN) 330.00 201.00 JT3D-7 25 108.3 6,** DC-08-62 (ADC QN) 350.00 250.00 JT3D-7 50 108.3 6,** DC-08-62 (ADC QN) 350.00 250.00 JT3D-3B 50 108.3 6,** B-707-300B ADV/C (SHN) 321.00 240.00 JT3D-3B 25 108.2 6,** DC-08-53 (BAC STC: SA3915NM) DC-08-52 (BAC STC: SA3915NM) DC-08F-54 (BAC STC: SA3915NM) DC-08-55 (BAC STC: SA3915NM) DC-08-61 (BAC STC: **SA3915NM) B-707-300B ADV/C (QNC)** 315.00 305.00 315.00 325.00 325.00 335.00 203.30 201.90 240.00 240.00 240.00 247.50 JT3D-3B JT3D-3B JT3D-3B JT3D-3B JT3D-3B JT3D-3B 50 50 35 35 35 25 108.1 108.0 107.9 107.9 107.9 107.9 6,26,** 6,26,** 6,26,** 6,26,** 6,26,** 6,** DC-08-62 (TNC QN) 350.00 250.00 JT3D-3B 50 107.9 6,** DC-08-63 (TNC QN) 350.00 250.00 JT3D-3B 50 107.9 6,** DC-08-51 (BAC STC: SA3915NM) DC-08-51 (BAC STC: SA3915NM) DC-08-51 (BAC STC: SA3915NM) 276.00 276.00 286.00 199.50 199.50 199.50 JT3D-1 JT3D-3B JT3D-3B 50 50 50 107.8 107.8 107.8 6,26,** 6,26,** 6,26,** Page 1 ### Page 272 11/15/01 **MANUFACTURER BOEING BOEING BOEING** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS BOEING BOEING BOEING BOEING** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS BOEING BOEING BOEING BOEING** MCDONNELL DOUGLAS AC 36-1H APPENDIX 5 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***APPROACH*** MODEL MTOW 1000# MLW 1000# ENGINE MODEL AP FLAPS AP NOISE LEVEL (EPNdB) NOTES B-747-200 800.00 630.00 JT9D-7J 30 107.8 * ** B-747-200 800.00 630.00 JT9D-7F 30 107.8 * ** B-747-200 805.00 630.00 JT9D-7FW 30 107.8 * ** DC-08-63 (BAC II STC: 353.00 275.00 JT3D-7 50 107.6 6,26,** SA4892NM) DC-08-62 (TNC QN) 355.00 275.00 JT3D-7 35 107.6 6,** DC-08F-54 (QNC PLS QN) 315.00 240.00 JT3D-3B 35 107.4 6,26,** DC-08F-55 (QNC PLS QN) 317.80 240.00 JT3D-3B 35 107.4 6,26,** B-747-100 710.00 564.00 JT9D-7 30 107.4 * ** B-747-100 750.00 585.00 JT9D-7F 30 107.4 * ** B-747-100 750.00 585.00 JT9D-7FW 30 107.4 * ** B-747-200 812.00 630.00 JT9D-7FW/-7J 30 107.4 * ** DC-08F-54 (QNC PLS QN) 315.00 217.00 JT3D-3B 35 107.3 6,** DC-08-63 (TNC QN) 355.00 275.00 JT3D-7 35 107.3 6,** B-747-200 785.00 630.00 JT9D-7WET 30 107.3 * ** B-747-200 785.00 630.00 JT9D-7A 30 107.3 * ** B-747-200 820.00 630.00 RB211-524B/B2 30 107.3 ** B-747-300 820.00 630.00 RB211-524B2 30 107.3 ** DC-08-52 (QNC PLS QN) 300.00 202.00 JT3D-3B 35 107.2 6,** Page 2 ### Page 273 11/15/01 **MANUFACTURER** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS BOEING** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS BOEING BOEING BOEING** MCDONNELL DOUGLAS BOEING BOEING BOEING AC 36-1H APPENDIX 5 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***APPROACH*** MODEL MTOW 1000# MLW 1000# ENGINE MODEL AP FLAPS AP NOISE LEVEL (EPNdB) NOTES DC-08-55 (QNC PLS QN) 320.30 217.00 JT3D-3B 35 107.2 6,26,** DC-08-61 (QNC PLS QN) 270.00 240.00 JT3D-3B 35 107.2 6,26,** DC-08-61 (QNC PLS QN) 320.30 240.00 JT3D-3B 35 107.2 6,** B-747-100 734.00 564.00 JT9D-3A 30 107.2 * ** DC-08-51 (QNC PLS QN) 276.00 199.50 JT3D-1 35 107.1 6,** DC-08-51 (QNC PLS QN) 276.00 199.50 JT3D-3B 35 107.1 6,** DC-08-51 (QNC PLS QN) 286.00 207.00 JT3D-3B 35 107.1 6,26,** DC-08-53 (QNC QN) 315.00 207.00 JT3D-3B 35 107.1 6,** DC-08-53 (QNC PLS QN) 318.00 207.00 JT3D-3B 35 107.1 6,26,** DC-08-51 (QNC PLS QN) 276.00 199.50 JT3D-3B 35 107.0 6,26,** DC-08-52 (QNC PLS QN) 300.00 202.00 JT3D-3B 35 107.0 6,26,** B-747-SP 702.00 410.00 RB211-524D4 30 107.0 B-747-200 833.00 585.00 RB211-524C2 30 107.0 * B-747-200 820.00 630.00 CF6-50E 30 107.0 DC-08-61F (QNC QN) 309.80 248.00 JT3D-3B 25 106.9 6,26,** B-747-SR 610.00 564.00 JT9D-7A 30 106.9 * B-747-100 750.00 585.00 JT9D-7A 30 106.9 * ** B-747-100 750.00 585.00 JT9D-7WET 30 106.9 * ** Page 3 ### Page 274 11/15/01 **MANUFACTURER BOEING BOEING** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS BOEING BOEING** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS BOEING BOEING BOEING BOEING** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS BOEING** MCDONNELL DOUGLAS AC 36-1H APPENDIX 5 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***APPROACH*** MODEL MTOW 1000# MLW 1000# ENGINE MODEL AP FLAPS AP NOISE LEVEL (EPNdB) NOTES B-747-200 770.00 564.00 JT9D-7 30 106.7 * ** B-747-200 773.00 585.00 JT9D-3AWET 30 106.7 * ** DC-10-30 565.00 411.00 CF6-50A 50 106.6 * DC-10-30 572.00 411.00 CF6-50C/H 50 106.6 DC-10-30 590.00 411.00 CF6-50C1 50 106.6 B-747-200 833.00 630.00 JT9D-7R4G2 30 106.6 ** B-747-300 833.00 630.00 JT9D-7R4G2 30 106.6 DC-08-61 (QNC QN) 309.80 240.00 JT3D-3B 25 106.5 6,26,** DC-08F-54 (QNC QN) 309.80 240.00 JT3D-3B 25 106.5 6,26,** DC-08F-55 (QNC QN) 309.80 240.00 JT3D-3B 25 106.5 6,26,** B-747-200 767.00 564.00 JT9D-3A 30 106.5 * ** B-747-100 750.00 585.00 RB211-524C2 30 106.5 * ** B-747-300 800.00 630.00 CF6-50E2 30 106.5 B-747-200 833.00 630.00 CF6-50E2 30 106.5 DC-10-40 555.00 403.00 JT9D-59A 50 106.4 * DC-10-30 590.00 436.00 CF6-50C2 50 106.4 15 B-727-200 177.60 142.50 JT8D-7FCD 40 106.3 3,16 DC-08F-54/55 (BAC STC: 313.70 240.00 JT3D-3B 35 106.3 6,26,** SA3915NM) Page 4 ### Page 275 APPENDIX 5 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***APPROACH*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL AP FLAPS AP NOISE LEVEL (EPNdB) NOTES 580.00 436.00 CF6-50C2 50 MCDONNELL DOUGLAS DC-10-30 106.0 15 MCDONNELL DOUGLAS MD-10-30 106.3 57 572.00 424.00 CF6-50C2-B 50 BOEING B-747-200 750.00 630.00 JT9D-7F 25 106.0 30 BOEING B-747-200 770.00 630.00 JT9D-7J 25 106.0 30 BOEING B-747-200 820.00 630.00 JT9D-70A 30 106.0 MCDONNELL DOUGLAS MD-10-10 440.00 373.50 CF6-6D 50 105.9 56 MCDONNELL DOUGLAS MD-10-10 440.00 373.50 CF6-6D W/ FSMS 50 105.9 56 BOEING B-727-100 169.50 137.50 JT8D-9FCD 40 105.8 3,17 BOEING B-727-200 178.00 150.00 JT8D-9FCD 30 105.8 3,17 MCDONNELL DOUGLAS DC-10-30 105.8572.00 421.00 CF6-50C2-R 50 BOEING B-707-300B ADV/C ( SHN) 322.30 247.00 JT3D-1-3B(IC) 25 105.7 6,21,** MCDONNELL DOUGLAS DC-10-40 105.7 *530.00 403.00 JT9D-20D 50 BOEING B-747-200 105.7 30710.00 630.00 JT9D-3A 25 MCDONNELL DOUGLAS DC-10-10 105.5 *455.00 363.50 CF6-6D1 50 MCDONNELL DOUGLAS DC-10-10 105.5 *455.00 363.50 CF6-6D 50 MCDONNELL DOUGLAS DC-10-10 105.5 *455.00 363.50 CF6-6D1A 50 BOEING B-747-100 105.5 29734.00 630.00 JT9D-7A 25 BOEING B-747-SR 105.4571.00 564.00 CF6-45A2 30 Page 5 ### Page 276 11/15/01 **MANUFACTURER BOEING BOEING BOEING BOEING** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS BOEING** **MCDONNELL DOUGLAS BOEING BOEING** **MCDONNELL DOUGLAS** MCDONNELL DOUGLAS BOEING BOEING BOEING BOEING BOEING BOEING AC 36-1H APPENDIX 5 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***APPROACH*** MODEL MTOW 1000# MLW 1000# ENGINE MODEL AP FLAPS AP NOISE LEVEL (EPNdB) NOTES B-737-200 NON-ADV. 117.00 101.70 JT8D-9QN 40 105.3 2,17 B-737-200 ADV. 122.50 105.00 JT8D-9QN 40 105.3 2,17 B-707-120B (SHANNON) 258.00 190.00 JT3D-1 30 105.3 21,** B-707-138B (SHANNON) 258.00 190.00 JT3D-1 30 105.3 21,** DC-10-30 590.00 411.00 CF6-50C2 50 105.3 DC-10-30 590.00 411.00 CF6-50C2-B 50 105.3 B-747-300 820.00 630.00 JT9D-70A 30 105.3 ** DC-08-55 (QNC QN) 309.80 217.00 JT3D-3B 25 105.2 6,26,** B-747-200 734.00 630.00 JT9D-7 25 105.2 30 B-747-300 833.00 666.00 CF6-80C2B1 30 105.2 DC-08-55 (BAC STC: 325.00 217.00 JT3D-3B 35 105.1 6,26,** SA3915NM) DC-08-53 (QNC QN) 306.80 207.00 JT3D 25 105.0 6,** B-747-200 734.00 630.00 JT9D-7A 25 105.0 30 B-727-200 172.50 142.50 JT8D-7QN 40 104.9 2,16 B-747-200 833.00 630.00 RB211-524D4 30 104.9 B-747-300 833.00 630.00 RB211-524D4 30 104.9 ** B-720B (SHANNON) 234.00 175.00 JT3D-1 30 104.7 6,** B-720B (SHANNON) 234.00 175.00 JT3D-3B 30 104.7 6,** Page 6 ### Page 277 APPENDIX 5 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***APPROACH*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL MCDONNELL DOUGLAS DC-08-52 (QNC QN) 300.00 202.00 JT3D-3B BOEING B-747-400 875.00 652.00 PW4056 MCDONNELL DOUGLAS DC-08-51 (QNC QN) 286.00 207.00 JT3D-3B MCDONNELL DOUGLAS DC-08-53 (QNC QN) 309.80 207.00 JT3D-3B BOEING B-747-100 710.00 540.00 JT9D-3A BOEING B-727-200 203.10 158.00 JT8D-17QN MCDONNELL DOUGLAS DC-08-51 (QNC QN) 276.00 199.50 JT3D-3B MCDONNELL DOUGLAS MD-11 A-1 630.50 481.50 CF6-80C2D1F BOEING B-747-100 750.00 520.00 JT9D-7F MCDONNELL DOUGLAS MD-11 630.50 481.50 PW4460 MCDONNELL DOUGLAS MD-11 630.50 481.50 PW4462 MCDONNELL DOUGLAS MD-11 A-1 630.50 481.50 PW4460 (-3) MCDONNELL DOUGLAS MD-11 A-1 630.50 481.50 PW4462 (-3) MCDONNELL DOUGLAS MD-10-10 440.00 375.00 CF6-6K MCDONNELL DOUGLAS MD-10-10 440.00 375.00 CF6-6K W/ FSMS BOEING B-747-200 833.00 630.00 JT9D-7Q MCDONNELL DOUGLAS DC-09-30 110.00 101.00 JT8D-7 MCDONNELL DOUGLAS DC-09-30 110.00 101.00 JT8D-9 AP FLAPS AP NOISE LEVEL (EPNdB) NOTES 25 104.7 6,** 30 104.7 25 104.6 6,26,** 25 104.6 6,26,** 25 104.6 29 40 104.5 2,19 25 104.5 6,** 50 104.5 25 104.5 29 50 104.4 50 104.4 50 104.4 50 104.4 50 104.4 56 50 104.4 56 25 104.4 50 104.3 16,24 50 104.3 24 Page 7 ### Page 278 APPENDIX 5 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***APPROACH*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL AP FLAPS AP NOISE LEVEL (EPNdB) NOTES BOEING B-727-100 169.50 137.50 JT8D-1FCD 40 104.3 3 BOEING B-727-100 169.50 137.50 JT8D-7FCD 40 104.3 3,16 MCDONNELL DOUGLAS DC-08-52 (QNC QN) 300.00 202.00 JT3D-3B 25 104.3 6,26,** MCDONNELL DOUGLAS MD-11 618.00 471.50 CF6-80C2 50 104.3 MCDONNELL DOUGLAS DC-08-51 (QNC QN) 276.00 199.50 JT3D-3B 25 104.2 6,26,** BOEING B-747-100 734.00 540.00 JT9D-7 25 104.1 29 MCDONNELL DOUGLAS DC-08-55/F54 (BAC STC: 313.70 217.00 JT3D-3B 35 104.0 6,26,** SA3915NM) BOEING B-737-200 ADV. 128.10 88.00 JT8D-15QN 40 103.8 2,18 MCDONNELL DOUGLAS DC-10-10 455.00 363.50 CF6-6K 50 103.8 * MCDONNELL DOUGLAS DC-10-10 455.00 363.50 CF6-6K2 50 103.8 * BOEING B-747-SP 660.00 475.00 JT9D-7F 30 103.8 BOEING B-747-SP 702.00 475.00 JT9D-7J 30 103.8 BOEING B-747-400 870.00 652.00 RB211-524H 30 103.8 BOEING B-747-400 875.00 652.00 CF6-80C2B1F 30 103.8 BOEING B-747-400 875.00 652.00 RB211-524H2 30 103.8 BOEING B-747-400 875.00 652.00 RB211-524G 30 103.8 BOEING B-747-400 875.00 652.00 CF6-80C2B1F W/N1 MOD 30 103.8 BOEING B-747-400 875.00 652.00 CF6-80C2B5F 30 103.8 Page 8 ### Page 279 11/15/01 **MANUFACTURER** **MCDONNELL DOUGLAS BOEING** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS BOEING** **LOCKHEED BOEING BOEING BOEING BOEING** **MCDONNELL DOUGLAS AIRBUS AIRBUS** **MCDONNELL DOUGLAS BOEING** DASSAULT AIRBUS BOEING AC 36-1H APPENDIX 5 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***APPROACH*** MODEL MD-11 MTOW 1000# 602.50 MLW 1000# 430.00 **ENGINE MODEL CF6-80C2D1F** AP FLAPS 50 AP NOISE LEVEL (EPNdB) 103.6 NOTES B-747-400 875.00 652.00 PW4056 PH3 (FB2B) 30 103.6 DC-08-51 (BAC STC: SA3915NM) DC-08-51 (BAC STC: SA3915NM) B-747-400 276.00 276.00 875.00 199.50 199.50 **652.00 JT3D-1 JT3D-3B PW4056 PKG B/PHASE I 35 35 30** 103.4 103.4 103.4 6,** 6,** L1011-385-1-14/15 466.00 368.00 RB211-524B4 42 103.3 * B-727-200 184.80 142.50 JT8D-9QN 40 103.2 2,17 B-727-200 190.50 142.50 JT8D-15QN 40 103.2 2,18 B-727-200 208.00 142.50 JT8D-17RQN 40 103.2 2,20 B-747-SP 696.00 450.00 RB211-524B2 30 103.2 DC-09-10 90.70 81.70 JT8D-7 50 103.1 24 A300B2-1C 313.00 286.60 CF6-50C2-R 25 103.1 A300B2-203 313.10 286.60 CF6-50-C2 25 103.1 DC-10-15 455.00 363.50 CF6-50C2-F 50 103.1 B-747-400 600.00 564.00 PW4056 30 103.1 FALCON 20-F (M1400) 28.66 27.32 CF700-2D-2 40 103.0 A300B4-103 347.20 295.40 CF6-50-C2 25 103.0 B-767-300 351.00 320.00 JT9D-7R4E 30 103.0 Page 9 ### Page 280 11/15/01 **MANUFACTURER BOEING** **RAYTHEON BOEING BOEING BOEING BOEING BOEING** **LOCKHEED** **LOCKHEED** **LOCKHEED** **LOCKHEED** **LEARJET BOEING** MCDONNELL DOUGLAS BOEING BOEING BOEING AIRBUS AC 36-1H APPENDIX 5 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***APPROACH*** MODEL B-747-400 MTOW 1000# 875.00 MLW 1000# 652.00 **ENGINE MODEL PW4056 PH3 (FB2C)** AP FLAPS 30 AP NOISE LEVEL (EPNdB) 103.0 NOTES HAWKER 125- 600A 25.50 22.00 VIPER 601-22 45 102.9 12 B-707-300B/C (QSI STC: ST00702LA) B-747-SP 336.00 701.00 247.00 465.00 JT3D-3B JT9D-7A 25 30 102.9 102.9 12 B-737-200 ADV. 128.10 79.10 JT8D-17QN 40 102.8 2,19 B-707-100B (QNC) 241.30 190.00 JT3D-1 30 102.8 6,** B-707-100B (QNC) 258.00 190.00 JT3D-3B 30 102.8 6,** L-1011 430.00 358.00 RB211-22B 42 102.8 5 * L-1011-1 430.00 358.00 RB211-22B 42 102.8 5 * L-1011-100 466.00 368.00 RB211-22B 42 102.8 5 * L1011-385-1-14/15 474.00 368.00 RB211-22B 42 102.8 25D 15.00 13.30 CJ610-6 40 102.7 14 B-707-300B/C (QSI STC: ST00702LA) DC-08-63 (BAC II STC: SA4892NM or SA5455NM) B-767-200 336.00 353.00 351.00 247.00 267.00 300.00 JT3D-7 JT3D-7 JT9D-7R4D(A) 25 35 30 102.7 102.7 102.7 12 12 B-767-200 360.00 300.00 JT9D-7R4D(B) 30 102.6 B-767-200 360.00 300.00 JT9D-7R4E 30 102.6 A300B4-203 363.70 299.83 CF6-50-C2 25 102.4 31 Page 10 ### Page 281 11/15/01 **MANUFACTURER** **SABRELINER** **MCDONNELL DOUGLAS BOEING BOEING** **MCDONNELL DOUGLAS** **LOCKHEED** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS FOKKER** **LEARJET** **LEARJET** DASSAULT BOEING BOEING BOEING BOEING BOEING AC 36-1H APPENDIX 5 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***APPROACH*** MODEL SABRELINER 60A/60SC MTOW 1000# 22.70 MLW 1000# 20.60 ENGINE MODEL JT12A-8 AP FLAPS AP NOISE LEVEL (EPNdB) 102.2 NOTES DC-08-62 (BAC II STC: SA4892NM or SA5455NM) B-747-400 335.00 875.00 250.00 652.00 JT3D-7 PW4056 PH3 (FB2C) NR 35 30 102.2 102.1 12 B-737-200 NON-ADV. 109.00 98.00 JT8D-7QN 40 102.1 2,16 DC-08-62 (BAC II STC: SA4892NM) L-1011-500 