Advisory U.S. Department of Transportation Circular Federal Aviation Administration Subject: Date: 8/27/97 AC No: 36-1G Initiated by: AEE-110 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 36-1F, Noise Levels for U.S. Certificated and Foreign Aircraft, dated June 5, 1992, is canceled.
3. BACKGROUND. The agency's regulatory program for airplane 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 J36.305 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).
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 FAA Form 1320-15 (4-82) Supersedes WA Form 1320-2
AC36-1G 08/27/97 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 °F, 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 1.
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 takeoff weights, 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 °F, 70% relative humidity conditions where required by 14 CFR part 36, Appendix F.
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 Page 2
08/27/97 AC36-1G Appendix 1 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 "Stage 2" helicopter means a helicopter which 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. The airplane noise level listings of this Advisory Circular will be revised and updated periodically.
оли, James D. Erickson Director, of Environment and Energy Page 3
AC36-IG 08/27/97
LIST OF APPENDICES Appendix 1 Aircraft Noise Data for United States Certificated Turbojet Powered Aircraft Appendix 2 Aircraft Noise Data for Foreign Certificated Turbojet Powered Aircraft Appendix 3 Stage 3 Turbojet Powered Aircraft Appendix 4 Aircraft Noise Certification Levels in Descending EPNdB for U.S. Certificated Turbojet Powered Aircraft - Takeoff Appendix 5 Aircraft Noise Certification Levels in Descending EPNdB for U.S. Certificated Turbojet Powered Aircraft - Approach Appendix 6 Aircraft Noise Data for Propeller Driven Aircraft Certificated in the Transport Category Appendix 7 Aircraft Noise Data for U.S. Certificated Propeller Driven Small Airplanes (14 CFR Part 36, Appendix F) Appendix 8 Aircraft Noise Data for U.S. Certificated Propeller Driven Small Airplanes and Commuter Category Airplanes (14 CER part 36, Appendix G) Appendix 9 Aircraft Noise Data for Foreign Certificated Propeller Driven Small Aircraft Appendix 10 Aircraft Noise Data for U.S. Certificated Helicopters (14 CFR part 36, Appendix H) Appendix 11 Aircraft Noise Data for U.S. Certificated Helicopters (14 CFR part 36, Appendix J) Appendix 12 Abbreviations.
• Page 4 ...
APPENDIX 1
AIRCRAFT NOISE DATA FOR
UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES
MTOW MLW THRUST FLAPS NOISE LEVEL (EPNABI MANUTACTURER MODEL 1000M 1000% ENCINEMODEL 1000# BPR IQ SL AP STAGE NOTES AFROSPATIALE SN601 CORVETTE 13.90 12.40 J15D-4 2.50 2.50 15 35 80.4 85.4 89.5 AEROSPATIALE SN601 CORVETTE 14.60 13.20 SISD4 2 2.52 2.50 35 74.0 81.0 90 0 AIRBUS A300 B4-605R 330.40 290.00 CF6-80C2ASF 61.5 5.00 40 $7.4 98.8 99.5 AIRBUS A300 B4-605R 385.46 319.38 CF6-80C2ASF 2 61.5 5.00 40 91.5 98.5 100.0 3 AIRBUS A300B2-1C 291.00 .268.00 CF6-50C2-R 50 $ 4.40 25 89.9 97.5 102.9 3 AIRBUS A300B2-1C 313.00 286.60 CF6-50C2-R 2 50.4 4.40 25 91.8 97.4 103.1 AIRBUS A300B2-203 313.10 286.60 CF6-50-C2 2 S1.8 4.31 16 25 91.1 97.9 103.1 AIRBUS A300B4-103 347.20 295.40 CF6-50-C2 2 51.8 4.31 16 25 93.6 97.7 103.0 AIRBUS A300B4-203 313.05 286.60 CF6-50C2 2 $1.8 4.31 25 90.5 97.3 102.4 3 31 AIRBUS A300B4-203 363.70 299.83 CF6-50-C2 51.8 4.31 25 94.0 96.9 102.4 3 31 AIRBUS A300B4-622R 330.00 275.00 PW-4158 2 58.0 4.85 40 88.0 98.3 101.3 3 AIRBUS A300B4-622R 385.00 304.50 PW-4158 2 58.0 4.85 40 93.1 97.9 101.9 AIRBUS A310-221 305.60 267.90 JT9D-7R4D1 48.0 4.50 15 40 90.5 94.8 100.6 3 AIRBUS A310-304 275.58 261.25 CF6-80C2A2 2 53.5 5.00 40 85.7 96.5 98.5 AIRBUS A310-304 352.74 286.60 CF6-80C2A2 2 53.5 5.00 40 92.9 56.1 98.8 3 AIRBUS A310-324 330.69 271.16 PW-4152 52.0 4.85 15 40 90.6 97.2 100.2 AIRBUS A319-112 123.46 121.25 CFM56-SB6 w/SAC 23.5 6.00 10 40 78.6 93.3 82.4 3 AIRBUS A319-112 158.73 149.91 CFM56-5B6 w/SAC 2 23.5 6.00 10 40 85.4 92.6 93.1 3 Page 1
APPENDIX 1
AIRCRAFT NOISE DATA FOR
UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST ELAPS NOISE LEVEL (EPNdB) MANVEACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR IQ IQ SL AP STAGE NOTES AIRBUS A319-113 123.46 121.25 CFM56-5A4 22.0 6.00 10 40 80.1 93.9 94.0 AIRBUS A319-113 158.73 149.91 CFM56-5A4 2 22.0 6.00 10 40 87.5 93.1 94.8 AIRBUS A319-131 123.46 121.25 V2522-A5 2 22.0 4.90 10 40 79.2 92.5 94.0 AIRBUS A319-131 158.73 149.91 V2522-AS 2 22.0 4.90 10 40 85.3 91.4 94.5 AIRBUS A320-211 162.00 142.20 CFM56-5A1 2 25.0 6.00 10 35 87.8 94.3 96.4 - 3 AIRBUS A320-211 149.90 142.20 CFMS6-SA1 2 25.0 6.00 10 35 85.3 94.4 96.4 AIRBUS A320-231 149.90 142.20 V2500.A1 2 25.0 6.00 10 40 84.0 93.0 96.6 AIRBUS A320-231 162.00 142.20 V2500.A1 2 25.0 6.00 10 40 86.6 92.8 96.6 3 AIRBUS A330-301 396.83 361.56 CF6-80E1A2 2 65.8 5.05 14 32 $7.0 97.9 98.5 AIRBUS A330-301 507.06 418.88 CF6-80E1A2 65.8 5.05 14 32 94.2 97.2 98.7 3 AIRBUS A330-321 396.83 330.69 PW4164 2 64.0 4.85 32 88.5 98.0 97.3 3 AIRBUS A330-321 507.06 418.88 PW4164 2 64.0 4.85 32 95.6 