350.00 510.00 240.00 368.00 JT3D-7 RB211-524B4 35 33 102.0 102.0 12 * DC-09-34 121.00 110.00 JT8D-17 50 101.9 1 DC-09-50 121.00 110.00 JT8D-17 50 101.9 1 DC-09-50 121.00 110.00 JT8D-15 50 101.9 1 F28 MK2000 65.00 SPEY MK555-15 42 101.8 * 24D 13.50 11.90 CJ610-6 40 101.7 14 28/29 15.00 14.30 CJ610-8A 40 101.7 FALCON 20-Basic/D/E 28.66 27.32 CF700-2D-2 40 101.7 B-767-200 360.00 300.00 CF6-80A2 30 101.7 B-767-200 360.00 300.00 CF6-80A 30 101.7 B-767-300 351.00 320.00 CF6-80A 30 101.7 B-767-300 351.00 320.00 CF6-80A2 30 101.7 B-720B (QNC) 234.00 175.00 JT3D-3B 30 101.6 6,** Page 11 ### Page 282 11/15/01 **MANUFACTURER BOEING** **MCDONNELL DOUGLAS** **LOCKHEED FOKKER** **MCDONNELL DOUGLAS** **LOCKHEED BOEING AIRBUS FOKKER** **SABRELINER** **MCDONNELL DOUGLAS BOEING BOEING** **LEARJET** **LEARJET** **MCDONNELL DOUGLAS AIRBUS** MCDONNELL DOUGLAS AC 36-1H APPENDIX 5 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***APPROACH*** MODEL B-720B (QNC) MTOW 1000# 234.00 MLW 1000# 175.00 **ENGINE MODEL JT3D-1** AP FLAPS 30 AP NOISE LEVEL (EPNdB) 101.6 NOTES 6,** DC-08-61 (BAC II STC: SA4892NM) L-1011-500 325.00 496.00 240.00 368.00 JT3D-3B RB211-524B 35 33 101.6 101.5 12 5 * F28 MK4000 73.00 69.50 SPEY MK555-15P 42 101.4 DC-09-34 121.00 110.00 JT8D-15 50 101.4 1 L-1011-200 466.00 368.00 RB211-524B 33 101.4 5 * B-747-400 870.00 652.00 CF6-80C2B1F 25 101.4 A300B4-622R 330.00 275.00 PW-4158 40 101.3 F28 MK1000 65.00 59.00 SPEY MK555-15 42 101.2 SABRELINER 80A/80SC 25.50 22.00 CF700-2D-2 101.1 * DC-09-30 108.00 98.10 JT8D-17 50 101.1 1 B-707-100B (BAC II STC: ST00956LA) B-777-300 200.00 660.00 160.00 524.00 JT3D-1 PW4098 30 30 101.1 101.1 12 25C 15.00 13.30 CJ610-6 40 100.8 13 24/24D 13.50 11.90 CJ610-6 40 100.7 13 DC-08-62 (BAC II STC: SA4892NM) A310-221 348.00 305.60 240.00 267.90 JT3D-3B JT9D-7R4D1 35 40 100.7 100.6 12 DC-09-10 90.70 81.70 JT8D-7/-7A 50 100.4 1 Page 12 ### Page 283 11/15/01 **MANUFACTURER BOEING BOEING BOEING BOEING** **SABRELINER** **SABRELINER BOEING BOEING BOEING** **MCDONNELL DOUGLAS AIRBUS BOEING BOEING BOEING** LOCKHEED BOEING BOEING BOEING AC 36-1H APPENDIX 5 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***APPROACH*** MODEL B-777-300 MTOW 1000# 660.00 MLW 1000# 524.00 **ENGINE MODEL RR TRENT 892** AP FLAPS 30 AP NOISE LEVEL (EPNdB) 100.4 NOTES B-777-300 660.00 524.00 RR TRENT 884 30 100.4 B727-200 (FED EX; STC SA4833NM) B727-200 (FED EX; STC SA4833NM) SABRELINER 75A 177.60 177.60 23.00 154.50 154.50 JT8D-9 w/BURBANK INLET+ FAN CSD JT8D-9 w/BURBANK INLET+CHIN CSD CF700-2D-2 30 30 25 100.3 100.3 100.2 35 35 * SABRELINER 80 23.30 22.00 CF700-2D-2 100.2 * B-737-400 142.50 121.00 CFM56-3-B1 40 100.2 B-737-400 150.00 124.00 CFM56-3C-1 40 100.2 B-737-400 150.00 124.00 CFM56-3B-2 40 100.2 DC-08-62 (BAC II STC: SA5455NM) A310-324 350.00 330.69 240.00 271.16 JT3D-3B PW-4152 35 40 100.2 100.2 12 B-767-300 407.00 320.00 PW 4060 30 100.2 B-767-300 407.00 320.00 PW 4056 30 100.2 B-767-300/300ER 412.00 320.00 PW4062 (FB2B) 30 100.2 L-1011-500 504.00 368.00 RB211-524B3 33 100.2 5 * B-737-300 139.50 121.00 CFM56-3B-2 40 100.1 B-737-300 139.50 121.00 CFM56-3-B1 40 100.1 B-737-500 132.80 114.00 CFM56-3-B1(R) 40 100.0 Page 13 ### Page 284 APPENDIX 5 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***APPROACH*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL AP FLAPS AP NOISE LEVEL (EPNdB) NOTES BOEING B-737-500 139.00 114.00 CFM56-3-B1 40 100.0 AIRBUS A300 B4-605R 385.46 319.38 CF6-80C2A5F 40 100.0 AIRBUS UK 1-11 400 89.50 79.00 SPEY511-14/14W 45 99.9 12 BOEING B727-200 (RAISBECK STC 193.00 161.00 JT8D-15 30 99.9 45 ST00685SE) BOEING B-777-300 660.00 524.00 PW4090 30 99.9 55 BOEING B-767-300 407.00 320.00 RB211-524H 30 99.8 BOEING B-767-300 407.00 320.00 RB211-524G 30 99.8 DASSAULT FALCON 20-Basic/D/E/F 28.66 27.32 CF700-2D-2Q 40 99.7 (M2851) AIRBUS UK 1-11 400 87.00 77.20 SPEY511-14/14W 45 99.7 12 BOEING B727-200 (FED EX; STC SA4833NM) 177.60 154.50 JT8D-9 w/BOEING INLET+FAN CSD 30 99.7 35 BOEING B727-200 (FED EX; STC SA4833NM) 177.60 154.50 JT8D-9 w/BOEING INLET+CHIN CSD 30 99.7 35 BOEING B-757-200 240.00 210.00 RB211-535C 25 99.6 BOEING B-777-200 545.00 470.00 RR TRENT 875 30 99.5 BOEING B-777-200 555.00 470.00 RR TRENT 877 30 99.5 BOEING B-777-200 632.50 470.00 RR TRENT 884 30 99.5 BOEING B-777-200 656.00 470.00 RR TRENT 895 30 99.5 BOEING B-777-200 656.00 470.00 RR TRENT 892 30 99.5 FOKKER F28 MK3000 71.00 64.00 SPEY MK555-15H 42 99.4 Page 14 ### Page 285 11/15/01 **MANUFACTURER FOKKER** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS BOEING BOEING BOEING** **MCDONNELL DOUGLAS BOEING BOEING BOEING BOEING** **LEARJET** **LEARJET** **LEARJET** MCDONNELL DOUGLAS BOEING BOEING AC 36-1H APPENDIX 5 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***APPROACH*** MODEL MTOW 1000# MLW 1000# ENGINE MODEL AP FLAPS AP NOISE LEVEL (EPNdB) NOTES **73.00 65.80 SPEY MK555-15H 42 F28 MK4000 99.4** 114.00 102.00 JT8D-9 50 DC-09-30 99.4 1 DC-09-40 114.00 102.00 JT8D-11 50 99.4 1 DC-09-40 114.00 102.00 JT8D-15 50 99.4 1 B727-200 (FED EX; STC 178.00 161.00 JT8D-7 w/BURBANK 30 99.4 35 SA4833NM) INLET+ FAN CSD B-727-200 RE (ROHR STC 203.10 164.00 JT8D-217C/JT8D-17A 30 99.3 23 SA4363NM) B-777-200 656.00 470.00 PW4090 30 99.2 55 DC-09-34 110.00 101.00 JT8D-9 50 99.1 1 B727-100 (FED EX; STC 175.50 154.50 JT8D-7 w/BURBANK 30 99.1 35 SA3993NM) INLET+CHIN CSD B727-100 (FED EX; STC 175.50 154.50 JT8D-7 w/BOEING 30 99.1 35 SA3993NM) INLET+CHIN CSD B727-200 (FED EX; STC 178.42 154.50 JT8D-7 w/BURBANK 30 99.1 35 SA4833NM) INLET+CHIN CSD B-727-200 RE (ROHR STC 209.42 164.00 JT8D-217C/JT8D-15 30 99.1 23,61 SA4363NM) 25/25B/C Raisb MK II 15.00 13.30 CJ610 40 99.0 16.00 13.30 CJ610-6 40 25 99.0 25B/C/D/F XR Dee Hwd 16.30 13.30 CJ610-6/8A 40 99.0 114.00 102.00 JT8D-15 50 DC-09-30 99.0 1 B727-200 (FED EX; STC 177.60 154.50 JT8D-7 w/BOEING 30 99.0 35 SA4833NM) INLET+FAN CSD B727-200 (FED EX; STC 177.60 154.50 JT8D-7 w/BOEING 30 99.0 35 SA4833NM) INLET+CHIN CSD Page 15 ### Page 286 APPENDIX 5 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***APPROACH*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL AP FLAPS AP NOISE LEVEL (EPNdB) NOTES BOEING B-727-200 RE (ROHR STC 198.50 162.00 JT8D-217C/JT8D-9 30 99.0 23,60 SA4363NM) BOEING B-727-200 RE (ROHR STC 198.70 162.00 JT8D-219/JT8D-9 30 99.0 7,23,63 SA4363NM) BOEING B-727-200 RE (ROHR STC 198.70 162.00 JT8D-219/JT8D-9 30 99.0 23,60 SA4363NM) BOEING B-727-200 RE (ROHR STC 198.70 162.00 JT8D-219/JT8D-15 30 99.0 7,23,64 SA4363NM) BOEING B-727-200 RE (ROHR STC 209.50 162.00 JT8D-217C/JT8D-17 30 99.0 23,62 SA4363NM) BOEING B-777-200 535.00 445.00 PW4074 30 99.0 BOEING B-777-200 545.00 460.00 PW4077 30 99.0 BOEING B727-100 (FED EX; STC SA3993NM) 174.50 142.50 JT8D-9 w/BOEING INLET+CHIN CSD 30 98.9 35 BOEING B-727-200 RE (ROHR STC 198.70 162.00 JT8D-219/JT8D-17 30 98.9 23 SA4363NM) BOEING B-777-200 535.00 445.00 PW4090 at PW4074 rating 30 98.9 55 BOEING B-777-200 545.00 445.00 PW4090 at PW4077 rating 30 98.9 55 BOEING B727-100 (FED EX; STC SA3993NM) 174.50 142.50 JT8D-9 w/BURBANK INLET+CHIN CSD 30 98.8 35 AIRBUS A310-304 352.74 286.60 CF6-80C2A2 40 98.8 BOEING B-737-500 132.80 114.00 CFM56-3 w/HWFAP 40 98.7 BOEING B-737-500 139.00 114.00 CFM56-3 w/HWFAP 40 98.7 BOEING B-767-400 450.00 350.00 CF6-80C2B8F 30 98.7 AIRBUS A330-301 507.06 418.88 CF6-80E1A2 32 98.7 BOEING B-737-400 150.00 124.00 CFM56-3 w/HWFAP 40 98.6 Page 16 ### Page 287 11/15/01 **MANUFACTURER BOEING BOEING BOEING BOEING BOEING BOEING BOEING BOEING BOEING** **MCDONNELL DOUGLAS BOEING** **SABRELINER BOEING BOEING** **MCDONNELL DOUGLAS BOEING** SABRELINER BOEING AC 36-1H APPENDIX 5 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***APPROACH*** MODEL MTOW 1000# MLW 1000# ENGINE MODEL AP FLAPS AP NOISE LEVEL (EPNdB) NOTES B-767-200/200ER 387.00 300.00 PW4060 30 98.6 B-737-200 ADV (NORDAM; 124.50 107.00 JT8D-9 40 98.6 27,41 STC SA5730NM) B-737-200 ADV (NORDAM; 126.50 107.00 JT8D-17 40 98.6 27 STC SA5730NM) B-737-200 ADV (NORDAM; 126.70 107.00 JT8D-15 40 98.6 27,42 STC SA5730NM) B-737-300 139.50 121.00 CFM56-3 w/HWFAP 40 98.6 B-737-300 139.50 121.00 CFM56-3 w/HWFAP 40 98.6 B-737-400 142.50 124.00 CFM56-3 w/HWFAP 40 98.6 B-737-400 150.00 124.00 CFM56-3 w/HWFAP 40 98.6 B727-200 (FED EX; STC 201.00 166.00 JT8D-15 w/BURBANK 30 98.6 27 SA5839NM) INLET+ FAN CSD 328.00 258.00 CFM56-2-C1 50DC-08-71 98.6 * 400.00 300.00 PW 4056 30B-767-200 98.6 20.20 JT12A-8 24SABRELINER 60 98.5 * B727-200 (FED EX; STC 191.20 160.00 JT8D-9 w/BURBANK 30 98.5 27 SA5839NM) INLET+CHIN CSD B727-200 (FED EX; STC 191.20 160.00 JT8D-9 w/BURBANK 30 98.5 27 SA5839NM) INLET+ FAN CSD 355.00 275.00 CFM56-2-C1 50DC-08-73 98.5 * 407.00 320.00 CF6-80C2B6F 30B-767-300 98.5 20.20 17.50 JT12A-8 25SABRELINER 40 98.4 B-727-100 (Dee Howard) 169.50 137.50 TAY 651-54 40 98.4 Page 17 ### Page 288 11/15/01 **MANUFACTURER BOEING BOEING BOEING BOEING BOEING** **GULFSTREAM** **MCDONNELL DOUGLAS BOEING BOEING BOEING BOEING** MCDONNELL DOUGLAS BOEING BOEING BOEING BOEING BOEING BOEING AC 36-1H APPENDIX 5 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***APPROACH*** MODEL B727-100 (FED EX; STC SA3993NM) B727-200 (FED EX; STC SA5839NM) B727-200 (FED EX; STC SA5839NM) B-767-300 MTOW 1000# 169.50 204.50 197.50 407.00 MLW 1000# 142.50 159.00 161.00 320.00 ENGINE MODEL JT8D-9 w/BOEING INLET+FAN CSD JT8D-17 w/BURBANK INLET+CHIN OR FAN CSD JT8D-17R w/BURBANK INLET+CHIN OR FAN CSD CF6-80C2-B6 AP FLAPS 30 30 30 30 AP NOISE LEVEL (EPNdB) 98.4 98.4 98.4 98.4 NOTES 35 27 27 B-767-300 407.00 320.00 CF6-80C2-B4 30 98.4 G-II GULFSTREAM 65.50 58.50 SPEY 511-8 39 98.3 12 DC-08-71 325.00 240.00 CFM-56-2C5 98.3 * B-777-200 632.50 470.00 GE90-85B (BLK IV) 30 98.3 54 B-777-200 656.00 470.00 GE90-90B (BLK IV) 30 98.3 54 B-777-200 656.00 470.00 GE90-94B BLK IV) 30 98.3 54 B727-100 (FED EX; STC SA3993NM) DC-08-72 169.50 350.00 142.50 250.00 JT8D-7 w/BURBANK INLET+ FAN CSD CFM56-2-C1 30 50 98.2 98.2 35 * B-767-200 351.00 285.00 PW4052 30 98.2 B-737-200 (AVAERO;STC ST223CH) B-737-200 ADV(AVAERO;STC ST223CH) B727-200 (FED EX; STC SA5839NM) B727-200 (FED EX; STC SA5839NM) B-757-200 117.00 119.50 199.05 199.05 255.50 90.00 95.00 166.00 166.00 210.00 JT8D-15 JT8D-9 JT8D-15 w/BOEING INLET+CHIN CSD JT8D-15 w/BOEING INLET+FAN CSD PW 2037 40 40 30 30 30 98.1 98.1 98.1 98.1 98.1 35,42 35,41 27 27 Page 18 ### Page 289 APPENDIX 5 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***APPROACH*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL AP FLAPS AP NOISE LEVEL (EPNdB) NOTES BOEING B-757-200 255.50 210.00 PW 2040 30 98.1 BOEING B-777-200 545.00 460.00 GE90-77B (BLK IV) 30 98.1 54 BOEING B-777-200 545.00 460.00 GE90-76B (BLK IV) 30 98.1 54 LEARJET 24B/D Raisbeck MK II 13.50 11.88 CJ610 40 98.0 LEARJET 23 Raisbeck MK II 12.50 11.90 CJ610-1/-4 98.0 LEARJET 24 Raisbeck MK II 13.00 11.90 CJ610-1/-4 98.0 BOEING B-737-200 (AVAERO;STC 121.50 107.00 JT8D-9 40 98.0 27,41 ST223CH) BOEING B727-100 (FED EX; STC SA3993NM) 169.50 142.50 JT8D-7 w/BOEING INLET+FAN CSD 30 98.0 35 BOEING B727-200 (FED EX; STC SA5839NM) 196.00 166.00 JT8D-9 w/BOEING INLET+CHIN CSD 30 98.0 27 BOEING B727-200 (FED EX; STC SA5839NM) 196.00 166.00 JT8D-9 w/BOEING INLET+FAN CSD 30 98.0 27 BOEING B727-200 (FED EX; STC SA5839NM) 203.10 166.00 JT8D-17 w/BOEING INLET+CHIN OR FAN CSD 30 98.0 27 AIRBUS A330-321 507.06 418.88 PW4164 32 98.0 AIRBUS A330-322 507.06 418.88 PW4168 32 98.0 BOEING B-767-300/300ER 412.00 320.00 PW4062 PH3 (FB2C) NRI 30 97.9 BOEING B-767-300/300ER 412.00 320.00 PW4060 PH3 (FB2C) NRI 30 97.9 AIRBUS UK 1-11 200 80.00 71.00 SPEY 506-14 45 97.8 12 BOEING B-777-200 545.00 460.00 GE90-77B 30 97.8 53 BOEING B-777-200 545.00 460.00 GE90-76B 30 97.8 53 Page 19 ### Page 290 APPENDIX 5 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***APPROACH*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL AP FLAPS AP NOISE LEVEL (EPNdB) NOTES BOEING B-777-200 632.50 460.00 GE90-85B 30 97.8 53 BOEING B-777-200 656.00 460.00 GE90-90B 30 97.8 53 BOEING B-737-200 ADV(AVAERO;STC 119.50 88.00 JT8D-15 40 97.7 35,42 ST223CH) BOEING B-737-200 ADV(AVAERO;STC 121.50 107.00 JT8D-9 40 97.7 27,41 ST223CH) BOEING B-737-200 ADV(AVAERO;STC 125.00 107.00 JT8D-17 40 97.7 27 ST223CH) BOEING B-737-400 142.50 124.00 CFM56-3 w/HWFAP 40 97.7 38 BOEING B-737-400 150.00 124.00 CFM56-3 w/HWFAP 40 97.7 38 BOEING B-737-400 150.00 124.00 CFM56-3 w/HWFAP 40 97.7 38 BOEING B-757-200 187.00 198.00 PW 2037 30 97.7 BOEING B-737-500 132.80 114.00 CFM56-3 w/HWFAP 40 97.6 38 BOEING B-737-500 139.00 114.00 CFM56-3 w/HWFAP 40 97.6 38 BOEING B-737-300 139.50 121.00 CFM56-3 w/HWFAP 40 97.6 38 BOEING B-737-300 139.50 121.00 CFM56-3 w/HWFAP 40 97.6 38 BOEING B-767-300/300ER 412.00 320.00 PW4056 PH3 (FB2C) NRI 30 97.6 BAE SYSTEMS (BAe) 146-300 101.50 88.50 LF 507-1H/-1F 33 97.6 BAE SYSTEMS (AVRO) 146-RJ 100 101.50 88.50 LF 507-1F 33 97.6 BOEING B727-200 (RAISBECK STC 166.40 153.30 JT8D-9 25 97.6 17,34,43 ST00399SE) BOEING B727-200 (FED EX; STC SA5839NM) 197.00 154.50 JT8D-17R w/BOEING INLET+CHIN OR FAN CSD 30 97.6 27 Page 20 ### Page 291 11/15/01 **MANUFACTURER** **BAE SYSTEMS (AVRO)** **BAE SYSTEMS (AVRO)** **GULFSTREAM** **BAE SYSTEMS (AVRO)** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS BOEING BOEING BOEING BOEING BOEING AIRBUS AIRBUS** DASSAULT BOEING BOEING BOEING BOEING AC 36-1H APPENDIX 5 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***APPROACH*** MODEL 146-RJ 70 MTOW 1000# 90.00 MLW 1000# 83.50 **ENGINE MODEL LF 507-1F** AP FLAPS 33 AP NOISE LEVEL (EPNdB) 97.5 NOTES 146-RJ 70 95.00 83.50 LF 507-1F 33 97.5 4 G-IIB/G-III 69.70 58.50 SPEY 511-8 39 97.3 12 146-RJ 85 97.00 85.00 LF 507-1F 33 97.3 DC-09-30 108.00 99.00 JT8D-7A 50 97.3 1 DC-09-30 110.00 101.00 JT8D-7 50 97.3 1 B-757-200 255.50 210.00 PW 2040QFC 30 97.3 59 B-757-200 255.50 210.00 PW 2037QFC 30 97.3 59 B727-100 (RAISBECK STC ST00448SE) B727-100 (DUGAN AIR STC) 172.60 174.50 142.50 142.50 JT8D-7 JT8D-7 25 26 97.2 **97.2 16,43 B727-200 (RAISBECK STC ST00555SE) A340-312** 179.70 595.24 166.00 **440.92 JT8D-9 CFM56-5C3 30 32** 97.2 97.2 34,44 A340-212 595.25 440.92 CFM56-5C3 32 97.2 FALCON 50 (M1230) 40.78 35.71 TFE731-3-1C 48 97.1 B-737-200 (AVAERO;STC ST223CH) B-737-200 ADV(AVAERO;STC ST223CH) B727-200 (DUGAN AIR STC) 128.10 128.10 190.50 93.00 98.00 164.00 JT8D-15 JT8D-15 JT8D-9 40 40 26 97.1 97.1 97.0 27,42 27,42 B727-200 (DUGAN AIR STC) 209.41 164.00 JT8D-15 26 97.0 Page 21 ### Page 292 APPENDIX 5 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***APPROACH*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL AP FLAPS AP NOISE LEVEL (EPNdB) NOTES LOCKHEED 1329-23 (AIRESEARCH) 43.80 TFE731-3-1E 59 96.9 * ** LOCKHEED 1329-23A/D/E (STAR 3 STC 44.25 36.00 TFE731-3-1R 59 96.9 ST00258SE) LOCKHEED 1329-25 (AIRESEARCH) 44.50 36.00 TFE731-3 96.9 * ** LOCKHEED 1329-25 (STAR 3 STC# 44.50 36.00 TFE731-3-1R 59 96.9 ST00259SE) BAE SYSTEMS (AVRO) 146-RJ 85 89.50 77.50 LF 507-1F 33 96.9 BOEING B-737-800 174.20 146.30 CFM56-7B24/2 DAC 40 96.8 50 BOEING B-737-800 174.20 146.30 CFM56-7B26/2 DAC 40 96.8 50 BOEING B-737-800 174.20 146.30 CFM56-7B27/2 DAC 40 96.8 50 BOEING B-737-800 174.20 146.30 CFM56-7B27/2B1 DAC 40 96.8 50 LEARJET 24D 13.50 11.90 CJ610-6 40 96.7 BOEING B-737-200 (AVAERO;STC 128.10 88.00 JT8D-17 40 96.7 27 ST223CH) BOEING B-767-200/200ER 395.00 300.00 PW4056 PH3 (FB2C) NRI 30 96.6 BOEING B-767-200/200ER 395.00 300.00 PW4060 PH3 (FB2C) NRI 30 96.6 AIRBUS A320-231 162.00 142.20 V2500.A1 40 96.6 BOEING B-737-800W 174.20 146.30 CFM56-7B27/2B1 DAC 40 96.6 50,52 BOEING B-737-800W 174.20 146.30 CFM56-7B27/2 DAC 40 96.6 50,52 BOEING B-737-800W 174.20 146.30 CFM56-7B26/2 DAC 40 96.6 50,52 BOEING B-737-800W 174.20 146.30 CFM56-7B24/2 DAC 40 96.6 50,52 Page 22 ### Page 293 APPENDIX 5 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***APPROACH*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL AP FLAPS AP NOISE LEVEL (EPNdB) NOTES AIRBUS A321-211 205.02 171.51 CFM56-5B3/P; Mod. No. 25 96.6 27772 RAYTHEON HAWKER 125- 800 27.40 23.35 TFE731-5R-1H 45 96.5 RAYTHEON HAWKER 125- 800A 27.40 23.35 TFE731-5R-1H 45 96.5 25 BOEING B-737-800 174.20 146.30 CFM56-7B24 40 96.5 BOEING B-737-800/BBJ 2 174.20 146.30 CFM56-7B26; -7B26/B1 40 96.5 BOEING B-737-800/BBJ 2 174.20 146.30 CFM56-7B27/B1; -7B27/B2 40 96.5 BOEING B-737-800/BBJ 2 174.20 146.30 CFM56-7B27; -7B27/B3 40 96.5 BOEING B-767-300 288.70 280.00 CF6-80C2B2 30 96.5 BOEING B-767-200/200ER 360.00 300.00 CF6-80C2B4F 30 96.5 BOEING B-767-200/200ER 360.00 300.00 CF6-80C2B2F 30 96.5 BOEING B-767-200/200ER 387.00 300.00 CF6-80C2B4F W/N1 MOD 30 96.5 BOEING B-767-200/200ER 400.00 300.00 CF6-80C2B6F W/N1 MOD 30 96.5 AIRBUS A320-211 162.00 142.20 CFM56-5A1 35 96.4 BOEING B-737-900 174.20 147.30 CFM56-7B27/B1 40 96.4 BOEING B-737-900 174.20 147.30 CFM56-7B24 40 96.4 BOEING B-737-900 174.20 147.30 CFM56-7B26 40 96.4 BOEING B-737-900 174.20 147.30 CFM56-7B27 40 96.4 BOEING B-767-200 351.00 300.00 CF6-80C2-B2 30 96.4 Page 23 ### Page 294 11/15/01 **MANUFACTURER BOEING** **RAYTHEON** **RAYTHEON** RAYTHEON BOEING BOEING BOEING BOEING BOEING BOEING BOEING BOEING BOEING BOEING BOEING BOEING BOEING MCDONNELL DOUGLAS AC 36-1H APPENDIX 5 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***APPROACH*** MODEL B-767-200 MTOW 1000# 387.00 MLW 1000# 300.00 **ENGINE MODEL CF6-80C2-B4** AP FLAPS 30 AP NOISE LEVEL (EPNdB) 96.4 NOTES HAWKER 125- 3A 21.70 20.00 TFE731-3-1H 45 96.3 HAWKER 125- 600A 25.50 22.00 TFE731-3-1H 45 96.3 HAWKER 125- 700A 25.50 22.00 TFE731-3-1H 45 96.3 33 B-737-200 (AVAERO;STC ST223CH) B-737-200 ADV(AVAERO;STC ST223CH) B-737-200 ADV(AVAERO;STC ST223CH) B-737-800W 118.50 119.50 124.50 174.20 107.00 107.00 107.00 **146.30 JT8D-9 JT8D-9 JT8D-15 CFM56-7B24 30 30 30 40** 96.3 96.3 96.3 96.3 35,41 35,41 35,42 52 B-737-800W/BBJ 2 174.20 146.30 CFM56-7B26; -7B26/B1 40 96.3 52 B-737-800W/BBJ 2 174.20 146.30 CFM56-7B27/B1; -7B27/B2 40 96.3 52 B-737-800W/BBJ 2 174.20 146.30 CFM56-7B27; -7B27/B3 40 96.3 52 B-737-200 ADV (NORDAM; STC ST00131SE) B-737-200 ADV (NORDAM; **STC ST00131SE) B-737-700** 117.00 118.50 154.50 107.00 107.00 129.20 JT8D-7 w/LGW-N HUSHKIT JT8D-9 w/LGW-N **HUSHKIT CFM56-7B26/2 DAC 30 30 40** 96.2 96.2 96.2 40 36 50 B-737-700 154.50 129.20 CFM56-7B24/2 DAC 40 96.2 50 B-737-700 154.50 129.20 CFM56-7B20/2 DAC 40 96.2 50 B-737-700 154.50 129.20 CFM56-7B22/2 DAC 40 96.2 50 DC-09-30(ABS/SA1613GL) 105.00 101.00 JT8D-9/9A 40 96.1 Page 24 ### Page 295 11/15/01 **MANUFACTURER BOEING BOEING BOEING** **RAYTHEON** **RAYTHEON** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS** DASSAULT BOEING BOEING BOEING BOEING BOEING AC 36-1H APPENDIX 5 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***APPROACH*** MODEL MTOW 1000# MLW 1000# ENGINE MODEL AP FLAPS AP NOISE LEVEL (EPNdB) NOTES B-737-700 IGW/-700C 171.00 134.00 CFM56-7B24 40 96.1 51 B-737-700 IGW/-700C/BBJ 171.00 134.00 CFM56-7B26; -7B26/B1 40 96.1 51 B-737-700 IGW/BBJ 171.00 134.00 CFM56-7B27/B3 40 96.1 51 HAWKER 125- 1A 21.70 19.60 TFE731-3-1H 45 96.0 HAWKER 125- 700A 25.50 22.00 TFE731-3-1H 45 96.0 25,33 DC-09-30(ABS/SA1613GL) 105.00 101.00 JT8D-7/7A/7B 40 96.0 DC-09-30 (ABS;STC SA1613GL) 107.00 101.00 JT8D-9/9A 40 96.0 DC-09-30(ABS/SA1785GL) 107.00 101.00 JT8D-7/7A/7B 40 96.0 DC-09-30(ABS/SA1785GL) 107.00 101.00 JT8D-9/9A 40 96.0 DC-09-31/32/32F/33F(ABS;STC 107.00 101.00 JT8D-7/7A/7B 40 96.0 SA1613GL) DC-09-30 (ABS) 111.00 101.00 JT8D-11 40 96.0 DC-09-30(ABS) 111.00 101.00 JT8D-11 40 96.0 12 FALCON 20-G (M2500) 32.00 27.56 ATF3-6-2C 40 95.9 B-737-200 ADV (NORDAM; 118.70 107.00 JT8D-9 w/LGW HUSHKIT 30 95.9 36 STC ST00131SE) B-737-200 ADV (NORDAM; 120.50 107.00 JT8D-17/-17A w/LGW 30 95.9 STC ST00131SE) HUSHKIT B-737-200 ADV (NORDAM; 121.60 107.00 JT8D-15 w/LGW HUSHKIT 30 95.9 37 STC ST00131SE) B-737-200 ADV (NORDAM; 122.90 107.00 JT8D-9 w/LGW-L 30 95.9 36 STC ST00131SE) HUSHKIT B-737-200 ADV (NORDAM; 125.90 107.00 JT8D-15 w/LGW-L 30 95.9 37 STC ST00131SE) HUSHKIT Page 25 ### Page 296 11/15/01 **MANUFACTURER BOEING BOEING BOEING BOEING** RAYTHEON BAE SYSTEMS (BAe) BOEING BOEING BOEING BOEING BOEING AIRBUS AIRBUS **RAYTHEON** **RAYTHEON** MCDONNELL DOUGLAS BAE SYSTEMS (BAe) BAE SYSTEMS (BAe) AC 36-1H APPENDIX 5 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***APPROACH*** MODEL B-737-700 MTOW 1000# 154.50 MLW 1000# 129.20 **ENGINE MODEL CFM56-7B20** AP FLAPS 40 AP NOISE LEVEL (EPNdB) 95.9 NOTES B-737-700 154.50 129.20 CFM56-7B26 40 95.9 B-737-700 154.50 129.20 CFM56-7B22 40 95.9 B-737-700 154.50 129.20 CFM56-7B24 40 95.9 C-29A 28.00 23.35 TFE731-5R-1H 45 95.8 146-200A 93.00 81.00 ALF502R-5 33 95.8 B-737-200 (NORDAM;STC ST00131SE) B-737-200 (NORDAM;STC ST00131SE) B-737-600 B-737-600 119.50 119.50 143.50 143.50 103.00 103.00 120.50 120.50 JT8D-15 w/LGW-L HUSHKIT JT8D-15 w/LGW HUSHKIT CFM56-7B/2 DAC (B18 derate) CFM56-7B20/2 DAC 30 30 40 40 95.8 95.8 95.8 95.8 37 37 50 50 B-737-600 143.50 120.50 CFM56-7B22/2 DAC 40 95.8 50 A320-214 182.80 150.00 CFM56-5B4/P 35 95.8 A321-231 205.02 171.51 V2533A5 25 95.8 HAWKER 125- 3A/RA 23.60 20.00 TFE731-3-1H 45 95.7 HAWKER 125- 400A 23.60 20.00 TFE731-3-1H 45 95.7 DC-09-20 (ABS;STC SA1613GL) 100.00 93.40 JT8D-9/9A 40 95.7 146-100A 84.00 77.50 ALF502R-5 33 95.6 146-200A 89.50 77.50 ALF502R-3 33 95.6 Page 26 ### Page 297 11/15/01 MANUFACTURER BAE SYSTEMS (BAe) BAE SYSTEMS (BAe) **MCDONNELL DOUGLAS BOEING BOEING BOEING BOEING BOEING BOEING BOEING BOEING BOEING** **LEARJET** **LEARJET** **LEARJET** **LEARJET** **DASSAULT** DASSAULT AC 36-1H APPENDIX 5 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***APPROACH*** MODEL MTOW 1000# MLW 1000# ENGINE MODEL AP FLAPS AP NOISE LEVEL (EPNdB) NOTES **89.50 77.50 ALF502R-3A 33 146-300A 95.6 146-200A 95.6** **97.50 84.50 ALF502R-5 33 DC-09-10 (AIRWELD STC 108.00 99.00 JT8D-9A 40 95.6 12** ST00934LA) B-737-600 143.50 120.50 CFM56-7B22 40 95.5 B-737-600 143.50 120.50 CFM56-7B20 40 95.5 B-737-600 143.50 120.50 CFM56-7B18 40 95.5 B727-100 RE (ROHR STC 174.50 142.50 JT8D-217C/JT8D-9 30 95.4 23 SA4363NM) **B727-100 RE (ROHR STC 174.50 142.50 JT8D-219/JT8D-7B 30 95.4 23** SA4363NM) **B727-100 RE (ROHR STC 174.50 142.50 JT8D-219/JT8D-9 30 95.4 23** SA4363NM) B-757-300 95.4 58275.00 224.00 RB211-535E4-B 30 B-757-300 95.4 58275.00 224.00 RB211-535-E4 30 B-757-300 95.4 58275.00 224.00 RB211-535E4-C 30 24F-A 95.312.50 11.90 CJ610-6 40 24E 95.312.90 11.90 CJ610-6 40 24F 95.313.50 11.90 CJ610-6 40 25D/25F 15.00 13.30 CJ610-6/8A 40 95.2 FALCON 10 95.219.30 17.64 TFE731-2-1C 52 FALCON 50 (M2193) 40.79 35.72 TFE731-40-1 48 95.2 Page 27 ### Page 298 11/15/01 **MANUFACTURER** DASSAULT BAE SYSTEMS (BAe) BOEING BOEING BOEING BOEING BAE SYSTEMS (BAe) **MCDONNELL DOUGLAS BOEING BOEING BOEING AIRBUS AIRBUS AIRBUS AIRBUS** DASSAULT CESSNA CESSNA AC 36-1H APPENDIX 5 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***APPROACH*** MODEL FALCON 50 ( M1810) MTOW 1000# 40.79 MLW 1000# 35.72 **ENGINE MODEL TFE731-40-1** AP FLAPS 48 AP NOISE LEVEL (EPNdB) 95.2 NOTES 146-100A 82.25 73.35 ALF502R-3A 33 95.2 B-757-200 255.50 210.00 RB211-535E4-B 30 95.2 58 B-757-200 255.50 210.00 RB211-535E4-B 30 95.2 B-757-200 255.50 210.00 RB211-535-E4 30 95.2 58 B-757-200 255.50 210.00 RB211-535-E4 30 95.2 146-100A 76.00 72.35 ALF502R-3 33 95.1 DC-09-10 (ABS) 90.70 81.70 JT8D-7/7A/7B 40 95.0 6 B-737-200 (AVAERO;STC ST223CH) B-737-200 ADV(AVAERO;STC ST223CH) B-737-200 ADV(AVAERO;STC ST223CH) A319-113 128.10 128.10 128.10 158.73 107.00 107.00 107.00 **149.91 JT8D-17 JT8D-17 JT8D-15 CFM56-5A4 30 30 30 40** 94.8 94.8 94.8 94.8 27 27 27,42 A319-114 163.14 149.91 CFM56-5A5 40 94.8 A319-131 158.73 149.91 V2522-A5 40 94.5 A319-112 166.44 149.91 CFM56-5B6/P 40 94.4 FALCON 200 (M5634) 32.00 28.88 ATF3-6A-4C 40 94.2 650 CITATION III 22.00 20.00 TFE731-3B-100S 37 93.8 22 650 CITATION VI 22.45 20.00 TFE731-3C-100S 40 93.8 Page 28 ### Page 299 11/15/01 **MANUFACTURER** **AIRBUS UK** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS** **LEARJET** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS** **LEARJET CESSNA** **DASSAULT** **ISRAEL AIRCRAFT FOKKER** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS** **ISRAEL AIRCRAFT** **GULFSTREAM** ISRAEL AIRCRAFT AC 36-1H APPENDIX 5 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***APPROACH*** MODEL MTOW 1000# MLW 1000# ENGINE MODEL AP FLAPS AP NOISE LEVEL (EPNdB) NOTES 1-11 400 (QTV STC: ST02167AT) 81.90 78.00 SPEY511-14/14W 26 93.8 MD-80 160.00 150.00 JT8D-217A 40 93.7 10 MD-80 160.00 150.00 JT8D-217C 40 93.7 10 MD-80 160.00 150.00 JT8D-219 40 93.7 10 45 20.50 19.20 TFE731-20R-1B or (-20AR­ 40 93.4 1B) MD-87 149.50 130.00 JT8D-217A 40 93.3 10 MD-87 149.50 130.00 JT8D-217C 40 93.3 10 MD-87 149.50 130.00 JT8D-219 40 93.3 10 31A 17.00 16.00 TFE731-2-3B 40 93.1 560XL EXCEL 20.00 18.70 PW545A 35 93.1 FALCON 2000 36.50 33.00 CFE738-1-1B 40 93.1 1124 WESTWIND 22.90 19.00 TFE731-3-1G 40 93.0 F100 98.00 88.00 TAY MK650-15 42 93.0 MD-80 149.50 130.00 JT8D-209 40 92.9 10 MD-80 149.50 130.00 JT8D-217 40 92.9 10 1124A WESTWIND 2 23.50 19.00 TFE731-3-1G 40 92.8 * G200 34.85 28.00 PW306A 40 92.7 46 Galaxy 34.85 28.00 PW306A 40 92.7 Page 29 ### Page 300 APPENDIX 5 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***APPROACH*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL AP FLAPS AP NOISE LEVEL (EPNdB) NOTES 16.50 15.30 TFE731-2-3B 40LEARJET 31 92.6 * 45.41 41.22 AE3007A 45EMBRAER EMB-145ER 92.6 EMBRAER EMB-145EP 46.29 41.22 AE3007A 45 92.6 * BOMBARDIER CL-600-2C10 (CRJ700) 75.00 66.90 CF34-8C1 45 92.6 EMBRAER EMB-145LR 48.50 42.54 AE3007A1/1 45 92.5 LEARJET 55C 21.50 17.00 TFE731-3AR-3B 40 92.4 * LEARJET 55C 21.50 18.00 TFE731-3AR-2B 40 92.4 * ISRAEL AIRCRAFT 1125 ASTRA SPX 24.65 20.70 TFE731-40R 40 92.3 **EMBRAER EMB-135LR 44.09 40.78 AE3007A1/3 45 92.3** **DASSAULT FALCON 900EX (M3000) 49.00 44.50 TFE731-60-1 40 92.3** LEARJET 35/36 18.00 14.30 TFE731-2-2B 40 92.2 * **10.40 9.70 FJ44-1A 35CESSNA 525 CESSNA JET 92.1** 34.52 31.72 PW306B 32FAIRCHILD DORNIER DORNIER 328-300 Mod 10 92.1 BOMBARDIER CL-600-2B19 (CRJ) 53.00 47.00 CF-34-3A1 45 92.1 BOMBARDIER CL-600-2B19 (CRJ) 53.00 47.00 CF-34-3B1 45 92.1 BOEING B-717-200 121.00 110.00 BR700-715C1-30 (MP) 40 92.1 49 BOEING B-717-200 121.00 110.00 BR700-715A1-30 (MP) 40 92.1 49 12.50 11.60 FJ44-2A 30RAYTHEON 390 PREMIER 92.0 Page 30 ### Page 301 11/15/01 **MANUFACTURER** **RAYTHEON** **GULFSTREAM** **GULFSTREAM** **MCDONNELL DOUGLAS** **MCDONNELL DOUGLAS** **DASSAULT** **DASSAULT** **DASSAULT** **BOMBARDIER** **BOMBARDIER** **BOMBARDIER BOEING BOEING CESSNA BEECH** **MITSUBISHI** **LEARJET** LEARJET AC 36-1H APPENDIX 5 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***APPROACH*** MODEL MTOW 1000# MLW 1000# ENGINE MODEL AP FLAPS AP NOISE LEVEL (EPNdB) NOTES 35.50 28.50 PW305 25HAWKER 125-1000 92.0 G-IV GULFSTREAM w/ASC 190 74.60 66.00 