97.5 98.0 AIRBUS A330-322 396.83 330.69 PW4168 68.0 4.85 32 87.6 98.6 97.3 3 AIRBUS A330-322 507.06 418.88 PW4168 2 68.0 4.85 32 94.3 98.3 98.0 3 AIRBUS A340-212 485.01 363.76 CFM56-5C3 2 32.5 6.60 17 32 88.1 95.8 97.3 3 AIRBUS A340-212 595.25 440.92 CFM56-5C3 2 32.5 6.60 17 32 96.1 95.4 97.2 AIRBUS A340-312 485.02 363.76 CFM56-5C3 32.5 6.60 17 32 88.0 95.8 97.3 3 AIRBUS A340-312 595.24 440.92 CFM56-5C3 2 32.5 6.60 17 32 96.2 95.3 97.2 Page 2
AIRCRAFT NOISE DATA FOR
UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES
MTOW MLW THRUST SITI MANUYASTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR IQ AP TO SL AVRO 146-RJ 85 80.00 77.50 1.F 507-IF 7.00 5.10 18 33 79.0 89.1 96.9 AVRO 146-RJ 85 97.00 85.00 LF 507-IF 7.00 5.10 18 33 84.3 88.4 97.3 BAe 1-11 200 80.00 71.00 SPEY 506-14 2 10.4 1.00 3 45 93 3 99.1 97.8 12 BAe 1-11 400 87.00 77.20 SPEYSI1-14/14W 2 11.4 0.70 45 94 8 103.4 99 7 12 BAc 1-11 400 89.50 79.00 SPEYS11-14/14W 11.4 0.70 45 95.7 103.3 99.9 2 12 BAe 146-100 A 76.00 72.35 ALF502R-3 6.70 5.90 18 33 80.7 87.2 95.1 3 BAe 146-100A 76.00 72.35 ALF502R-3A 6.97 5.70 18 33 79.0 88.0 94.9 BAe 146-100 A 82.25 73.35 ALF502R-3A 6.97 5.70 18 33 82.3 87.6 95.2 BAc 146-100 A 82.25 73.35 ALF502R-5 6.97 5.70 33 82.3 87.6 95.2 3 146-100 A 34.00 77.50 ALF502R-5 6.97 5.70 18 33 81.8 87.7 95.6 3 BAe 146-200 A 89.50 77.50 ALF502R-3 6.70 5.90 18 33 85.9 86.6 95.6 BAc 146-200 A 89.50 77.50 ALF502R-3A 6.97 3.70 18 33 84.9 87.3 95.6 BAe 146-200 A 89.50 77.50 ALF502R-5 6.97 5.70 18 33 84.9 87.3 95.6 3 ВАє 146-200 A 93.00 81.00 AL F5022-5 6.97 5.70 18 33 85.2 87.3 95.B BAc 146-300 95.00 83.00 LF 507-1H/-1F 7.00 5.10 18 33 84.0 87.9 97.2 BAe 146-300 101.50 88.50 LF 507-1H-1F 7.00 5.10 18 33 86.3 87.6 97.6 ВАє 146-300 A 95.00 83.00 ALF S02R-5 6.97 5.70 18 33 86.0 87.0 96.0 BAE 146-300 A 97.50 84.50 ALF502R-5 4 6.97 5.70 18 33 86.5 86.7 95.6 3 Page 3
APPENDIX 1
AIRCRAFT NOISE DATA FOR
UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANVFACTURER MODEL 1000฿ 1000฿ ENGINE MODEL NO. 1000# BPR IQ IQ SL AP STAGE NOTES BAc C-29 A 28.00 23.35 TFE731-5R-IH 2 4.30 3.30 45 81.4 87.3 95.8 BEECH BEECHJET 400 15.78 14.22 ITISD-S 2 2.88 2.10 10 30 88.6 93.7 91 4 BOEING B-707-100B (QNC) 241.30 190.00 JT3D-1 30 103.4 102.8 102.8 6.0* BOEING B-707-100B (QNC) 258 00 190.00 JT3D-3B 30 103.8 1027 102.8 6.00 BOEING B-707-120B (SHANNON) 258.00 190.00 JT3D-1 30 103.5 97.6 105.3 21.