TAY 611-8 39 92.0 G100 24.65 20.70 TFE731-40R-200G 40 91.9 MD-90-30 166.00 142.00 V2525-D5 40 91.9 MD-90-30 166.00 142.00 V2528-D5 40 91.9 FALCON 900 45.50 42.00 TFE731-5AR-1C 40 91.7 FALCON 900 (M1196) 46.50 42.00 TFE731-5AR-1C 40 91.7 FALCON 900B (M1200) 46.50 42.00 TFE731-5BR-1C 40 91.7 CL-600 40.40 36.00 ALF 502L/L-2/L-2C 45 91.6 * CL-600 41.25 36.00 ALF-502L/L-2/L-2C 45 91.6 * CL-600 (WINGLETS) 41.25 36.00 ALF-502L/L-2/L-2C 45 91.6 121.00 110.00 BR700-715A1-30 40B-717-200 91.6 48 121.00 110.00 BR700-715C1-30 40B-717-200 91.6 48 525A CITATION JET II (CJ-2) 12.37 11.50 FJ44-2C 35 91.4 BEECHJET 400 91.4 *15.78 14.22 JT15D-5 30 MU-300-10 (DIAM. II) 15.78 14.22 JT15D-5 30 91.4 * 35A/36A 18.30 15.30 TFE731-2-2B 40 91.4 18.30 15.30 TFE731-2-2B 4036A 91.4 * Page 31 ### Page 302 APPENDIX 5 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***APPROACH*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL AP FLAPS AP NOISE LEVEL (EPNdB) NOTES 18.00 14.30 TFE731-2-2B 40 CESSNA 550 CITATION Bravo 91.2 LEARJET 35A 91.3 * 14.80 13.50 PW530A 40 BOMBARDIER CL-600 36.00 33.00 ALF-502 45 91.2 * FAIRCHILD DORNIER DORNIER 328-300 33.51 31.06 PW306B 32 91.1 LEARJET 55B 21.50 18.00 TFE731-3A-2B 40 91.0 * GULFSTREAM G-IV 73.20 58.50 TAY 611-8 39 91.0 GULFSTREAM G200 34.85 28.00 PW306A 40 90.9 47 CESSNA 650 CITATION VII 23.00 20.00 TFE731-4R-3S 40 90.8 GULFSTREAM G-V 90.50 75.30 BR700-710A1-10 39 90.8 DASSAULT FALCON 20-C5/D5/E5 (M3500) 29.10 27.73 TFE731-5AR-2C 40 90.7 DASSAULT FALCON 20-C5/D5/E5 (M3530) 29.10 27.73 TFE-731-5BR-2C 40 90.7 LEARJET 55 90.6 *21.00 17.00 TFE731-3A-2B 40 SABRELINER SABRELINER 65 90.6 *24.00 21.80 TFE731-3R DASSAULT FALCON 20-C5/D5/E5 (M3547) 30.50 28.88 TFE731-5BR-2C 40 90.6 CESSNA 551 CITATION II 90.5 * 12.50 12.00 JT15D-4 40 CESSNA 550 CITATION II 90.514.10 13.50 JT15D-4 40 CESSNA 560 ENCORE 90.516.63 15.20 PW535A 35 DASSAULT FALCON 20-F5 (M3547) 30.50 28.88 TFE731-5BR-2C 40 90.3 Page 32 ### Page 303 APPENDIX 5 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***APPROACH*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL AP FLAPS AP NOISE LEVEL (EPNdB) NOTES 48.20 38.00 GE CF34-3B 45BOMBARDIER CL-604 90.3 * 35.70 31.80 AE3007C 35CESSNA 750 CITATION X 90.2 BOMBARDIER CL-601-1A 45.10 36.00 CF-34-1A 45 90.1 * BOMBARDIER CL-601-3A 45.10 36.00 CF-34-3A/-3A2 45 90.1 * BOMBARDIER CL-601-3R 45.10 36.00 CF-34-3A1 45 90.1 * AEROSPATIALE SN601 CORVETTE 14.60 13.20 JT15D-4 35 90.0 DASSAULT FALCON 20-F5 (M3500) 29.10 27.73 TFE731-5AR-2C 40 90.0 DASSAULT FALCON 20-F5 (M3530) 29.10 27.73 TFE-731-5BR-2C 40 90.0 ISRAEL AIRCRAFT 1125 ASTRA 24.70 20.70 TFE731-3A-200G 40 89.8 BOMBARDIER BD-700-1A10 (Global Express) 96.00 78.50 BR700-710-A2-20 30 89.8 BOMBARDIER BD700-1A10 (Global Express) 75.00 75.00 Rolls Royce/ BR700-710- 30 89.7 (Learjet STC: SA8184NM-D) A2-20 BOMBARDIER CL-601 89.4 *43.00 36.00 CF34-1A 45 43.10 36.00 CF-34-3A 45BOMBARDIER CL-601-3A 89.4 * **16.30 15.20 JT15D-5A 35CESSNA 560 CITATION V 88.9** 15.50 14.30 JT15D-5 35CESSNA 552 88.5 * FOKKER F70 92.00 81.00 TAY MK620-15 42 CESSNA 500/501 CITATION I 11.80 11.30 JT15D-1/-1A 40 87.9 * CESSNA 500 CITATION 87.7 *10.30 9.90 JT15D-1 40 Page 33 88.3 ### Page 304 APPENDIX 5 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***APPROACH*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL AP FLAPS AP NOISE LEVEL (EPNdB) NOTES LEARJET 60 23.10 19.50 PW305A 40 87.7 LEARJET 60 23.50 19.50 PW305A 40 87.7 CESSNA S550 CITATION S/II 15.10 14.40 JT15D-4B 35 86.2 MITSUBISHI MU-300 (DIAMOND I) 14.10 13.20 JT15D-4 30 85.8 * MITSUBISHI MU-300 (DIAMOND I) 15.50 13.20 JT15D-4D 30 85.8 CESSNA 560 CITATION Ultra 16.30 15.20 JT15D-5D 35 85.7 Refer to Appendix 1 for Note Explanations Page 34 ### Page 305 **APPENDIX 6 MODEL** **MANUFACTURER** AEROSPATIALE ATR42-200 MTOW MLW 1000# 34.70 34.20 **MFR, MODEL** **ENGINE DATA SHPNO.** **AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN** **AIRPLANES IN THE TRANSPORT CATEGORY** **RPM MFR, MODEL** **PROPELLER BLADESDIAM (IN) PITCH PW 120 2 2000 1200 HAMILTON STD 14SF-1 156 4 V** **PRATT&WHITNEY TO AP FLAPS 15 30** TO SL AP STAGE NOISE LEVEL (EPNdB) **82.1 83.8 96.8 3 NOTES** **AEROSPATIALE ATR42-300** 35.60 **35.30 PW 120 PRATT&WHITNEY 2 2000 1200 HAMILTON STD 14SF-5 156 4 V 15 30 82.6 83.8 96.8 3** **AEROSPATIALE ATR42-300** 37.30 **36.20 PW 120 PRATT&WHITNEY 2 2000 1200 HAMILTON STD 14SF-5 156 4 V 15 30 83.3 83.7 96.7 3** **AEROSPATIALE ATR42-320** 35.60 **35.30 PW 121 PRATT&WHITNEY 2 2100 1200 HAMILTON STD 14SF-5 156 4 V 15 30 82.2 83.9 96.8 3** **AEROSPATIALE ATR42-320** 37.30 **36.20 PW 121 PRATT&WHITNEY 2 2100 1200 HAMILTON STD 14SF-5 156 4 V 15 30 83.0 83.9 96.7 3** **AEROSPATIALE ATR42-400** 39.50 **38.80 PW 121A PRATT&WHITNEY 2 2200 1200 HAMILTON STD 568F 155 6 V 15 35 77.2 80.9 93.1 3** **AEROSPATIALE ATR42-400** 40.10 **39.50 PW 121A PRATT&WHITNEY 2 2200 1200 HAMILTON STD 568F 155 6 V 15 35 77.6 80.9 93.0 3** **AEROSPATIALE ATR42-500** 41.00 **40.30 PW 127E PRATT&WHITNEY 2 2400 1200 HAMILTON STD 568F 155 6 V 15 35 76.6 80.7 92.4 3** **AEROSPATIALE ATR42-500** 44.05 **42.95 PW 127E PRATT&WHITNEY 2 2400 1200 HAMILTON STD 568F 155 6 V 15 35 78.5 80.7 92.2 3** **AEROSPATIALE ATR72-100** 44.10 **43.90 PW 124 PRATT&WHITNEY 2 2400 1200 HAMILTON STD 14SF11 156 4 V 15 30 85.2 84.8 94.1 3** **AEROSPATIALE ATR72-200** 48.50 **47.10 PW 124 PRATT&WHITNEY 2 2400 1200 HAMILTON STD 14SF11 156 4 V 15 30 86.9 84.7 91.1 3** **AEROSPATIALE ATR72-200** 47.40 **47.10 PW 124 PRATT&WHITNEY 2 2400 1200 HAMILTON STD 14SF11 156 4 V 15 30 86.5 84.7 94.1 3** **AEROSPATIALE ATR72-210** 47.40 **47.10 PW 127 PRATT&WHITNEY 2 2450 1200 HAMILTON STD 247F 156 4 V 15 33 80.2 84.8 92.7 3** **AEROSPATIALE ATR72-210** 47.40 47.10 PW 127 PRATT&WHITNEY 2 2450 1200 HAMILTON STD 14SF11 156 4 V 15 33 86.1 86.1 94.2 3 Page 1 ### Page 306 **APPENDIX 6 MODEL** **MANUFACTURER** AEROSPATIALE ATR72-210 MTOW MLW 1000# 48.50 48.20 **MFR, MODEL** **ENGINE DATA SHPNO.** **AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN** **AIRPLANES IN THE TRANSPORT CATEGORY** **RPM MFR, MODEL** **PROPELLER BLADESDIAM (IN) PITCH PW 127 2 2450 1200 HAMILTON STD 14SF11 156 4 V** **PRATT&WHITNEY TO AP FLAPS 15 33** TO SL AP STAGE NOISE LEVEL (EPNdB) **86.5 86.0 94.2 3 NOTES** **AEROSPATIALE ATR72-210** 50.66 **49.56 PW127 PRATT&WHITNEY 2 1200 HAMILTON STD.** 247F 156 4 V 15 33 82.2 84.7 92.4 3 BAE SYSTEMS (BAe) 748-2A 44.50 43.00 DART 532-2 ROLLS-ROYCE 2 2470 1394 DOWTY ROTOL CR212/4-30-4/22 144 4 V 15 28 92.5 96.8 103.8 2 BAE SYSTEMS (BAe) 748-2B 46.00 43.00 DART 535-2 ROLLS ROYCE 2 2470 1394 DOWTY ROTOL CR212/4-30-4/22 144 4 V 15 28 92.5 96.8 103.4 2 BAE SYSTEMS (BAe) 748-2B 46.00 43.00 DART 536-2 ROLLS ROYCE 2 2470 1394 DOWTY ROTOL CR212/4-30-4/22 144 4 V 8 28 88.7 93.3 92.8 3 1 BAE SYSTEMS (BAe) ATP 50.55 **49.05 PW124A PRATT&WHITNEY 2 2160 1200 HAMILTON STD.** 6/5500/F 165 6 V 7 22 80.7 82.1 96.5 3 BAE SYSTEMS (BAe) ATP 50.55 49.05 PW126A PRATT&WHITNEY 2 2396 1200 HAMILTON STANDARD 6/5500/F 165 6 V 7 20 79.5 82.7 97.0 3 BAE SYSTEMS (BAe) ATP 50.55 **49.05 PW126A PRATT&WHITNEY 2 2396 1200 HAMILTON STD.** 6/5500/F.1 165 6 V 7 15 79.5 82.7 97.9 3 **BAE SYSTEMS (JETSTREAM) JETSTREAM 4100** 23.00 22.30 TPE-331-14G(H)R-801 ALLIEDSIGNAL 2 1500 1552 MCCAULEY B/C5JFR36C1101/2L114G 114 5 V 9 15 85.8 83.5 87.8 3 * **BAE SYSTEMS (JETSTREAM) JETSTREAM 4100** 24.00 23.30 TPE-331-14G(H)R-801 ALLIEDSIGNAL 2 1500 1552 MCCAULEY B/C5JFR36C1101/2L114G 114 5 V 9 15 86.4 83.4 87.8 3 * **BAE SYSTEMS (JETSTREAM) JETSTREAM 4100** 24.00 23.30 TPE-331-14G(H)R-805 ALLIEDSIGNAL 2 1650 1552 MCCAULEY B/C5JFR36C1103/4L114H 114 5 V 9 15 86.5 84.3 87.8 3 * **BAE SYSTEMS (JETSTREAM) JETSTREAM 4100** 24.00 23.30 TPE-331-14G(H)R-901 ALLIEDSIGNAL 2 1650 1552 MCCAULEY B/C5JFR36C1103/4L114H 114 5 V 9 15 86.7 84.3 87.9 3 * **BOMBARDIER DHC-7-101** 43.00 **41.01 PT6A-50 PRATT&WHITNEY 4 1017 1210 HAMILTON STD.** 24PF-305 135 4 V 25 25 80.1 83.3 91.6 3 * **BOMBARDIER DHC-7-103** 44.00 **42.00 PT6A-50 PRATT&WHITNEY 4 1120 1210 HAMILTON STD.** 24PF-305 135 4 V 25 25 80.5 84.0 91.4 3 * Page 2 ### Page 307 **APPENDIX 6 MODEL** **MANUFACTURER** BOMBARDIER DHC-8 MTOW MLW 1000# 33.00 32.40 **MFR, MODEL** **ENGINE DATA SHPNO.** **AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN** **AIRPLANES IN THE TRANSPORT CATEGORY** **RPM MFR, MODEL** **PROPELLER BLADESDIAM (IN) PITCH PW 120 2 1800 HAMILTON STD.** 14SF-1 156 4 V **PRATT&WHITNEY TO AP FLAPS 15 35** TO SL AP STAGE NOISE LEVEL (EPNdB) **80.7 86.3 95.1 3 NOTES** **BOMBARDIER DHC-8-102** 34.50 **33.90 PW 120 PRATT&WHITNEY 2 1800 1150 HAMILTON STD 14SF-7 156 4 V 15 35 80.8 86.3 90.7 3** **BOMBARDIER DHC-8-102** 34.50 **33.90 PW 120 PRATT&WHITNEY 2 1800 1200 HAMILTON STD 14SF-7 156 4 V 15 35 80.8 86.3 94.8 3** **BOMBARDIER DHC-8-103** 34.50 **33.90 PW 121 PRATT&WHITNEY 2 1945 1150 HAMILTON STD 14SF-7 156 4 V 15 35 79.8 85.3 90.7 3** **BOMBARDIER DHC-8-103** 34.50 **33.90 PW 121 PRATT&WHITNEY 2 1945 1200 HAMILTON STD 14SF-7 156 4 V 15 35 79.8 86.1 94.8 3** **BOMBARDIER DHC-8-103** 34.50 **33.90 PW 121 PRATT&WHITNEY 2 1945 1100 HAMILTON STD 14SF-7 156 4 V 15 35 77.8 82.9 91.0 3** **BOMBARDIER DHC-8-106** 36.30 **33.90 PW 121 PRATT&WHITNEY 2 1945 1100 HAMILTON STD 14SF-7 156 4 V 15 35 79.9 84.0 94.8 3** **BOMBARDIER DHC-8-106** 36.30 **33.90 PW 121 PRATT&WHITNEY 2 1945 1200 HAMILTON STD 14SF-7 156 4 V 15 35 80.5 85.6 94.8 3** **BOMBARDIER DHC-8-201** 36.30 **33.90 PW 123 PRATT&WHITNEY 2 1945 1100 HAMILTON STD 14SF-7 156 4 V 15 35 79.9 84.0 94.8 3** **BOMBARDIER DHC-8-201** 36.30 **33.90 PW 123 PRATT&WHITNEY 2 1945 1200 HAMILTON STD 14SF-7 156 4 V 15 35 80.5 85.6 94.8 3** **BOMBARDIER DHC-8-202** 36.30 **33.90 PW 123 PRATT&WHITNEY 2 1945 1100 HAMILTON STD 14SF-7 156 4 V 15 35 79.9 84.0 94.8 3** **BOMBARDIER DHC-8-202** 36.30 **33.90 PW 123 PRATT&WHITNEY 2 1945 1200 HAMILTON STD 14SF-7 156 4 V 15 35 80.5 85.6 94.8 3** **BOMBARDIER DHC-8-300** 41.10 **40.00 PW123 PRATT&WHITNEY 2 1200 HAMILTON STD.** 14SF-15 156 4 V 5 15 84.3 87.4 98.9 3 **BOMBARDIER DHC-8-311** 41.10 40.00 PW123 PRATT&WHITNEY 2 2142 HAMILTON STANDARD 14SF-15 156 4 V 5 35 79.5 87.0 93.3 3 Page 3 ### Page 308 **APPENDIX 6 MODEL** **MANUFACTURER** BOMBARDIER DHC-8-311 MTOW MLW 1000# 43.00 42.00 **MFR, MODEL** **ENGINE DATA SHPNO.** **AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN** **AIRPLANES IN THE TRANSPORT CATEGORY** **RPM MFR, MODEL** **PROPELLER BLADESDIAM (IN) PITCH PW 123 2 2142 1200 HAMILTON STD 14SF-15 156 4 V** **PRATT&WHITNEY TO AP FLAPS 5 35** TO SL AP STAGE NOISE LEVEL (EPNdB) **80.0 86.8 93.3 3 NOTES** **BOMBARDIER DHC-8-314** 41.10 40.00 PW123 PRATT&WHITNEY 2 2249 1200 HAMILTON STANDARD 14SF-15 156 4 V 5 35 79.9 87.3 93.3 3 **BOMBARDIER DHC-8-314** 41.10 40.00 PW123 PRATT&WHITNEY 2 2249 1100 HAMILTON STANDARD 14SF-15 156 4 V 5 35 80.7 84.7 93.3 3 **BOMBARDIER DHC-8-314** 43.00 42.00 PW123 PRATT&WHITNEY 2 2249 1200 HAMILTON STANDARD 14SF-15 156 4 V 5 35 80.7 87.2 93.3 3 **BOMBARDIER DHC-8-314** 43.00 42.00 PW123 PRATT&WHITNEY 2 2249 1100 HAMILTON STANDARD 14SF-15 156 4 V 5 35 81.7 84.6 93.2 3 **BOMBARDIER DHC-8-315** 41.10 40.00 PW123E PRATT&WHITNEY 2 2142 1200 HAMILTON STANDARD 14SF-15 156 4 V 5 35 79.5 87.0 93.3 3 **BOMBARDIER DHC-8-315** 43.00 42.00 PW123E PRATT&WHITNEY 2 2142 1200 HAMILTON STANDARD 14SF-15 156 4 V 5 35 80.0 86.9 93.3 3 **BOMBARDIER DHC-8-400 (Q400)** 61.70 60.50 PWC 150A PRATT&WHITNEY 2 5070 1020 DOWTY R408/6-123-F/17 162 6 V 5 15 77.1 84.1 94.9 3 **BOMBARDIER DHC-8-400 (Q400)** 61.70 60.50 PWC 150A PRATT&WHITNEY 2 5070 1020 DOWTY R408/6-123-F/17 162 6 V 5 35 77.1 84.1 93.0 3 3 **BOMBARDIER DHC-8-400 (Q400)** 65.20 62.00 PWC 150A PRATT&WHITNEY 2 5070 1020 DOWTY R408/6-123-F/17 162 6 V 5 35 78.6 84.0 93.1 3 3 **BOMBARDIER DHC-8-400 (Q400)** 65.20 62.00 PWC 150A PRATT&WHITNEY 2 5070 1020 DOWTY R408/6-123-F/17 162 6 V 5 15 78.6 84.0 94.8 3 **BOMBARDIER DHC-8-401 (Q400)** 61.70 60.50 PWC 150A PRATT&WHITNEY 2 5070 1020 DOWTY R408/6-123-F/17 162 6 V 5 35 77.1 84.1 93.0 3 3 **BOMBARDIER DHC-8-401 (Q400)** 61.70 60.50 PWC 150A PRATT&WHITNEY 2 5070 1020 DOWTY R408/6-123-F/17 162 6 V 5 15 77.1 84.1 94.9 3 **BOMBARDIER DHC-8-401 (Q400)** 65.20 62.00 PWC 150A PRATT&WHITNEY 2 5070 1020 DOWTY R408/6-123-F/17 162 6 V 5 15 78.6 84.0 94.8 3 Page 4 ### Page 309 **APPENDIX 6 MODEL** **MANUFACTURER** BOMBARDIER DHC-8-401 (Q400) MTOW MLW 1000# 65.20 62.00 **MFR, MODEL** **ENGINE DATA SHPNO.** **AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN** **AIRPLANES IN THE TRANSPORT CATEGORY** **RPM MFR, MODEL** **PROPELLER BLADESDIAM (IN) PITCH PWC 150A 2 5070 1020 DOWTY R408/6-123-F/17 162 6 V** **PRATT&WHITNEY TO AP FLAPS 5 35** TO SL AP STAGE NOISE LEVEL (EPNdB) **78.6 84.0 93.1 3 NOTES 3** **BOMBARDIER DHC-8-402 (Q400)** 61.70 60.50 PWC 150A PRATT&WHITNEY 2 5070 1020 DOWTY R408/6-123-F/17 162 6 V 5 15 77.1 84.1 94.9 3 **BOMBARDIER DHC-8-402 (Q400)** 61.70 60.50 PWC 150A PRATT&WHITNEY 2 5070 1020 DOWTY R408/6-123-F/17 162 6 V 5 35 77.1 84.1 93.0 3 3 **BOMBARDIER DHC-8-402 (Q400)** 65.20 62.00 PWC 150A PRATT&WHITNEY 2 5070 1020 DOWTY R408/6-123-F/17 162 6 V 5 35 78.6 84.0 93.1 3 3 **BOMBARDIER DHC-8-402 (Q400)** 65.20 62.00 PWC 150A PRATT&WHITNEY 2 5070 1020 DOWTY R408/6-123-F/17 162 6 V 5 15 78.6 84.0 94.8 3 CASA C-212-CB 14.33 13.80 TPE 331-5-251C ALLIEDSIGNAL 2 750 1591 HARTZELL HC-B4TN-5CL/LT10282H 107 4 V 10 20 87.3 84.0 91.2 3 * CASA C-212-CC 16.98 16.42 TPE 331-10/10R-501C/ ALLIEDSIGNAL 2 900 1591 HARTZELL HC-B4MN-5AL 110 4 V 10 15 85.9 85.1 90.9 3 * CASA C-212-CD/CE 16.98 16.42 TPE331-10R-502C/512 ALLIEDSIGNAL 2 900 1591 DOWTY-ROTOL (C)R.334/4-82-F/13 110 4 V 10 40 82.9 83.0 93.2 3 * CASA C-212-CF 16.98 16.42 TPE 331-10R-501C/511 ALLIEDSIGNAL 2 900 1591 HARTZELL HC-B4MN-5AL 110 4 V 10 15 85.9 85.1 90.9 3 * CASA C-212-DE 16.98 16.42 PT6A-65B PRATT&WHITNEY 2 1000 1700 MCCAULEY 4HFR34C756 106 4 V 10 40 84.1 84.7 88.0 3 * CASA C-212-DF 16.98 16.42 TPE331-10R-502C/512 ALLIEDSIGNAL 2 900 1591 DOWTY-ROTOL (C)R.334/4-82-F/13 110 4 V 10 40 82.9 83.0 93.2 3 * CASA C-295 46.30 45.63 PW127-G PRATT&WHITNEY 2 2645 1200 HAMILTON STANDARD HS E568F 155 6 V 10 15 87.1 88.2 93.9 3 * CASA CN-235 31.75 **31.30 CT7-7A GENERAL ELECTRIC 2 1700 1384 HAMILTON STD.** 14RF-21 132 4 V 8 23 84.5 86.5 87.2 3 * CASA CN-235-100 31.75 31.30 CT7-9C GENERAL ELECTRIC 2 1750 1384 HAMILTON STANDARD 14RF-21 132 4 V 10 23 84.8 86.7 87.2 3 * Page 5 ### Page 310 **APPENDIX 6 MODEL** MANUFACTURER CASA CN-235-100 MTOW MLW 1000# 33.29 32.85 **MFR, MODEL** **ENGINE DATA SHPNO.** **AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN** **AIRPLANES IN THE TRANSPORT CATEGORY** **RPM MFR, MODEL** **PROPELLER BLADESDIAM (IN) PITCH CT7-9C 2 1750 1384 HAMILTON STANDARD 14RF-21 132 4 V** **GENERAL ELECTRIC TO AP FLAPS 10 23** TO SL AP STAGE NOISE LEVEL (EPNdB) 85.3 87.8 87.2 3 NOTES * CASA CN-235-200 34.83 34.39 CT7-9C GENERAL ELECTRIC 2 1750 1384 HAMILTON STANDARD 14RF-21 132 4 V 10 23 80.5 87.4 92.4 3 * CASA CN-235-300 34.83 34.39 CT7-9C3 GENERAL ELECTRIC 2 1750 1384 HAMILTON STANDARD 14RF-37 144 4 V 10 15 85.0 87.8 93.3 3 * CONVAIR 580 (Aeroprod.) 58.16 52.00 501-D13H ALLISON 2 3460 1020 AEROPRODUCTS A6441FN-606A 162 4 V 10 28 87.4 91.1 98.3 3 **DORNIER 328-100/MOD 10** 30.84 29.17 PW119B PRATT&WHITNEY 2 2180 1300 HARTZELL HD-E6C-3B 142 6 V 12 12 82.1 83.8 94.8 3 2,* **DORNIER 328-100/MOD 20** 30.84 29.17 PW119C PRATT&WHITNEY 2 2180 1300 HARTZELL HD-E6C-3B 142 6 V 12 12 82.7 83.8 94.8 3 2,* **DORNIER 328-100/MOD 30** 30.84 29.17 PW119C PRATT&WHITNEY 2 2180 1300 HARTZELL HD-E6C-3B 142 6 V 12 12 82.7 83.8 94.8 3 2,* **EMBRAER EMB-120** 21.17 **21.17 PW 115 PRATT&WHITNEY 2 1500 HAMILTON STD.** 14RF-9 126 4 V 15 25 76.6 81.6 92.5 3 **EMBRAER EMB-120** 25.40 **24.80 PW118 PRATT&WHITNEY 2 HAMILTON STD.** 14RF-9 126 4 V 15 25 81.2 83.5 92.3 3 * FOKKER 50 45.86 **41.83 125B PRATT&WHITNEY 2 V 8 26 81.0 85.0 96.8 3 FOKKER F27 MK500** 45.00 42.00 DART 7/MK535-7R ROLLS ROYCE 2 DOWTY ROTOL R193-4-30-4 138 4 V 0 40 90.6 92.2 100.3 2 FOKKER F27 MK500 45.00 43.50 DART 7/MK535-7 ROLLS ROYCE 2 DOWTY ROTOL R193-4-30-4 138 4 V 0 40 86.9 90.1 94.3 3 1 FOKKER F27 MK500 45.00 43.50 DART 7/MK535-7R ROLLS ROYCE 2 DOWTY ROTOL R193-4-30-4 138 4 V 0 40 87.4 89.8 94.3 3 1 FOKKER F27 MK500 45.90 43.50 DART 7/MK551-7R ROLLS ROYCE 2 DOWTY ROTOL R193-4-30-4 138 4 V 0 40 87.6 89.8 94.3 3 1 Page 6 ### Page 311 **APPENDIX 6 MODEL** MANUFACTURER FOKKER F27 MK500/600 MTOW MLW 1000# 45.00 41.00 **MFR, MODEL** **ENGINE DATA SHPNO.** **AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN** **AIRPLANES IN THE TRANSPORT CATEGORY** **RPM MFR, MODEL** **PROPELLER BLADESDIAM (IN) PITCH DART 7/MK552-7R 2 2307 DOWTY ROTOL R193-4-30-4 138 4 V** **ROLLS ROYCE TO AP FLAPS 0 40** TO SL AP STAGE NOISE LEVEL (EPNdB) **87.4 89.8 94.1 3 NOTES 1 FOKKER F27 MK500/600** 45.90 43.50 DART 7/MK552-7R ROLLS ROYCE 2 2307 DOWTY ROTOL R193-4-30-4 138 4 V 0 40 87.6 89.8 94.3 3 1 FOKKER F27 MK600 45.00 **42.00 DART7 MK532-7R ROLLS ROYCE 2 DOWTY ROTOL R193-4-30-4 138 4 V 0 40 90.6 92.2 100.3 2** **LOCKHEED L382G** 155.00 **135.00 501-D22A ALLISON 4 4050 1020 HAMILTON STD.** 54H60 162 4 V 18 35 94.8 96.7 98.1 3 * **MCDONNELL DOUGLAS DC3C (BTC STC)** 28.75 28.75 PT6A-67R PRATT&WHITNEY 2 HARTZELL HC-B5MA-3/M11276 115 5 V 0 45 82.4 84.4 91.9 3 SAAB 2000(w/PECS mod) 50.20 **48.50 AE2100A ALLISON 2 DOWTY ROTOL R381/6-123-F/5 15 35 78.4 87.5 87.9 3 SAAB 340B** 28.50 28.00 CT7-9B GENERAL ELECTRIC 2 1384 DOWTY ROTOL R354/4-123-F/13/20 132 4 V 15 20 78.0 85.9 91.6 3 SAAB 340B 28.50 **28.00 CT7-9B GENERAL ELECTRIC 2 1384 HAMILTON STD.** **14RF-19 132 4 V 15 20 77.7 86.1 90.1 3 SAAB 340B** 28.50 28.00 CT7-9B GENERAL ELECTRIC 2 1384 DOWTY ROTOL R375/4-123-F/21 132 4 V 15 20 78.0 85.9 91.6 3 SAAB SF340A 28.00 27.20 CT7-5A2 GENERAL ELECTRIC 2 1384 DOWTY ROTOL R375/4-123-F/21 132 4 V 15 20 78.2 85.8 84.4 3 SAAB SF340A 28.00 27.20 CT7-5A2 GENERAL ELECTRIC 2 1384 DOWTY ROTOL R354/4-123-F/13/20 132 4 V 15 20 78.2 85.8 84.4 3 **SAAB FAIRCHILD 340** 27.00 26.50 CT7-5A GENERAL ELECTRIC 2 1210 DOWTY ROTOL R320/4-123-F/1 126 4 V 15 35 79.3 87.6 89.6 3 **SAAB FAIRCHILD 340** 27.00 26.50 CT7-7E GENERAL ELECTRIC 2 1210 DOWTY ROTOL R320/4-123-F/1 126 4 V 15 35 79.5 87.4 89.6 3 **SAAB-SCANIA 340A W/APU** 27.28 26.50 CT7-5A2 GENERAL ELECTRIC 2 1735 DOWTY ROTOL R354/4-123-F13 132 4 V 35 77.5 86.2 86.3 3 Page 7 ### Page 312 **APPENDIX 6 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN** **AIRPLANES IN THE TRANSPORT CATEGORY MTOW MODEL** MANUFACTURER MLW 1000# MFR, MODEL **ENGINE DATA NO. SHP RPM MFR, MODEL** **PROPELLER DIAM (IN) BLADES** **PITCH TO AP FLAPS** TO SL AP STAGE NOISE LEVEL (EPNdB) NOTES SHORT BROS. 22.00 PRATT&WHITNEY 2 1120 1675 HARTZELL 111 5 8 35 88.5 83.9 92.8 3 * SD3-30 21.61 PT6A-45 HC-35MP-34/M10282B-6 V SHORT BROS. 26.00 PRATT&WHITNEY 2 1327 HARTZELL 111 5 5 30 84.4 83.7 89.9 3 ** SD3-60 25.70 PT6A-65R HC-B5MP-3C/M10876K V SHORT BROS. 27.10 PRATT&WHITNEY 2 1700 HARTZELL 108 6 15 15 80.0 82.7 94.3 3 SD3-60-300 25.70 PT6A-67R HC-A6A-3/A1046E V Page 8 ### Page 313 11/15/01 AC36-1H Appendix 6 Appendix 6 Notes 1 Equipped With Standard Hushkit 2. APU On For Approach 3. Mod Sup 39; Propeller RPM limited to 850 for approach. * Full Thrust Takeoff ** 650 Meter Sideline See Appendix 1 For Charts And Equations For The Calculation Of Noise Certification Limits Page 9 ### Page 314 APPENDIX 7 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CFR PART 36, APPENDIX F) MANUFACTURER MTOW ENGINE DATA PROPELLER DATA NOISE LEVEL (dBA) MODEL MLW (1000#) MFR, MODEL NO. SHP EXH MFR, MODEL DIAM (IN) BLADES PITCH RPM MdBA PC CdBA NOTES AEROTECH/AUST. 9.10 ALLISON 2 HARTZELL 91 3 2071 78.00 -2.10 75.9 N22S 250-B17E HC-A3VF-7B/V10133N ANDERSON GREEN 3.15 AVCO LYCOMING 1 250 3 HARTZELL 77 2 2575 75.20 -1.50 73.7 WOOD 51 3.15 O-540-A4D5 HC-E2YR-1S/8465-7R V BEECH 12.50 PRATT&WHITNEY 2 847 1 HARTZELL 98 3 2000 82.80 -3.60 79.2 (200) 12.50 PT6A-41 HC-B3TN-3G/T10178H V BEECH 16.60 PRATT&WHITNEY 2 1100 2 HARTZELL 110 4 1700 80.50 3.00 77.4 1 1900/1900C 16.10 PT6A-65B HCB4MP-3A/M10877K V BEECH 14.40 PRATT & WHITNEY 2 1200 McCAULEY 104 5 1700 84.28 -5.47 79.3 2000 XPT6A-67 D-L104DSZ-O V BEECH 5.50 TCM 2 300 MCCAULEY 77 3 80.65 -3.26 77.4 58/58A 5.40 IO-550-C 3AF32C512/82-NEA-5 V BEECH 3.60 TELEDYNE 1 260 5 MCCAULEY 80 3 2700 78.80 -0.60 78.2 A36 3.60 I0-520-B 3A32C760/82 NB-2 V BEECH 3.60 TELEDYNE 1 228 5 MCCAULEY 84 2 2550 78.00 -0.60 77.4 A36 3.60 I0-520-N 2A36C23/84B-0 V BEECH 3.65 TCM 1 300 MCCAULEY 80 3 78.24 -1.57 76.7 A36 3.65 IO-550-B 3A32C406/82NDB-2 V BEECH 3.65 TELEDYNE 1 300 5 MCCAULEY 80 3 2700 79.50 -0.30 79.2 A36TC 3.65 TSI0-520-U 3A32C760/82 NB-2 V BEECH 11.80 AIRESEARCH 2 715 1 HARTZELL 90 4 2000 80.20 -2.90 77.3 B100 11.20 TPE331-6-252B HC-B4TN-5C/T10173F V BEECH 12.50 PRATT&WHITNEY 2 845 1 HARTZELL 99 3 1996 82.80 -3.60 79.2 B200 12.50 PT6A-41 HC-B3TN-3G/T10178H V BEECH 12.50 PRATT&WHITNEY 2 850 1 HARTZELL 98 3 2000 82.80 -3.60 79.2 B200/B200C 12.50 PT6A-42 HC-B3TN-3G/T10178H V Page 1 ### Page 315 APPENDIX 7 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CFR PART 36, APPENDIX F) MANUFACTURER MTOW ENGINE DATA PROPELLER DATA NOISE LEVEL (dBA) MODEL MLW (1000#) MFR, MODEL NO. SHP EXH MFR, MODEL DIAM (IN) BLADES PITCH RPM MdBA PC CdBA NOTES BEECH 12.50 PRATT&WHITNEY 2 850 2 MCCAULEY 98 3 2000 79.32 -3.93 75.4 B200/B200C 12.50 PT6A-42 3GFR34C702/100LA-2 V BEECH 12.50 PRATT&WHITNEY 2 850 MCCAULEY 94 4 80.68 -3.93 76.8 B200/B200C/C12F 12.50 PT6A-42 4HFR34C754/94LA-0 V BEECH 12.50 PRATT&WHITNEY 2 845 1 HARTZELL 99 3 1996 82.80 -3.30 79.5 B200CT 12.50 PT6A-42 HC-B3TN-3G/T10178H V BEECH 12.50 PRATT&WHITNEY 2 850 1 MCCAULEY 98 3 2000 79.32 -3.84 75.5 B200T/B200CT 12.50 PT6A-42 3GFR34C702/100LA-Z BEECH 12.50 PRATT&WHITNEY 2 850 MCCAULEY 94 4 80.68 -3.84 76.8 B200T/B200CT 12.50 PT6A-42 4HFR34C754/94LA-O V BEECH 15.00 PRATT&WHITNEY 2 1050 2 HARTZELL 105 4 1700 75.90 -3.80 72.1 1 B300 PT6A-60A HC-B4MP-3/M10476K BEECH 3.86 TELEDYNE 1 293 MCCAULEY 78 3 2700 78.70 0.50 79.2 B36TC 3.86 TS10-520-U 82NDA-4 V BEECH 5.10 TELEDYNE 2 221 2 HARTZELL 76 3 2550 77.70 -3.00 74.7 B55 5.10 I0-470-L PHC-C3YF-2/FC7663-2 V BEECH 5.10 TELEDYNE 2 223 2 HARTZELL 78 2 2550 81.00 -3.00 78.0 B55 5.10 IO-470-L BHC-C2YF-2CH/FC846 V BEECH 5.40 TELEDYNE 2 254 2 HARTZELL 78 2 2550 82.00 -3.10 78.9 B58 5.40 10-520-C BHC-J2YF-2C/FC8475­ V BEECH 5.40 TELEDYNE 2 256 2 HARTZELL 76 3 2650 81.90 -3.10 78.8 B58 5.40 I0-520-C PHC-J3YF-2/FC7663-D V BEECH 5.50 TCM 2 300 HARTZELL 4 2700 78.48 -3.08 75.4 B58 5.40 IO-550-C4B FC-7063Q V BEECH 6.10 TELEDYNE 2 301 2 HARTZELL 78 3 2600 80.60 -1.50 79.1 B58P 6.10 TSIO-520-L PHC-J3YF-2/FC7663-D V Page 2 ### Page 316 APPENDIX 7 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CFR PART 36, APPENDIX F) MANUFACTURER MTOW ENGINE DATA PROPELLER DATA NOISE LEVEL (dBA) MODEL MLW (1000#) MFR, MODEL NO. SHP EXH MFR, MODEL DIAM (IN) BLADES PITCH RPM MdBA PC CdBA NOTES BEECH 6.20 CONTINENTAL 2 294 4 HARTZELL 78 3 2600 78.20 -2.10 76.1 B58P 6.20 TS10-520-WB PHC-J3YF-2UF/FC7663 V BEECH 6.10 TELEDYNE 2 294 4 HARTZELL 78 3 2600 78.20 -2.10 76.1 B58TC 6.10 TS10-520-WB PHC-J3YF-2UF/FC7663 V BEECH 6.20 CONTINENTAL 2 301 2 HARTZELL 78 3 2600 80.60 -1.50 79.1 B58TC 6.20 TS10-520-L PHC-J3Y-2F/FC7663-D V BEECH 6.78 LYCOMING 2 296 2 HARTZELL 74 3 2750 82.10 -2.50 79.6 B60 6.78 TIO-541-E1C4 HC-F3YR-2UF/FC7479 V BEECH 9.02 PRATT&WHITNEY 2 700 4 HARTZELL 93 3 1900 76.20 -5.80 70.4 B65-90 8.55 PT6A-135 HC-B3TN-2(B)/T10173 V BEECH 3.98 LYCOMING 2 165 1 HARTZELL 76 2 2700 79.50 -2.30 77.2 B76 O-360-A1G6D HC-M2YR-2CLUF/FC7 V BEECH 3.90 LYCOMING 2 165 2 HARTZELL 76 2 2700 80.20 -1.50 78.7 B76 3.90 O-360-A1G6D HC-M2YR-2CEUF/FC7 V BEECH 1.68 LYCOMING 1 115 8 SENSENICH 72 2 2700 65.10 -1.30 63.8 B77 1.68 0-235-L2C 72CKS12-0-52 F BEECH 5.30 TCM 2 300 2 HARTZELL 74 4 2700 78.48 -3.08 75.4 B95-C55 5.30 IO-550-C FC-7063Q V BEECH 2.45 LYCOMING 1 163 2 SENSENICH 76 2 2700 73.30 0.00 73.3 C23 2.45 0-360-A4J 76EM8S5-0-60 F BEECH 2.75 LYCOMING 1 202 2 HARTZELL 76 2 2700 73.00 -1.30 71.7 C24R 2.75 0-360-A1B6 HC-M2YR-1BF/FC7666 V BEECH 9.66 PRATT&WHITNEY 2 550 HARTZELL 93 3 2200 78.70 -4.40 74.3 C90 9.17 PT6A-21 HC-B3TN-2B/T10173B­ V BEECH 10.10 PRATT&WHITNEY 550 4 HARTZELL 93 3 2200 78.69 -4.44 74.3 C90A PT6A-21 HC-B3TN-2(B) Page 3 ### Page 317 APPENDIX 7 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CFR PART 36, APPENDIX F) MANUFACTURER MTOW ENGINE DATA PROPELLER DATA NOISE LEVEL (dBA) MODEL MLW (1000#) MFR, MODEL NO. SHP EXH MFR, MODEL DIAM (IN) BLADES PITCH RPM MdBA PC CdBA NOTES BEECH 11.30 PRATT&WHITNEY 2 715 HARTZELL 93 3 2200 79.30 -3.40 75.9 C99 11.30 PT6A-34 HC-B3TN-3/T10173B-8 V BEECH 5.30 TCM 2 300 2 HARTZELL 74 4 2700 78.48 -3.44 75.0 D55 5.30 IO-550-C FC-7063Q V BEECH 5.30 TELEDYNE 2 256 2 HARTZELL 76 3 2650 81.90 -3.20 78.7 E55 5.30 I0-520-C PHC-J3Y-2F/FC7663-2 V BEECH 5.30 TELEDYNE 2 254 2 HARTZELL 78 2 2550 82.00 -3.20 78.8 E55 5.30 IO-520-C BHC-C2YF-2C/FC8475­ V BEECH 5.30 TCM 2 300 V HARTZELL 74 4 2700 78.48 -3.44 75.0 E55 5.30 IO-550-C FC-7063Q V BEECH 5.30 TCM 2 300 V HARTZELL 74 4 2700 78.48 -3.44 75.0 E55 5.30 IO-550-C FC-7063Q V BEECH 5.30 TCM 2 300 2 HARTZELL 74 4 2700 78.48 -3.44 75.0 E55 5.30 IO-550-C FC-7063Q V BEECH 10.10 PRATT&WHITNEY 2 550 HARTZELL 93 3 2200 79.00 -4.00 75.0 E90 9.70 PT6A-28 HC-B3TN-2B/T10173B­ V BEECH 3.40 TELEDYNE 1 260 5 MCCAULEY 80 3 2700 78.30 -1.40 76.9 F33 A/C 3.40 I0-520-B 3A32C76/82NB-2 V BEECH 3.40 TELEDYNE 1 228 5 MCCAULEY 84 2 2550 78.10 -1.50 76.6 F33 A/C 3.40 I0-520-BA 2A36C23/84 B-0 V BEECH 10.95 PRATT&WHITNEY 2 754 1 HARTZELL 92 4 1900 77.90 -5.00 72.9 F90 SUPER 10.95 PT6A-135 HC-B4TN-3B/T10173F V BEECH 3.40 TELEDYNE 1 260 5 MCCAULEY 80 3 2700 78.80 -2.00 76.8 V35B 3.40 I0-520-B 3A32C76/82 NB-2 V BEECH 3.40 TELEDYNE 1 228 5 MCCAULEY 84 2 2550 78.10 -1.50 76.6 V35B 3.40 I0-520-BA 2A36C23/84B-0 V Page 4 ### Page 318 APPENDIX 7 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CFR PART 36, APPENDIX F) MODEL MANUFACTURER MTOW MLW (1000#) **MFR, MODEL** **ENGINE DATA NO. SHP EXH MFR, MODEL** PROPELLER DATA DIAM (IN) BLADES PITCH RPM MdBA PC CdBA NOISE LEVEL (dBA) NOTES **BELLANCA 17-30A** 3.20 3.20 **CONTINENTAL I0-520-K 1 225 8 MCCAULEY D3A34C401/90DFA-12 78 3 F 2550 79.40 -1.90 77.5** **BELLANCA 7ECA** 1.65 1.65 **LYCOMING 0-235-K2C 1 115 2 SENSENICH 74DM6S8-1-56 72 2 F 2700 71.50 -2.70 68.8** **BELLANCA 7GCAA** 1.65 1.65 **LYCOMING 0-320-A2B/-A2D 1 150 2 SENSENICH 74DM6S8-1-56 73 2 F 2800 71.50 -4.70 66.8** **BELLANCA 7GCBC** 1.65 1.65 **LYCOMING 0-320-A2B/A2D 1 150 2 SENSENICH 74DM6S8-1-56 73 2 F 2700 71.50 -4.60 66.9** **BELLANCA 7GCBC SEAPLANE** 1.80 1.80 **LYCOMING 0-320 1 150 2 MCCAULEY 1A175GMA/8040 80 2 F 2500 68.40 1.90 70.3** **BELLANCA 8GCBC** 2.15 2.15 **LYCOMING 0-360-C1A/-C1E 1 180 2 HARTZELL HC-C2YR-1BF/F7666A 76 2 F 2550 76.30 -3.40 72.9** **BELLANCA 8GCBC** 2.15 2.15 **LYCOMING 0-360-C2A/-C2E 1 149 2 MCCAULEY 1A200/HFA 80 2 F 2550 76.30 -3.50 72.8** **BELLANCA 8KCAB** 1.80 1.80 **LYCOMING AEIO-320-E1B 1 150 2 HARTZELL HC-C2YL-4F/FC7663-4 72 2 V 2800 72.20 -2.20 70.0** **BELLANCA 8KCAB** 1.80 1.80 **LYCOMING AEIO-320-E2B 1 150 2 SENSENICH 74DM6S8-0 74 2 F 2800 72.20 -3.00 69.2** **BELLANCA 8KCAB** 1.80 1.80 LYCOMING AEIO-360-H1A 1 180 2 HARTZELL HC-C2YR-4CF/FC7666 74 2 V 2900 72.20 -5.00 67.2 CESSNA 152 1.67 1.67 LYCOMING O-235-L2C 1 110 8 MCCAULEY 1A102/TCM6955 69 2 F 2550 65.80 -1.00 64.8 CESSNA 152/A152 1.67 1.67 LYCOMING O-235-L2C 1 110 8 MCCAULEY 1A103/TCM6958 69 2 F 2550 66.70 -0.40 66.3 CESSNA 172N (LAND) 2.30 2.30 LYCOMING O-320-H2AD 1 160 8 MCCAULEY 1C160/DTM 7557 75 2 F 2700 74.30 -0.50 73.8 Page 5 ### Page 319 APPENDIX 7 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CFR PART 36, APPENDIX F) MANUFACTURER MTOW ENGINE DATA PROPELLER DATA NOISE LEVEL (dBA) MODEL MLW (1000#) MFR, MODEL NO. SHP EXH MFR, MODEL DIAM (IN) BLADES PITCH RPM MdBA PC CdBA NOTES CESSNA 2.20 LYCOMING 1 160 8 MCCAULEY 80 2 2700 73.60 -1.40 72.2 172N (SEA) 2.18 O-320-H2AD IA175/ETM8042 F CESSNA 2.40 LYCOMING 1 160 8 MCCAULEY 75 2 2700 74.30 -0.50 73.8 172P 0-320-D25 1C160/DTM7557 F CESSNA 2.65 LYCOMING 1 180 8 MCCAULEY 76 2 2700 73.40 0.50 73.9 172RG 2.65 O-360-F1A6 B2D34C220/80VLA-3.5 V CESSNA 2.50 LYCOMING 1 180 8 MCCAULEY 76 2 2700 72.00 -0.30 71.7 177B 2.50 IO-360-A1F6D B2D34C211/82PCA-6 V CESSNA 2.80 LYCOMING 1 200 8 MCCAULEY 78 2 2700 76.30 -0.70 75.6 177RG 2.80 IO-360-AIB6D B2D34C207/78TCA-0 V CESSNA 2.95 TCM 1 230 8 MCCAULEY 88 2 2400 74.00 -2.20 71.8 180K (AMPHIB) 2.95 O-470-U C2A34C204/90DCA-2 V CESSNA 2.80 TCM 1 230 8 MCCAULEY 90 2 2400 73.00 -3.00 70.0 180K (LAND) 2.80 O-470-U C2A34C204/90DCB-0 V CESSNA 2.95 TCM 1 230 8 MCCAULEY 82 2 2400 72.00 -2.90 69.1 182Q 2.95 O-470-U D2A34C203/90DCA-8 V CESSNA 3.10 TCM 1 230 8 MCCAULEY 82 2 2400 72.00 -2.90 69.1 182R 0-470-V D2A34C203/90DCA-8 V CESSNA 3.80 TCM 1 285 8 MCCAULEY 80 3 2700 77.80 -0.10 77.7 207A 3.80 IO-520-F D3A32C90/82NC-2 V CESSNA 3.80 TCM 1 285 8 MCCAULEY 80 3 2700 79.00 0.80 79.8 207A 3.80 IO-520-F D3A32C404/80VA-0 V CESSNA 7.30 PRATT&WHITNEY 600 2 HARTZELL 100 3 1900 72.80 -1.10 71.7 208 7.30 PT6A-114 HC-B3MN-3 V CESSNA 8.00 PRATT&WHITNEY 600 2 HARTZELL 100 3 1900 72.80 0.66 73.5 208 7.80 PT6A-114 HC-B3MN-3 V Page 6 ### Page 320 APPENDIX 7 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CFR PART 36, APPENDIX F) MANUFACTURER MTOW ENGINE DATA PROPELLER DATA NOISE LEVEL (dBA) MODEL MLW (1000#) MFR, MODEL NO. SHP EXH MFR, MODEL DIAM (IN) BLADES PITCH RPM MdBA PC CdBA NOTES CESSNA 8.00 PRATT&WHITNEY 600 2 HARTZELL 100 3 1900 72.80 0.66 73.5 208A 7.80 PT6A-114 HC-B3MN-3 V CESSNA 8.75 PRATT&WHITNEY 600 2 HARTZELL 100 3 1900 72.80 2.31 75.1 208B 8.50 PT6A-114 HC-B3MN-3 V CESSNA 3.80 TCM 1 285 8 MCCAULEY 80 3 2700 79.60 0.30 79.9 210M 3.80 IO-520-L-3A D3A34C404/80VA-0 V CESSNA 3.80 TCM 1 285 8 MCCAULEY 80 3 2700 79.60 0.00 79.6 210N 3.80 IO-520-L-3A D3A34C404/80VA-0 V CESSNA 3.85 TCM 1 285 8 McCAULEY 80 3 2700 79.60 -0.60 79.0 210R 3.85 IO-520-L D3A34C404/8OVA-0 V CESSNA 5.50 TCM 2 285 8 MCCAULEY 77 3 2700 82.00 -2.90 79.1 310R 5.41 IO-520-M 3AF32C87/82NC-5.5 V CESSNA 5.99 TCM 2 300 4 MCCAULEY 77 3 2700 79.60 -1.50 78.1 335 5.99 TSIO-520-EB 3AF32C87/82NC-5.5 V CESSNA 4.63 TCM 2 195 8 MCCAULEY 78 2 2600 78.60 1.30 79.9 337H 4.41 TSIO-360-C D2AF34C310/90DEA-1 V CESSNA 4.63 TCM 2 195 8 MCCAULEY 76 2 2600 78.60 1.30 79.9 337H 4.41 TSIO-360-C D2AF34C307/L78CBA­ V CESSNA 5.99 TCM 2 310 3 MCCAULEY 77 3 2700 83.40 -3.70 79.7 340A 5.99 TSIO-520-N 3AF32C93/82NC-5.5 V CESSNA 5.99 TCM 2 310 4 MCCAULEY 76 3 2700 82.00 -5.50 76.5 340A 5.99 TSIO-520-N 3AF32C93/82NC-5.5 V CESSNA 6.85 TCM 2 300 3 MCCAULEY 76 3 2700 81.60 -2.80 78.8 402B 6.85 TSIO-520-E 3AF32C87M/82NC-5.5 V CESSNA 6.85 TCM 2 325 4 MCCAULEY 76 3 2700 80.80 -2.20 78.6 402C 6.85 TSIO-520-UB 3AF32C92N/82NC-6.5 V Page 7 ### Page 321 APPENDIX 7 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CFR PART 36, APPENDIX F) MANUFACTURER MTOW ENGINE DATA PROPELLER DATA NOISE LEVEL (dBA) MODEL MLW (1000#) MFR, MODEL NO. SHP EXH MFR, MODEL DIAM (IN) BLADES PITCH RPM MdBA PC CdBA NOTES CESSNA 6.85 TCM 2 310 4 MCCAULEY 77 3 2600 77.20 -2.10 75.1 402C 6.85 TSIO-520-VB 3AF32C93/82NC-5.5 V CESSNA 8.40 TCM 2 375 4 MCCAULEY 90 3 3350 81.60 -2.70 78.9 404 8.09 GTSIO-520-M 3FF32C501/90UMB-0 V CESSNA 8.40 PRATT&WHITNEY 2 550 4 HARTZELL 93 3 2000 81.10 -5.00 76.1 404 8.10 PT6A-34 HCB3TN-3B/T10173-8 V CESSNA 9.36 PRATT&WHITNEY 2 500 1 MCCAULEY 93 3 1900 75.00 -3.00 72.0 406 9.36 PT6A-112 3GFR34C701/93KB-0 V CESSNA 6.75 TCM 2 298 4 MCCAULEY 77 3 2600 79.10 -2.50 76.6 414A 6.75 TSIO-520-N 3AF32C93/82NC-5.5 V CESSNA 7.45 TCM 2 375 4 MCCAULEY 90 3 3350 80.30 -3.60 76.7 421C 7.21 GTSIO-520-L 3FF32C501/90UMB-0 V CESSNA 8.20 PRATT&WHITNEY 2 450 4 MCCAULEY 93 3 1900 75.70 -4.30 71.4 425 8.00 PT6A-112 36FR34C701/93KB-0 V CESSNA 8.20 PRATT&WHITNEY 2 450 4 HARTZELL 93 3 1900 75.70 -4.30 71.4 425 8.00 PT6A-112 HC-B3TN-3C/T10178B­ V CESSNA 8.60 PRATT&WHITNEY 2 450 4 HARTZELL 93 3 1900 75.70 -3.40 72.3 425 8.00 PT6A-112 HC-B3TN-3C/T10178B­ V CESSNA 9.85 AIRESEARCH 2 636 4 MCCAULEY 90 3 1990 78.00 -4.00 74.0 441 9.36 TPE331-8-401S 36FR34C601/93JA V CESSNA 9.85 AIRESEARCH 2 636 4 HARTZELL 90 3 1990 78.00 -4.00 74.0 441 9.36 TPE331-8-401S HC-B3TN-5E/T10178-1 V CESSNA 3.27 TCM 1 285 8 MCCAULEY 80 3 2700 78.90 -1.20 77.7 A185F (AMPHIB) 3.12 IO-520-D D3A34C403/80VA-0 V CESSNA 3.32 TCM 1 285 8 MCCAULEY 80 3 2700 78.90 -1.00 77.9 A185F (FLOAT) 3.32 IO-520-D-24 D3A32C90/82NC-2 V Page 8 ### Page 322 APPENDIX 7 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CFR PART 36, APPENDIX F) MANUFACTURER MTOW ENGINE DATA PROPELLER DATA NOISE LEVEL (dBA) MODEL MLW (1000#) MFR, MODEL NO. SHP EXH MFR, MODEL DIAM (IN) BLADES PITCH RPM MdBA PC CdBA NOTES CESSNA 3.35 TCM 1 285 8 MCCAULEY 80 3 2700 78.90 -1.00 77.9 A185F (LAND) 3.35 IO-520-D D3A34C403/80VA-0 V CESSNA 3.30 TCM 1 260 8 MCCAULEY 80 3 2700 77.30 -1.50 75.8 A188B 3.30 IO-520-D D3A32C408/82NDA-2 V CESSNA 4.00 TCM 1 285 4 MCCAULEY 80 3 2600 77.10 0.90 78.0 P210N 3.80 TSIO-520-P D3A34C402/90DFA-10 V CESSNA 4.00 PRATT&WHITNEY 1 450 2 HARTZELL 77 3 1900 68.70 -2.00 66.8 P210N ADVANCED PT6A-135 HC-83TN-3C/T10282K­ V CESSNA 4.10 TCM 1 325 4 McCAULEY 80 3 2700 80.20 -0.80 79.4 P210R 4.10 T510-520-CE D3A36C410/80VM8-0 V CESSNA 4.70 TCM 2 208 4 MCCAULEY 76 2 2600 80.80 -1.10 79.7 P337H 4.45 TSIO-360-C D2AF34C305/L78CBA­ V CESSNA 4.70 TCM 2 208 4 MCCAULEY 78 2 2600 80.80 -1.10 79.7 P337H 4.45 TSIO-360-C D2AF34C308/90DEA-1 V CESSNA 2.55 TCM 1 195 8 MCCAULEY 76 2 2600 74.70 -0.60 74.1 R172K (LAND) 2.55 IO-360-K 2A34C203/90DCA-14 V CESSNA 2.55 TCM 1 195 8 MCCAULEY 80 2 2600 76.40 -1.40 75.0 R172K (SEA) 2.55 IO-360-K 2A34C203/90DCA-10 V CESSNA 3.10 LYCOMING 1 235 8 MCCAULEY 82 2 2400 72.70 -2.00 70.7 R182 3.10 O-540-J3C5D B2D34C214/90DHB-8 V CESSNA 3.10 LYCOMING 1 235 8 MCCAULEY 79 3 2400 70.30 -2.00 68.3 R182 3.10 O-540-J3C5D B3D32C407/82NDA-3 V CESSNA 3.10 LYCOMING 1 235 4 MCCAULEY 79 3 2400 69.50 -0.70 68.8 T182 3.10 O-540-L3C5D B3D32C407/82NDA-3 V CESSNA 3.10 LYCOMING 1 235 4 MCCAULEY 82 2 2400 73.20 -0.70 72.5 T182 3.10 O-540-L3C5D B2D34C219/90DHB-8 V Page 9 ### Page 323 APPENDIX 7 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CFR PART 36, APPENDIX F) MANUFACTURER MTOW ENGINE DATA PROPELLER DATA NOISE LEVEL (dBA) MODEL MLW (1000#) MFR, MODEL NO. SHP EXH MFR, MODEL DIAM (IN) BLADES PITCH RPM MdBA PC CdBA NOTES CESSNA 3.80 TCM 1 285 4 MCCAULEY 80 3 2600 77.90 -1.60 76.3 T207A 3.80 TSIO-520-G-1A 3A32C401/90DFA-10 V CESSNA 3.80 TCM 1 285 4 MCCAULEY 80 3 2600 77.40 -1.60 75.8 T210M 3.80 TSIO-520-H-4A D3A34C-102/90DFA-1 V CESSNA 4.00 TCM 1 285 4 MCCAULEY 80 3 2600 77.40 0.00 77.4 T210N 3.80 TSIO-520-R D3A34C402/90DFA-10 V CESSNA 4.10 TCM 1 325 4 McCAULEY 80 3 2700 80.20 -0.80 79.4 T210R 4.10 T510-520-CE D3A36C410/80VM8-0 V CESSNA 5.15 TCM 2 250 4 MCCAULEY 74 3 2400 76.50 -2.20 74.3 T303 5.00 TSIO-520-AE 3AF32C506/82NEB-8 V CESSNA 5.50 TCM 2 285 4 MCCAULEY 78 3 2700 80.90 -3.20 77.7 T310R 5.41 TSIO-520-BB 3AF32C87/82NC-4 V CESSNA 4.63 TCM 2 195 4 MCCAULEY 76 2 2600 79.40 -1.00 78.4 T337H 4.40 TSIO-360-H D2AF34C305/L78CBA­ V CESSNA 4.63 TCM 2 195 4 MCCAULEY 78 2 2600 79.40 -1.00 78.4 T337H 4.42 TSIO-360-H D2AF34C308/90DEA-1 V CESSNA 3.10 LYCOMING 1 235 4 MCCAULEY 82 2 2400 73.80 -1.20 72.6 TR182 3.10 O-540-L3C5D B2D34C217/90DHB-8 V CESSNA 3.10 LYCOMING 1 235 4 MCCAULEY 79 3 2400 70.60 -1.20 69.4 TR182 3.10 O-540-L3C5D B3D32C407/82NDA-3 V CESSNA 3.60 TCM 1 285 4 MCCAULEY 80 3 2600 78.50 -3.10 75.4 TU206G 3.60 TSIO-520-M D3A34C402/90DFA-10 V CESSNA 3.60 TCM 1 285 4 MCCAULEY 80 3 2600 78.00 1.20 79.2 TU206G (AMPHIB) 3.60 TSIO-520-M D3A34C402/90DFA-10 V CESSNA 3.60 TCM 1 285 8 MCCAULEY 80 3 2700 77.90 -0.40 77.5 U206G 3.60 IO-520-F D3A34C404/80VA-0 V Page 10 ### Page 324 APPENDIX 7 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CFR PART 36, APPENDIX F) MANUFACTURER MTOW ENGINE DATA PROPELLER DATA NOISE LEVEL (dBA) MODEL MLW (1000#) MFR, MODEL NO. SHP EXH MFR, MODEL DIAM (IN) BLADES PITCH RPM MdBA PC CdBA NOTES CESSNA 3.60 TCM 1 285 8 MCCAULEY 80 3 2700 79.80 -0.40 79.4 U206G (LAND) 3.60 IO-520-F-9 D3A34C404/80VA-0 V CESSNA 3.50 TCM 1 285 8 MCCAULEY 80 3 2700 80.20 -0.80 79.4 U206G(SEAPLANE) 3.50 IO-520-F D3A34C404/80VA-0 V CLASSIC AIRCRAFT 2.65 JACOBS 245 SENSENICH 96 2 2050 75.10 -2.30 72.8 WACO F5 2.65 R-755B2M W96JA72 F CLASSIC AIRCRAFT 2.77 JACOBS 275 SENSENICH 90 2 2200 76.30 -0.70 75.6 WACO F5 2.77 R-755B2M W90T6JA72 F CURTISS-WRIGHT 2.45 LYCOMING 1 225 2 HAMILTON STD 102 2 2050 75.20 -1.60 75.6 TRAVEL AIR 4000 2.45 R-680E3B 2B20/6135A F DEHAVILLAND 8.00 PRATT&WHITNEY 1 HARTZELL 102 3 76.30 -0.30 76.0 DHC-3 W/SAE STC PT6A-135/135A HC-B3TN-3C/T10282 V DORNIER 12.50 GARRETT 2 715 HARTZELL 106 4 73.5 228-100 12.50 TPE331-5-252D HC-B4TN-5ML/LT EMBRAER 12.50 PRATT&WHITNEY 2 750 HARTZELL 93 3 2002 78.70 -1.40 77.3 EMB-110 12.02 PT6A-34 HC-BT3N-3C/T10178H­ V FAIRCHILD 12.50 GARRETT 2 1000 MCCAULEY 106 4 1591 77.23 -1.94 75.3 SA226-AT TPE331-11U-612G (X)-L106LA-0 V FAIRCHILD 12.50 GARRETT 2 806 HARTZELL 102 3 1920 83.58 -3.84 79.7 SA226-AT TPE331-3U-303G T10282HB V FAIRCHILD 12.50 AIRESEARCH 2 840 HARTZELL 98 4 2000 84.80 -3.40 81.4 SA226-T TPE331-3U-303G T10282HDB-4R V FAIRCHILD 12.50 AIRESEARCH 2 900 4 HARTZELL 106 4 1591 77.40 -4.60 72.8 SA226-T(B) 12.50 TPE331-1OU-501G HC-B4TN-5EL/LT1028 V FAIRCHILD 13.23 AIRESEARCH 2 806 HARTZELL 102 3 1920 80.97 -2.50 78.4 SA226-TC TPE331-3UW-303G T10282HB V Page 11 ### Page 325 APPENDIX 7 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CFR PART 36, APPENDIX F) MANUFACTURER MTOW ENGINE DATA PROPELLER DATA NOISE LEVEL (dBA) MODEL MLW (1000#) MFR, MODEL NO. SHP EXH MFR, MODEL DIAM (IN) BLADES PITCH RPM MdBA PC CdBA NOTES FAIRCHILD 12.50 AIRESEARCH 2 806 4 HARTZELL 102 3 1920 83.58 -3.84 79.7 SA226-TC 12.50 TPE331-3UW-303G HCB3 TN-5/T10282HB V FAIRCHILD 14.50 GARRETT 2 1000 MCCAULEY 106 4 1591 77.23 -1.94 75.3 SA227-AC TPE331-11U-612G (X)-L106LA-0 V FAIRCHILD 16.00 GARRETT 2 1000 MCCAULEY 106 4 1591 77.23 0.97 78.2 SA227-AC TPE331-11U-612G (X)-L106LA-0 V FAIRCHILD 14.50 GARRETT 2 1000 DOWTY-ROTOL 106 4 1591 77.23 -2.43 74.8 1 SA227-AC 14.00 TPE331-11U-601G R321/4-82-F/8 V FAIRCHILD 16.00 GARRETT 2 1000 DOWTY-ROTOL 106 4 1591 77.23 0.97 78.2 1 SA227-AC 15.50 TPE331-11U-601G R321/4-82-F/8 V FAIRCHILD 16.00 GARRETT 2 1000 DOWTY-ROTOL 106 4 1591 77.40 0.32 77.7 SA227-AT TPE331-11U-601G (C)R.321/4-82-F/8 V FAIRCHILD 16.00 GARRETT 2 1000 MCCAULEY 106 4 1591 77.40 0.32 77.7 SA227-AT TPE331-11U-612G (X)-L106LA-0 V FAIRCHILD 14.50 AIRESEARCH 2 1000 4 DOWTY ROTOL 106 4 1591 77.23 -1.94 75.3 1 SA227-AT 14.00 TPE331-11U-601G (C)R321/4-82-F/8 V FAIRCHILD 16.00 GARRETT 2 1000 MCCAULEY 106 4 1591 77.40 -0.90 76.5 SA227-BC TPE331-12UA-701G (X)-L106LA-0 V FAIRCHILD 12.50 AIRESEARCH 2 900 4 DOWTY ROTOL 106 4 1591 77.42 -4.62 72.8 SA227-TT 12.50 TPE331-1OU-503G (C)R324/4-82-F/9 V FAIRCHILD 13.23 AIRESEARCH 2 900 4 DOWTY ROTOL 106 4 1591 77.42 -4.08 73.3 1 SA227-TT 13.23 TPE331-1OU-503G (C)R324/4-82-F/9 V FUJI HEAVY IND. 6.75 LYCOMING 2 340 4 HARTZELL 79 3 2500 80.80 -3.20 77.6 700 6.60 TI0-540-R2AD HC-E3YR-2ATF/FC846 V FUJI HEAVY IND. 8.30 LYCOMING 2 450 4 HARTZELL 93 3 2133 82.70 -3.30 79.4 710 8.30 TIG0-541-D1B HC-C3YN-2LDUF/FJC- Page 12 ### Page 326 APPENDIX 7 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CFR PART 36, APPENDIX F) MANUFACTURER MTOW ENGINE DATA PROPELLER DATA NOISE LEVEL (dBA) MODEL MLW (1000#) MFR, MODEL NO. SHP EXH MFR, MODEL DIAM (IN) BLADES PITCH RPM MdBA PC CdBA NOTES GRUMMAN 5.50 LYCOMING 2 HARTZELL 87 3 82.80 -3.20 79.6 G-44/SCAN 30 TIO/LTIO-540-J2BD HC-C3YR-2UF/HC-C3 V GULFSTREAM AMERICAN 2.80 AVCO LYCOMING 1 200 3 HARTZELL 77 2 2700 75.10 -0.50 74.6 112B 2.80 IO-360-C1D6 HC-E2YR-1BF/F8467-7 V GULFSTREAM AMERICAN 2.85 AVCO LYCOMING 1 210 4 HARTZELL 77 2 2575 76.10 -1.30 74.8 112TC 2.76 T0-360-C1A6 HC-E2YR-1BF/F8467-7 V GULFSTREAM AMERICAN 2.95 AVCO LYCOMING 1 210 4 HARTZELL 77 2 2575 76.10 -1.30 74.8 112TCA 2.95 T0-360-C1A6 HC-E2YR-18F/F8467-7 V GULFSTREAM AMERICAN 3.14 AVCO LYCOMING 1 260 3 HARTZELL 77 2 2700 79.70 -1.20 78.5 114 3.14 I0-540-T4A5D HC-C2YR-1BF/F8467-7 V GULFSTREAM AMERICAN 3.25 AVCO LYCOMING 1 260 3 MCCAULEY 77 3 2700 79.70 -1.20 78.5 114A 3.13 I0-540-T4B5D B3D34C405/90DFA-13 V GULFSTREAM AMERICAN 10.25 AIRESEARCH 2 700 4 HARTZELL 106 3 1591 76.40 -5.00 71.4 690 9.59 TPE331-5-251K HC-B3TN-5FLLT10282 V GULFSTREAM AMERICAN 10.25 AIRESEARCH 2 700 4 HARTZELL 106 3 1591 76.40 -5.00 71.4 690A 9.59 TPE331-5-251K HC-B3TN-5FLLT1028H V GULFSTREAM AMERICAN 10.32 AIRESEARCH 2 700 4 HARTZELL 106 3 1591 76.40 -5.00 71.4 690B 9.68 TPE331-5-251K HC-B3TN-5FLLT10282 V GULFSTREAM AMERICAN 10.32 AIRESEARCH 2 700 4 DOWTY ROTOL 106 3 1591 76.40 -5.00 71.4 690C 9.68 TPE331-5-254K (C)R306/3-82-F/7(C)VP V GULFSTREAM AMERICAN 10.70 AIRESEARCH 2 737 4 DOWTY ROTOL 106 3 1591 76.40 -5.00 71.4 690D 10.55 TPE331-5-254K (C)R306/3-82-F/7(C)VP V GULFSTREAM AMERICAN 10.32 AIRESEARCH 2 700 4 DOWTY ROTOL 106 3 1591 76.40 -5.00 71.4 695 9.68 TPE331-10-501K (C)R306/3-82-F/7(C)VP V GULFSTREAM AMERICAN 11.20 AIRESEARCH 2 700 4 DOWTY ROTOL 106 3 1591 71.80 0.00 71.8 695A 10.56 TPE331-10-501K (C)R306/3-82-F/7(C)VP V Page 13 ### Page 327 APPENDIX 7 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CFR PART 36, APPENDIX F) MANUFACTURER MTOW ENGINE DATA PROPELLER DATA NOISE LEVEL (dBA) MODEL MLW (1000#) MFR, MODEL NO. SHP EXH MFR, MODEL DIAM (IN) BLADES PITCH RPM MdBA PC CdBA NOTES GULFSTREAM AMERICAN 6.95 AVCO LYCOMING 2 340 4 HARTZELL 79 3 2500 77.80 -2.40 75.4 700 6.59 TI0-540-R2AD HC-E3YR-2AFT/FC846 V GULFSTREAM AMERICAN 1.54 LYCOMING 1 108 7 MCCAULEY 71 2 2600 66.30 0.60 66.9 AA-1B 1.54 0-235-C2C SCM1A105/7157 F GULFSTREAM AMERICAN 1.54 LYCOMING 1 108 7 MCCAULEY 71 2 2600 66.70 1.10 67.8 AA-1B 1.54 0-235-C2C SCM1A105/7154 F GULFSTREAM AMERICAN 1.57 LYCOMING 1 115 7 SENSENICH 71 2 2700 68.30 0.50 68.8 AA-1C 1.57 0-235-L2C 72CK-0-56 F GULFSTREAM AMERICAN 3.78 LYCOMING 2 160 HARTZELL 73 2 2700 74.20 -2.20 72.0 GA-7 3.78 0-320-D1D F2YL-2VFFC7663D-3 V JETSTREAM 15.21 GARRETT 2 940 DOWTY ROTOL 106 4 1591 74.10 -2.40 71.7 1 JETSTREAM 31 14.55 TPE331-10UF/UR513H R333/4-82-F/12 V JETSTREAM 14.60 AIRESEARCH 2 900 DOWTY ROTOL 106 4 1591 74.40 -3.50 70.9 1 JETSTREAM 31 14.60 TPE331-IOU-501H R333/4-82-F/12 V JETSTREAM 16.20 GARRETT 2 1020 DOWTY ROTOL 106 4 1591 76.20 -3.20 73.0 JETSTREAM 3201 15.60 TPE331-12UA(R)701H R333/4-82-F/12 V MAULE 2.30 LYCOMING 1 175 3 HARTZELL 76 2 2700 72.30 0.00 72.3 M-5-180C/-180TC 2.30 0-360-C1F HC-C2YR-1BF/F7666A V MAULE 2.30 LYCOMING 1 190 3 HARTZELL 77 2 2600 73.30 0.00 73.3 M-5-200 2.30 IO-360-J1A6D HC-E2YR-1BF/F8468A V MAULE 2.30 LYCOMING 1 210 HARTZELL 74 2 2575 74.60 -1.00 73.6 M-5-210TC 2.30 I0-360-C1A-6D HC-E2YR-1BF/F8467-7 V MAULE 2.75 LYCOMING 1 235 3 HARTZELL 81 2 2400 74.70 0.90 75.6 M-5-235 2.75 0-540-J1A5D HC-C2YR-1BF/F8468A V MAULE 2.30 LYCOMING 1 235 HARTZELL 78 2 72.60 -5.00 67.6 M-5-235C 2.30 0-540-J1A5D/-W1A5D HC-C2YR-1BF/F8468A V Page 14 ### Page 328 APPENDIX 7 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CFR PART 36, APPENDIX F) MANUFACTURER MTOW ENGINE DATA PROPELLER DATA NOISE LEVEL (dBA) MODEL MLW (1000#) MFR, MODEL NO. SHP EXH MFR, MODEL DIAM (IN) BLADES PITCH RPM MdBA PC CdBA NOTES MAULE 2.30 LYCOMING 1 175 3 HARTZELL 76 2 2600 70.90 0.90 71.8 M-6-180 2.30 0-360-CIF HC-C2YR-1BF/F7666A V MAULE 2.30 LYCOMING 1 235 HARTZELL 78 2 2400 72.60 -5.00 67.6 M-6-235 2.30 0-540-J1A5D/-W1A5D HC-E2YR-1BF/F8468A V MAULE 2.50 LYCOMING 1 235 HARTZELL 81 2 2700 71.3 M-6-235 2.50 O-540-J1A5D HC-C2YR-1BF/F8468A V MAULE 2.50 LYCOMING 1 235 3 HARTZELL 78 2 2400 72.60 -0.30 72.3 M-7-235 2.50 O-540-J1A5D HC-C2YR-1BF/F8468A V MAULE 2.50 LYCOMING 1 235 3 HARTZELL 81 2 2400 74.70 -2.50 72.2 M-7-235 2.50 O-540-J1A5D HC-C2YR-1BF/F8468A V MITSUBISHI 10.47 AIRESEARCH 2 665 4 HARTZELL 98 4 1591 77.40 -2.90 74.8 MU-2B-40 9.96 TPE331-10-501 HC-B4TN-5DL/LT1028 V MITSUBISHI 11.56 AIRESEARCH 2 715 4 HARTZELL 98 4 1591 77.70 -1.40 76.5 MU-2B-60 11.60 TPE331-10-501M HC-B4TN-5DL/LT1028 V MOONEY 2.74 LYCOMING 1 192 MCCAULEY 74 2 2700 75.30 -1.30 74.0 M20J 2.74 IO-360-A3B6D B2D34C212/78CDA-4 V MOONEY 2.90 PORSCHE 7 HARTZELL 74 3 76.6 M20L 2.92 PRM3200N03 BHC-J2YF-1C/B7421 V MOONEY AIRCRAFT 2.90 TELEDYNE 1 210 4 MCCAULEY 74 2 2700 76.60 -1.10 75.4 M20K 2.90 TSI0-360-GB1 2A34C216/90DHB-16E V PARTENAVIA 4.39 AVCO LYCOMING 2 HARTZELL 76 2 2575 75.4 P68-TC 4.39 TO-360-C1A60 HC-C2YK-2CUF V PIPER 1.75 LYCOMING 1 150 7 SENSENICH 74 2 2700 69.00 -3.10 65.9 PA-18-150 1.75 0-320-A2B M74DM6-0-56 F PIPER 5.20 LYCOMING 2 250 6 HARTZELL 77 2 2575 76.80 -1.10 75.7 PA-23-250 4.94 I0-540-C4B5 HC-E2YR-28465-7R V Page 15 ### Page 329 APPENDIX 7 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CFR PART 36, APPENDIX F) MANUFACTURER MTOW ENGINE DATA PROPELLER DATA NOISE LEVEL (dBA) MODEL MLW (1000#) MFR, MODEL NO. SHP EXH MFR, MODEL DIAM (IN) BLADES PITCH RPM MdBA PC CdBA NOTES PIPER 5.20 LYCOMING 2 250 4 HARTZELL 77 2 2575 77.00 -0.80 76.2 PA-23T-250 4.94 TIO-540-C1A HC-E2YR-28465-7R V PIPER 2.33 LYCOMING 1 160 5 SENSENICH 74 2 2700 71.40 0.60 72.0 PA-28-161 2.33 0-320-D3G 74DM6-0-60 F PIPER 2.55 LYCOMING 1 180 5 SENSENICH 76 2 2700 73.40 0.50 73.9 PA-28-181 2.55 O-360-A4M 76EM8S5-062 F PIPER 3.00 LYCOMING 1 235 5 HARTZELL 80 2 2400 72.50 0.40 72.9 PA-28-236 3.00 0-540-J3A5D HC-F2YR-1F/F8468A-4 V PIPER 2.65 LYCOMING 1 200 MCCAULEY 74 2 2700 75.50 0.00 75.5 PA-28R-200 2.65 IO-360-CIC B2D34C213 V PIPER 2.65 LYCOMING 1 200 HARTZELL 74 2 2700 75.50 0.00 75.5 PA-28R-200 2.65 IO-360-CIC HC-C2YK-1(1)/F766A­ V PIPER 2.90 CONTINENTAL 1 200 2 HARTZELL 76 2 2575 69.10 0.50 69.6 PA-28R-201T 2.90 TSIO-360-FB PHC-C3YF-1F/7663-2R V PIPER 2.75 LYCOMING 1 200 5 MCCAULEY 74 2 2700 74.40 1.10 75.5 PA-28RT-201 2.75 I0-360-C1C6 B2D34213/90DHA-16 V PIPER 2.90 CONTINENTAL 1 200 4 HARTZELL 76 3 2575 72.50 0.30 72.8 PA-28RT-201T 2.90 TSIO-360F PHC-C3YF-1F/F7663-2 V PIPER 2.90 CONTINENTAL 1 200 2 HARTZELL 76 2 2575 69.10 0.30 69.4 PA-28RT-201T 2.90 TSIO-360-F BHC-C2YF-1F/F8459A­ V PIPER 6.50 LYCOMING 2 275 4 HARTZELL 80 3 2400 77.00 -1.60 75.4 PA-31 6.50 TIO-540-2AC HC-E3YR-2ATF FC846 V PIPER 6.50 LYCOMING 2 275 4 HARTZELL 80 3 2400 78.00 -1.10 76.9 PA-31-325 6.50 TI0-540-F2BD HC-E3YR-2ATF FC846 V PIPER 7.01 LYCOMING 2 315 4 HARTZELL 80 3 2400 78.00 0.90 78.9 PA-31-350 7.01 TIO-540-J2BD HC-E3YR-2ATF FC846 V Page 16 ### Page 330 APPENDIX 7 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CFR PART 36, APPENDIX F) MANUFACTURER MTOW ENGINE DATA PROPELLER DATA NOISE LEVEL (dBA) MODEL MLW (1000#) MFR, MODEL NO. SHP EXH MFR, MODEL DIAM (IN) BLADES PITCH RPM MdBA PC CdBA NOTES PIPER 7.80 PRATT&WHITNEY 2 620 4 HARTZELL 93 3 1900 76.50 -5.00 71.5 PA-31P 7.80 PT6A-135 HC-B3TN-3C/T10178-8 V PIPER 9.00 PRATT&WHITNEY 2 620 4 HARTZELL 93 3 2000 79.20 -5.00 74.2 PA-31T 9.00 PT6A-28 HC-B3TN-3B/T-10173B V PIPER 8.70 PRATT&WHITNEY 2 455 4 HARTZELL 93 3 2000 76.60 -1.60 75.0 PA-31T1 8.70 PT6A-11 HC-B3TN-3B/T-10173B V PIPER 9.47 PRATT&WHITNEY 2 620 4 HARTZELL 93 3 1900 79.20 -2.10 77.1 PA-31T2 PT6A-135 HC-B3TN-3B/T-10173B V PIPER 9.00 PRATT&WHITNEY 2 455 1 HARTZELL 93 3 2200 76.60 -1.00 75.6 PA-31T3 PT6A-11 HC-B3TN-3B/T-10173K V PIPER 8.97 PRATT&WHITNEY 2 620 4 HARTZELL 93 3 2000 78.20 -4.00 74.2 PA-31T-62 8.97 PT6A-28 HC-BTN-3B V PIPER 3.40 LYCOMING 1 300 HARTZELL 80 2 2700 80.50 -1.20 79.3 PA-32-300 3.40 I0-540-K1A5 HC-C2YR-1( )F/F8475D V PIPER 3.60 LYCOMING 1 300 5 HARTZELL 78 3 2700 78.10 -0.60 77.5 PA-32-301 3.60 I0-540-K1G5 HC-C3YR-1( )F/F7663R V PIPER 3.60 LYCOMING 1 294 5 HARTZELL 80 2 2600 77.30 -0.60 76.7 PA-32-301 3.60 IO-540-K1G5D HC-C2YR-1( )F/F8475D V PIPER 3.60 LYCOMING 1 300 4 HARTZELL 78 3 2700 76.10 -1.30 74.8 PA-32-301T 3.60 TI0-540-SIAD HC-E3YR-1( )F/F7673D V PIPER 3.60 LYCOMING 1 294 4 HARTZELL 80 2 2575 75.70 -1.30 74.4 PA-32-301T 3.60 TIO-540-SIAD HC-E2YR-1( )F/F8477­ V PIPER 3.60 LYCOMING 1 300 5 HARTZELL 78 3 2700 78.10 0.30 78.4 PA-32R-301 3.60 IO-540-K1G5D HC-C3YR-1( )F/F7663R V PIPER 3.60 LYCOMING 1 294 5 HARTZELL 80 2 2600 77.30 0.30 77.6 PA-32R-301 3.60 IO-540-K1G5D HC-C2YR-1( )F/F8475D V Page 17 ### Page 331 APPENDIX 7 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CFR PART 36, APPENDIX F) MANUFACTURER MTOW ENGINE DATA PROPELLER DATA NOISE LEVEL (dBA) MODEL MLW (1000#) MFR, MODEL NO. SHP EXH MFR, MODEL DIAM (IN) BLADES PITCH RPM MdBA PC CdBA NOTES PIPER 3.60 LYCOMING 1 294 4 HARTZELL 80 2 2575 75.70 0.40 76.1 PA-32R-301T 3.60 TIO-540-SAID HC-E2YR-1( )F/F8477­ V PIPER 3.60 LYCOMING 1 300 4 HARTZELL 78 3 2700 76.10 0.40 76.5 PA-32R-301T 3.60 TIO-540-SAID HC-E3YR-1/F7673 V PIPER 3.60 LYCOMING 1 300 HARTZELL 80 2 2400 75.40 0.00 75.4 PA-32RT-300 3.60 IO-540-S1AD HC-E2YR-1BF/F8477-4 V PIPER 4.60 CONTINENTAL 2 200 4 HARTZELL 76 2 2575 75.70 -2.20 73.5 PA-34-200T 4.30 TS10-360-E FC8459-8R/FJC8459-8R V PIPER 4.60 TELEDYNE 2 200 4 MCCAULEY 76 3 2575 78.60 -2.20 76.4 PA-34-200T 4.30 TS10-360-E/EB 80HA-4/L80HA-4 V PIPER 4.70 CONTINENTAL 2 200 4 HARTZELL 76 2 2600 74.20 -2.80 71.4 PA-34-220T 4.50 TSIO-360-KB BHC-C2YF-2CKUF/FC V PIPER 4.70 CONTINENTAL 2 200 4 MCCAULEY 76 3 2600 77.00 -2.80 74.2 PA-34-220T 4.50 TSIO-360-KB 3AF32C50B/82NFA-6 V PIPER 1.68 LYCOMING 1 112 5 SENSENICH 72 2 2600 67.80 0.00 67.8 PA-38-112 1.68 O-235-L2C 72CK-O-56 F PIPER 11.20 PRATT+WHITNEY 2 720 4 HARTZELL 95 3 2000 80.30 -3.50 76.8 PA-42 10.23 PT6A-41 HC-B3TN-3B/T10173A V PIPER 12.05 GARRETT 2 1000 4 DOWTY ROTOL 106 4 1540 75.10 -5.00 70.1 PA-42-1000 11.10 TPE331-14A-801Y R339/4-123-F/8RH R34 V PIPER 3.80 LYCOMING 2 180 5 HARTZELL 73 2 2700 77.20 -2.50 74.7 PA-44-180 3.80 0-360-A1H6 HC-C2Y(K,R)-2CEUF/F V PIPER 3.80 LYCOMING 2 180 5 HARTZELL 73 3 2700 78.10 -2.50 75.6 PA-44-180 3.80 O-360-E1A6D HC-C3YR-2EUF/FC-76 V PIPER 3.92 LYCOMING 2 180 4 HARTZELL 73 3 2575 74.70 -2.30 72.4 PA-44-180T 3.80 TO-360-E1A6D HC-C3YR-2EUF FC-76 V Page 18 ### Page 332 APPENDIX 7 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CFR PART 36, APPENDIX F) MANUFACTURER MTOW ENGINE DATA PROPELLER DATA NOISE LEVEL (dBA) MODEL MLW (1000#) MFR, MODEL NO. SHP EXH MFR, MODEL DIAM (IN) BLADES PITCH RPM MdBA PC CdBA NOTES PIPER 3.92 LYCOMING 2 180 4 HARTZELL 74 2 2575 73.80 -2.30 71.5 PA-44-180T 3.80 TO-360-E1A6D HC-C2YR-2CUF FC766 V PIPER 4.10 CONTINENTAL 310 4 HARTZELL 80 2 74.50 0.00 74.5 PA-46-310P 3.90 TSIO-520-BE BHC-C2YF-1BF/F8052 V PIPER 4.30 LYCOMING 350 4 HARTZELL 80 2 2500 75.20 -0.50 74.7 PA-46-350P 4.10 TIO-540-AE2A HC-I2YR-1 V PIPER 5.49 LYCOMING 2 284 HARTZELL 78 3 2520 82.40 -2.40 80.0 PA-600A 5.49 IO-540-K1J5 HC-C3YR-2UF FG-848 V PIPER 5.97 LYCOMING 2 290 HARTZELL 78 2 81.50 -1.70 79.8 PA-601P 5.97 I0-540-S1A5/-P1A5 HC-C3YR-2/C8468-8R V PIPER 6.00 LYCOMING 2 290 4 HARTZELL 78 3 2425 81.90 -2.60 79.3 PA-602P 6.00 IO-540-AA1A5 HC-3YR-2UF/FC8468-8 V PIPER 6.32 LYCOMING 2 350 4 HARTZELL 76 3 2500 80.80 -1.90 78.9 PA-60-700P TIO-540-U2A HC-C3YR-2UF/FC7451 V SIAI MARCHETTI 2.43 AVCO LYCOMING 1 HARTZELL 76 2700 73.2 F-260C 2.43 AEIO-540-D4A5 HC-C2YK-1BF V SIAI MARCHETTI 7.50 ALLISON 2 HARTZELL 90 3 2030 74.3 SF 600 7.50 250-B17C HC-B3TF-7A/T10173-1 V SIAI MARCHETTI 2.56 ALLISON 320 4 HARTZELL 76 3 2030 77.00 -5.00 72.0 SF260 2.56 250-B17D HC-B3TF-7A SOCATA 2.54 LYCOMING 1 180 HARTZELL 74 2 2700 70.7 TB 10 2.41 O-360-A1-AD HC-C2YK-1BF/F 7666 V SOCATA 3.09 LYCOMING 1 250 HARTZELL 80 2 2575 74.0 TB 20 2.94 IO-540-C4D5D HC-C2YK-IBF/F 8477-4 V SOCATA 3.09 LYCOMING 1 310 HARTZELL 80 2 2575 75.4 TB 21 2.94 IO-540-AB1AD HC-C2YK-IBF/F 8477-4 V Page 19 ### Page 333 APPENDIX 7 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CFR PART 36, APPENDIX F) MANUFACTURER MTOW ENGINE DATA PROPELLER DATA NOISE LEVEL (dBA) MLWMODEL MFR, MODEL NO. SHP EXH MFR, MODEL DIAM BLADES RPM MdBA PC CdBA NOTES (1000#) (IN) PITCH SOCATA 2.34 LYCOMING 1 160 SENSENICH 74 2 2700 72.2 TB 9 2.34 O-320-D2A 74 DM 658-O-54 F TAYLORCRAFT 1.20 AVCO LYCOMING 1 118 3 HENDRICKSON 71 2 2500 72.60 -5.00 67.6 BC-12D 1.20 I0-360-E2A H73-A50 F TAYLORCRAFT 1.50 CONTINENTAL 1 100 5 MCCAULEY 69 2 2750 69.10 -0.70 68.4 F-19 1.50 0-200-A 1A105/SCM6950 F TAYLORCRAFT 1.50 LYCOMING 1 112 5 SENSENICH 71 2 2800 69.00 -0.20 68.8 F-21 1.50 0-235-L2C 72CK-0-50 F TRIDENT 3.80 TELEDYNE 1 232 7 HARTZELL 84 3 4000 78.20 -1.00 77.2 TR-1 3.80 TIARA 6-285-C4 HC-H3YF-3LF/FL-C96 V Page 20 ### Page 334 11/15/01 AC36-1H Appendix 7 Appendix 7 Notes 1 Maximum Takeoff Weight Greater Than 12,500 lb. - Aircraft Certificated To FAR Part 41 Or FAR Part 23 Commuter Category Exhaust Configurations (Reciprocating Engines) 1 Stub Pipes 2 Small Collector, Short Exhaust Pipe 3 Baffles In Collector and/or Cones In Exhaust Pipe 4 Turbine Or Turbocharger 5 Heat Muff 6 Collector Wraparound Manifold Straight Pipe 7 Manifold Muffler 8 Resonator Muffler Page 21 ### Page 335 11/15/01 AC36-1H Appendix 7 **EQUATIONS FOR THE CALCULATION OF NOISE CERTIFICATION** LIMITS FOR PROPELLER DRIVEN SMALL AIRPLANES AND COMMUTER CATEGORY AIRPLANES 14 CFR PART 36, APPENDIX F NOISE LIMIT (dBA) Up To And Including 1,320 lb. 68 dB(A) ( W -1320)Over 1,320 lb. Up To And Including 3,300 lb. 68 +Ł dB(A)165 ł Over 3,300 lb. 80 dB(A) W = Takeoff Gross Weight In Pounds Page 22 ### Page 336 / / / / I / 11/15/01 AC36-1H Appendix 7 NOISE CERTIFICATION REQUIREMENTS - FAR PART 36, APPENDIX F PROPELLER DRIVEN SMALL AIRPLANES AND COMMUTER CATEGORY AIRPLANES 88 86 84 82 80 80 78 76 74 72 70 68 66 64 62 60 0 2000 4000 6000 8000 10000 12000 14000 16000 18000 20000 Weight (lbs) Noise Level (dBA) Page 23 ### Page 337 APPENDIX 8, CHANGE 1 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CFR PART 36, APPENDIX G) MANUFACTURER MTOW ENGINE DATA PROPELLER DATA NOISE LEVEL (dBA) MODEL MLW (1000#) MFR, MODEL NO. SHP EXH MFR, MODEL DIAM (IN) BLADES PITCH RPM NOTES ADAM AIRCRAFT INDUSTRIES 7.00 CONTINENTAL 2 HARTZELL 3 2700 87.8 A500 6.75 TSIO-550-E PHC-H3YF-2UF/FC7693 V AGUSTA SpA 2.60 LYCOMING 1 260 HARTZELL 76 2 2700 79.3 F260 E 2.60 AEIO-540-D/E4A5 HC-C2YK-4F/FC8477-8 V AQUILA TECHNISCHE ENTWIC 1.65 ROTAX 1 MT-PROPELLER 2 2260 65.2 AT01 1.65 912 S3 MTV-21-A/175-05 V AVIAT 2.00 LYCOMING 1 SENSENICH 2 2700 75.2 A-1B (WITH ENG. OPT.) 2.00 0-320-D2A 74DM6S8-0-58 F AVIAT AIRCRAFT INC. 2.25 LYCOMING 1 HARTZELL 76 2 2700 80.2 9 A-1C-180 2.25 O-360-A1P HC-C2YK-1BF/F7666A F AVIAT AIRCRAFT INC. 2.25 LYCOMING 1 MT-PROPELLER 80.7 2 2600 80.2 9 A-1C-180 2.25 O-360-A1P (175 HP DE MTV-15-B/205-58 F AVIAT AIRCRAFT INC. 2.25 LYCOMING 1 HARTZELL 80 2 2600 80.2 9 A-1C-180 2.25 O-360-A1P (175 HP DE HC-C2YR-1BF/F8477-4 F AVIAT AIRCRAFT INC. 2.25 LYCOMING 1 HARTZELL 80 2 2700 80.1 9 A-1C-200 2.25 IO-360-A1D6 HC-C2YR-1BF/F8477-4 F AVIAT AIRCRAFT INC. 2.25 LYCOMING 1 MT-PROPELLER 80.7 2 2650 82.8 9 A-1C-200 2.25 IO-360-A1D6 (196 HP D MTV-15-B/205-58 F CESSNA 2.30 THIELERT 1 MT-PROPELLER 3 2300 77.0 172K,L,&M (THIELERT STC ST0 2.30 TAE 125-01 MTV-6-A/187-129 V CESSNA 2.45 THIELERT 1 MT-PROPELLER 3 2300 70.9 172K,L,,M&P (THIELERT STC ST 2.45 TAE 125-01 MTV-6-A/187-129 V CESSNA 2.30 THIELERT 1 MT-PROPELLER 3 2300 75.7 172N&P (THIELERT STC ST0130 2.30 TAE 125-01 MTV-6-A/187-129 V CESSNA 2.45 LYCOMING 1 152.6 8 MCCAULEY 75 2 2210 73.3 172R 2.45 IO360-L2A 1C235LFA/7570 F Page 1 ### Page 338 APPENDIX 8, CHANGE 1 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CFR PART 36, APPENDIX G) MANUFACTURER MTOW ENGINE DATA PROPELLER DATA NOISE LEVEL (dBA) MODEL MLW (1000#) MFR, MODEL NO. SHP EXH MFR, MODEL DIAM (IN) BLADES PITCH RPM NOTES CESSNA 2.30 THIELERT 1 MT-PROPELLER 3 2300 77.4 172R&S (THIELERT STC ST0130 2.30 TAE 125-01 MTV-6-A/187-129 V CESSNA 2.45 THIELERT 1 MT-PROPELLER 3 2300 71.3 172R&S (THIELERT STC ST0130 2.45 TAE 125-01 MTV-6-A/187-129 V CESSNA 2.95 CONTINENTAL TCM 1 HARTZELL 80 3 2700 77.8 182Q (BONAIRE STC# SA01218A 2.95 IO-550D PHC-G3YF-1RF/F8468 V CESSNA 3.10 LYCOMING 1 221.3 8 MCCAULEY 82 2 2400 79.7 182S 3.10 IO-540-AB1A5 B2D34C235/90DKB-8 V CESSNA 3.10 LYCOMING 1 229.3 8 MCCAULEY 79 3 2400 77.7 182S 3.10 IO-540-AB1A5 B3D36C431/80VSA-1 V CESSNA 3.60 LYCOMING 1 300 8 MCCAULEY 79 3 2700 84.5 206H 3.60 IO-540-X144 XB3D36C432-X/G80VS V CESSNA 3.60 LYCOMING 1 MCCAULEY 79 3 2500 79.6 206H 3.60 IO-580-AIA B3D36C432/80VSA-1 V CESSNA 3.60 LYCOMING 1 300 8 CESSNA 79 3 2500 79.8 206H 3.60 IO-580-X130 P4327345-01 V CESSNA 8.00 PRATT & WHITNEY 1 675 2 MCCAULEY 106 3 1900 79.0 208 8.00 PT6A-114A 3GFR34C703-106GA V CESSNA 8.00 PRATT & WHITNEY 1 600 MCCAULEY 106 3 1900 81.6 208/208A 8.00 PT6A-114 3GFR34C703-X/X-106G V CESSNA 8.75 PRATT & WHITNEY 1 600 MCCAULEY 106 3 1900 84.2 208B 8.75 PT6A-114 3GFR34C703-X/X-106G V CESSNA 8.75 PRATT & WHITNEY 1 675 HARTZELL 100 3 1900 80.1 208B 8.75 PT6A-114A HCBCMN3/M10083 V CESSNA 8.75 PRATT & WHITNEY 1 675 MCCAULEY 106 3 1900 82.7 208B 8.75 PT6A-114A 3GFR34C703-X/X-106G V Page 2 ### Page 339 APPENDIX 8, CHANGE 1 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CFR PART 36, APPENDIX G) MANUFACTURER MTOW ENGINE DATA PROPELLER DATA NOISE LEVEL (dBA) MODEL MLW (1000#) MFR, MODEL NO. SHP EXH MFR, MODEL DIAM (IN) BLADES PITCH RPM NOTES CESSNA 3.60 LYCOMING 1 MCCAULEY 79 3 2500 75.8 T206H 3.60 TIO-540-AJIA B3D36C432/80VSA-1 V CESSNA 3.60 LYCOMING 1 305.9 4 CESSNA 79 3 2500 75.8 T206H 3.60 TIO-540-X143 XB3D36432-X/80VSA-1 V CESSNA 3.80 CONTINENTAL TCM 1 MCCAULEY 80 3 2700 82.0 TU206G(WIPAIRE) TSIO-520M D3A34C402/90DFA-10 V CESSNA 3.80 CONTINENTAL TCM 1 MCCAULEY 80 3 2700 84.3 U206F(WIPAIRE) 3.80 IO-550-F D3A34C402/90DFA-10 V CESSNA 3.80 CONTINENTAL TCM 1 MCCAULEY 80 3 2700 84.3 U206G(WIPAIRE) 3.80 IO-550-F D3A34C402/90DFA-10 V CIRRUS DESIGN CORP. 2.90 CONTINENTAL 1 HARTZELL 76 2 2700 82.5 SR 20 2.90 IO-360-ES BHC-J2YF-1BF/F7694 V CIRRUS DESIGN CORP. 2.90 CONTINENTAL 1 HARTZELL 74 3 2700 82.5 SR 20 2.90 IO-360-ES PHC-J3YF-1MF/F7392-1 V CIRRUS DESIGN CORP. 3.40 CONTINENTAL 1 HARTZELL 78 3 2700 83.7 SR 22 3.40 IO-550-N PHC-J3YF-1RFX/F7694 V CLASSIC AIRCRAFT 2.95 JACOBS 1 SENSENICH 92 2 2200 79.4 F5C 2.95 R755B2 W96JB-4-68 F CUB CRAFTERS INCORPORATE 2.30 LYCOMING 1 MCCAULEY 2 2700 82.8 CC18 2.30 O-360-C4P 1A200FA8242 F CUB CRAFTERS INCORPORATE 2.30 LYCOMING 1 SENSENICH 2 2700 77.1 CC18 2.30 O-360-C4P M76EM8-0-56 F DATWYLER (MDC) 2.03 LYCOMING 1 MCCAULEY 74 2 2700 67.9 MD3-160(MUFFLED EXHAUST) 2.03 0-320-D2A 1C172/AGM7462 F DATWYLER (MDC) 2.03 LYCOMING 1 MCCAULEY 74 2 2700 71.7 MD3-160(STNDRD EXHAUST) 2.03 0-320-D2A 1C172/AGM7462 F Page 3 ### Page 340 APPENDIX 8, CHANGE 1 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CFR PART 36, APPENDIX G) MANUFACTURER MTOW ENGINE DATA PROPELLER DATA NOISE LEVEL (dBA) MODEL MLW (1000#) MFR, MODEL NO. SHP EXH MFR, MODEL DIAM (IN) BLADES PITCH RPM NOTES DORNIER 10.14 PRATT & WHITNEY 2 MCCAULEY 94.5 4 1900 78.5 SEASTAR CD 2 9.92 PT6A-135A 4HFR34C760/4HFR34C7 V ESTUMKEDA, LTD d.b.a MICCO 2.85 LYCOMING 1 HARTZELL 78 3 2700 82.8 MAC-145B 2.74 IO-540-T4B5 HC-C3YR-1RF/F7693F V EXTRA FLUGZEUGBAU 4.41 CONTINENTAL 1 MT-PROPELLER 76.77 4 2500 79.0 EA 400 4.41 TSIOL-550-A MTV-14-D/195-30A V FAIRCHILD 16.50 ALLIEDSIGNAL 2 1000 MCCAULEY 106 4 1591 80.4 SA227-CC 15.67 TPE 331-11U-612G 4HFR34C652(X)/(X)L10 V FAIRCHILD 16.50 GARRETT 2 1000 MCCAULEY 106 4 1591 80.9 SA227-DC 15.67 TPE331-12UHR-701G 4HFR34C652(X)/(X)L10 V FAIRCHILD 16.50 ALLIEDSIGNAL 2 1000 MCCAULEY 106 4 1591 80.9 SA227-DC 15.70 TPE331-12UA/AR701G 4HFR34C652X/X-L106L V FFA 2.40 LYCOMING 1 HARTZELL 74 2 2700 77.1 AS202/18A4 2.30 AEIO-360-B1F HC-C2YK-1BF V FOUND AIRCRAFT CANADA 3.20 LYCOMING 1 HARTZELL 84 3 2700 85.2 FBA-2C1 3.20 IO-540-D4A5 HC-C3YR-1RF/F8468A- V GENERAL AVIA 1.68 LYCOMING 1 101 2450 76.9 F22 1.68 0-235-N2C MT 180R 120-2C F GIPPSLAND AERONAUTICS PT 4.00 LYCOMING 1 HARTZELL 84 2 2700 87.1 9 GA8 4.00 IO-540-K1A5 HC-C2YR-1BF/F8475R V GYROFLUG-INGENIEUR 1.58 LYCOMING 1 153 MT-PROPELLER 60.25 3 2500 72.0 SC 01 B-160 1.58 O-320 D1A MTV-6-C/LD 152-07 V KINGS ENGINEERING 5.80 LYCOMING 2 HARTZELL 76 3 2700 84.2 44 5.80 IO-540-M1A5 HC-E3YR-2ALTF/FLC-7 V LIBERTY AEROSPACE 1.65 CONTINENTAL 1 SENSENICH 2 2800 74.6 XL-2 1.65 IOF-240 W69E7-63 F Page 4 ### Page 341 APPENDIX 8, CHANGE 1 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CFR PART 36, APPENDIX G) MODEL MANUFACTURER MTOW MLW (1000#) MFR, MODEL **ENGINE DATA NO. SHP EXH MFR, MODEL** PROPELLER DATA DIAM (IN) BLADES PITCH RPM NOISE LEVEL (dBA) NOTES **LUSCOMBE IIE** 2.28 2.28 **CONTINENTAL (TCM) IO-360-ES 1 MCCUALEY EX1B235BFA7660 76 2 F 2550 80.5 MICCO AIRCRAFT CO.** **MAC-145A** 2.60 2.49 LYCOMING IO-360-C1E6 1 200 MCCUALEY B3D36C424-E/74SA-0 74 2 V 2700 81.5 MOONEY M20F (MODWORK STC SA02204 2.74 2.74 **CONTINENTAL IO-360-ES 1 HARTZELL BHC-J2YF-1BF/F7694-1 75 2 V 2800 84.2 MOONEY M20M** 3.40 3.40 LYCOMING TIO-540-AF1A 1 270 MCCAULEY B3D32C417/G82NRd07 75 2 V 2575 74.0 **OSTMECKLENBURGISCHE FLU OMF-100-160** 1.96 1.96 **LYCOMING O-320-D2A 1 MT-PROPELLER MT 186 R 140-30 73 2 F 2700 70.7** **PACIFIC AEROSPACE CORPOR 750XL** 7.50 7.13 **PRATT&WHITNEY PT6A-34 1 HARTZELL HC-B3TN-3D/T10282NS 3 V 2006 86.9** **PARTENAVIA P68 OBSERVER 2** 4.60 4.40 **LYCOMING IO360 A1B6 2 HARTZELL HC-C2YK-2F/F07666A- 72 2 V 2700 78.2** **PIAGGIO P180** 10.80 10.80 **PRATT & WHITNEY PT6A-66 2 HARTZELL M8218X9/LM8218X9** 84.96 5 V 2000 81.9 **PIAGGIO P180** 11.60 11.60 **PRATT & WHITNEY PT6A-66 2 HARTZELL HC-E5N-3/HE8218 85 5 V 2000 81.8** **PILATUS BRITTEN BN-2T-4R** 8.50 8.50 ALLISON 250-B17F/1 2 HARTZELL HC-C3YF-5F/FC7818K 80 3 V 2030 76.0 PILATUS FLUG. AG PC-6/B2-H4 6.20 6.20 **PRATT & WHITNEY PT6A-27 1 HARTZELL HC-B3TN-3** **102.6 3 V 2000 79.4 PIPER PA-28-161 III** 2.44 2.44 **LYCOMING 0-320-D3G 1 SENSENICH 74DM6-0-60 74 2 F 2700 76.0 PIPER PA-28-181 III** 2.55 2.55 LYCOMING O-360-A4M 1 SENSENICH 76EM8S14-0-62 76 2 V 2700 73.1 Page 5 ### Page 342 APPENDIX 8, CHANGE 1 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CFR PART 36, APPENDIX G) MODEL MANUFACTURER MTOW MLW (1000#) MFR, MODEL **ENGINE DATA NO. SHP EXH MFR, MODEL** PROPELLER DATA DIAM (IN) BLADES PITCH RPM NOISE LEVEL (dBA) NOTES PIPER PA-32R-301 HP 3.60 3.60 **LYCOMING IO-540-K1G5 1 300 HARTZELL HC-I3YR-1RF 78 3 V 2700 81.7 PIPER PA-46-500TP** 4.85 4.85 **PRATT & WHITNEY PT6A-42A 500 HARTZELL HC-E4N-3Q/E8501B-3.5 4 2205 73.7** **POLSKIE ZAKLADY LOTNICZE PZL M28 05 (WITH UNDER FUS** 16.53 16.53 **PRATT&WHITNEY PT6A-65B 2 HARTZELL HC-B5MP-3D 5 V 1700 81.9** **PZL WARZAW PZL KOLIBER 150A** 1.90 1.90 **LYCOMING 0-320-EZA 1 SENSENICH 74DM6-0-54** 74.25 2 F 2700 73.8 **PZL WARZAW PZL KOLIBER 150A** 1.90 1.90 **LYCOMING 0-320-EZA 1 SENSENICH 74DM6-0-58** 74.25 2 F 2700 72.3 **QUEST AIRCRAFT COMPANY, KODIAK 100** 7.26 6.69 **PRATT&WHITNEY PT6A-34 1 HARTZELL HC-E4N-3P(Y)/D9511FS 96 4 V 2200 82.5 9** **QUEST AIRCRAFT COMPANY, KODIAK 100 (WITH POD)** 7.26 6.69 **PRATT&WHITNEY PT6A-34 1 HARTZELL HC-E4N-3P(Y)/D9511FS 96 4 V 2200 83.3 9 RANS INC.** S-7C 1.20 **1.20 ROTAX 912S 1 SENSENICH W72RR 72 2 F 2400 70.2** **RAYTHEON 3000** 6.50 6.50 **PRATT & WHITNEY PT6A-68 1 HARTZELL HC-E4A-2/E9612 97 4 V 2000 76.7** **RAYTHEON B300** 15.00 15.00 PRATT & WHITNEY PT6A-60A 2 HARTZELL HC-B4MP-3C 105 4 V 1700 72.9 Page 6 ### Page 343 04/24/2012 AC36-1H Appendix 8, Change 1 Appendix 8 Notes 9 Ground Level Microphone Exhaust Configurations (Reciprocating Engines) 1 Stub Pipes 2 Small Collector, Short Exhaust Pipe 3 Baffles In Collector and/or Cones In Exhaust Pipe 4 Turbine Or Turbocharger 5 Heat Muff 6 Collector Wraparound Manifold Straight Pipe 7 Manifold Muffler 8 Resonator Muffler Page 7 ### Page 344 **APPENDIX 9 MODEL** MANUFACTURER A. SCHLEICHER ASK 16 MTOW MLW 1000# 1.65 **MFR, MODEL** **ENGINE DATA SHPNO.** AIRCRAFT NOISE DATA FOR FOREIGN CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (ICAO ANNEX 16, CHAPTER 6) **RPM MFG, MODEL** **PROPELLER BLADESDIAM (IN) PITCHEXH LIMBACH 1 74 HOFFMANN HO-V62R/LT160T 63 2 VL2000-EB-1** MDBA PC CDBA NOISE LEVEL (dBA) **60.0 -1.3 58.7 NOTES** **AIRCONCEPT VOWI-10** **0.73 LIMBACH SL-1700-EA 1 59 HOFFMANN HO-11-150B65L 59 2 F** 64.1 -1.3 62.8 **AKA-FLIEG STUTTGART FS-28** **1.98 LYCOMING IO-360-B17 1 181 HOFFMANN HO-V-132K-X/LD210 78 2 V** 72.1 -1.4 70.6 **ALPLA-WERKE AVO-68S** **1.50 LIMBACH SL-1700-EI 1 59 HOFFMANN HO-11-150B75L 59 2 F** 62.8 1.8 64.6 **ALPLA-WERKE AVO-68S** **1.51 LIMBACH SL-1700-EI 1 59 HOFFMANN HO-11-150B-75L 59 2 F** **64.1 1.8 65.9 BEECH B76** **3.98 LYCOMING O-360-A1G6D 2 165 2700 1 HARTZELL HC-M2YR-2CLUF/FC76 76 2 V** 79.5 -2.3 77.2 **BEECH (EXCALIBUR) 65-B80** 8.80 8.80 **LYCOMING IO-720-A1B 2 2400 HARTZELL HC-A3VK-2/V8433N-2R 3 V** 77.0 -0.7 76.3 **BUCKER (UMBAU) BU 131** **1.48 LYCOMING AIO-320-C1B 1 153 HOFFMANN HO-23 A-188 125 74 2 F** **69.6 -6.2 64.6 CASA** 1.131E S2000 **1.59 LYCOMING AEIO-360-B2F 1 170 HOFFMANN HO-27 HM-198B 78 2 F** **71.4 -5.0 66.4 CASA** 1.131E S2000 **1.59 ENHASA** **TIGRE G-IV-B 1 118 ENHASA HC 212.111 83 2 F** 67.0 67.0 **CASA SPANIER** 1.131-E **1.59 TIGER ENHASA G-IV-A2 1 99 ENHASA HC-212-111 83 2 F** 71.4 -1.8 69.6 **DEHAVILLAND DH6-300** 12.57 12.35 PRATT+WHITNEY PT6A-27 2 620 2112 HARTZELL HC-B3TN-3D 102 3 V 82.3 -4.9 77.4 **DORNIER 228-101** **13.15 GARRETT TPE331-5-252D 2 HARTZELL HC-B4TN-5ML/LT10574 107 4 75.3** **DORNIER 228-201** 13.15 GARRETT TPE331-5-252D 2 HARTZELL HC-B4TN-5ML/LT10574 107 4 75.3 Page 1 ### Page 345 **APPENDIX 9 MODEL** **MANUFACTURER** DORNIER DO-28-D MTOW MLW 1000# 9.59 **MFR, MODEL** **ENGINE DATA SHPNO.** AIRCRAFT NOISE DATA FOR FOREIGN CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (ICAO ANNEX 16, CHAPTER 6) **RPM MFG, MODEL** PROPELLER BLADESDIAM (IN) PITCHEXH PRATT+WHITNEY 2 399 HARTZELL HC-B-3TN-3D 100 3 VPT-6A-110 MDBA PC CDBA NOISE LEVEL (dBA) **70.8 -5.0 65.8 NOTES FOKKER P-149D** **2.61 AVCO LYCOMING GO-480-B1A6 1 260 HARTZELL HC-A3V20-1D/V8433SP 85 3 V** **68.8 -0.1 68.7 FUJI HEAVY IND.** FA-200-180 **2.54 LYCOMING IO-360-B1B 1 180 MCCAULY B2D34-C53/74E-O 74 2 V** 73.1 0.5 73.6 **GREAT LAKES AIRCRAFT 2T-1A-2** **1.80 LYCOMING AEIO-360-B1G6 1 177 HARTZELL HC-C2YK-4BF 74 2 V** 74.4 -5.0 69.4 **GULFSTREAM AMERICAN AA-1A** **1.52 LYCOMING O-235-C2C 1 108 2500 MC CAULEY SCM1A105/7154 71 2 F** 68.3 0.3 68.6 **GULFSTREAM AMERICAN AA-5A** **2.20 LYCOMING O-320-E2G 1 150 2680 MC CAULEY IC172/BTM7359 73 2 F** 73.3 -0.6 72.7 **LEICHTFLUG-TECHNIK LFU-205** **2.65 LYCOMING IO-360-A1C 1 197 HARTZELL HC-C2YK-1B/F7666A-2 74 2 V** 72.9 0.1 73.0 **LET KONVICE BLANIK-L-13M** **1.28 VK VW 1500-FR 1 50 HOFFMANN HO-11-130B-100D 51 2 F** **59.5 59.5 MBB BO-208** **1.39 CONTINENTAL 0-200-A 1 69 MCCAULY 1A-100MCM-6950 69 2 F** **66.9 66.9 MBB BO-208** **1.39 CONTINENTAL 0-200-A 1 99 MCCAULY 1A-100MCM-6955 69 2 F** **67.3 67.3 MBB BO-208** **1.39 CONTINENTAL O-200-A 1 99 MCCAULY 1A-100MCM-6758 67 2 F** **67.5 -1.0 66.5 MBB BO-209** 1.81 LYCOMING 0-320-E1F 1 147 HARTZELL HC-C2YL-1B/7663A-6 ` 76 2 V **70.7 -1.6 69.1 MBB BO-209** **1.81 LYCOMING IO-320-D1A 1 157 HARTZELL HC-C2YL-1B/7663-SP 76 2 V** **70.8 -3.2 67.6 MBB BO-209-FF** **1.81 LYCOMING O-320-E2F 1 147 MCCAULY 1C-172MGM70-5-66 70 2 F** 70.6 -0.9 69.7 Page 2 The text continues at https://openairdocs.org/ac/36-1.md?from=346 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). 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