°• BOEING B-707-138B (SHANNON) 258.00 190 00 3D-1 30 103 2 97 6 105 3 21.0° BOEING B-707-300B ADVIC QNC 335.00 247.50 JT3D.3B 25 104 4 98.9 107 9 2 6.00 BOEING B-707-300B ADV/C SHN 330.00 201.00 JT3D-7 25 104.7 99.6 108.3 6,00 BOEING B-707-300B ADV/C SHN 321.00 240.00 JT3D-3B 25 104.5 99.2 108.2 6.00 BOEING B-707-300B ADV/C SHN 322.30 247.00 JT3D-1-3B(IC) 14 25 105.5 99.3 105.7 6.21.90 BOEING B-720B (Q.IC) 234.00 175.00 JT3D-1 30 102.3 102.9 101.6 6.00 BOLING B-720B (QNC) 234.00 175.00 JT3D-3B 30 99.3 103.2 101.6 6,0= BOEING B-720B (SHANNON) 234.00 175.00 JT3D-1 30 98.9 98.0 104.7 BOEING B-720B (SHANNON) 234.00 175.00 TT3D-3B 30 97 3 99.5 104 7 6.9= BOEING B-727-100 152.50 135.00 JT8D-7FCD 14.0 1.10 40 94.4 100.3 104.1 3,16 BOEING B-727-100 160.50 137.50 ST&D-IFCD 14.0 1.10 40 96.6 99.2 104.3 BOEING B-727-100 169.50 137.50 IT&D-IFCD 14.0 1.10 40 98.5 99.1 104.3 BOEING B-727-100 169.50 137.50 JT8D-7FCD 14.0 1.10 5 40 97.9 100.0 104.3 3,16 Page 4
APPENDIX 1
AIRCRAFT NOISE DATA FOR
UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES MTOW MLW THRUST ELAPS NOISE LEVEL (EPNdB) MANKACTURER MODEL 1000₴ 1000# ENGINE MODEL NO. 1000# BPR IQ AF TO SL AP STAGE NOTES BOEING B-727-100 160.50 137.50 JT8D-9FCD 14.5 1.03 5 40 96.1 100.2 105.8 2 3,17 BOEING B-727-100 169.30 137.50 JT&D-9FCD 14.5 1.03 40 98.3 100.0 105.8 2 3.17 BOEING B-727-100 (Dee Howard) 169.50 137.50 TAY 651-54 15.4 40 92.1 92.3 98.4 BOEING B-727-100 (Dee Howard) $69.50 142.50 TAY 651-54 15.4 5 30 92.1 92.3 95.3 BOEING B-727-100 (FED EX;STC 160.50 137.50 JT8D-7 w/BOEING 14.0 1.10 30 92.5 95.6 97.8 35 S,A3993NM) INLET+CHIN CSD BORING B-727-100 (FED EX;STC 163.50 137.50 JT8D-7 w/BOEING 14.0 1.10 30 93.2 97.4 97.8 35 SA3993NM) INLET+FAN CSD : BOEING B-727-100 (FED EX;STC 169.50 137.50 JT8D-9 w/BOEING 14.5 1.03 5 30 93.9 97.5 98.1 3 35 SA3993NM) INLET+CHIN CSD BOBING B-727-100 (FED EX;STC 174.50 142.50 JT8D-7 w/BOEING 3 14.0 1.10 30 95.7 96.4 97.9 35 SA3993NM) INLET+CHIN CSD : BOEING B-727-100 (FED EX;STC 169.50 142.50 JT8D-7 w/BURBANK 14.0 1.10 5 30 94.1 96.6 98.2 3 35 SA3993NM) INLET+CHIN CSD BOEING B-727-100 (FED EX;STC 169.50 142.50 JT8D-7 w/BURBANK 3 14.0 1.10 5 30 94.1 97.2 98.2 35 SA3993NM) INLET+FAN CSD BOEING B-727-100 (FED EX;STC 169.50 142.50 JT8D-9 ₩/BOEING 14.5 1.03 30 93.9 98.0 98.4 35 SA3993NM) INLET+FAN CSD : BOEING B-727-100 (FED EX;STC 174.50 142.50 JT8D-9 w/BURBANK 14.5 1.03 30 94.9 97.1 98.8 35 ( 13993NM) INLET+CHIN CSD BOEING B-727-100 (FED EX;STC 169.50 142.50 JT8D-9 w/BURBANK 14.5 1.03 30 94.0 97.3 98.8 35 SA3993NM) INLET+CHIN CSD BOEING B-727-200 184.20 142.50 JT8D-15QN 15.5 1.00 40 98.8 102.2 103.2 2 2,18 BOEING B-727-200 190.50 142.50 JT8D-15QN 15.5 1.00 40 100.0 102.2 103.2 2 2,18 BOEING B-727-200 190.50 142.50 ST8D-17QN 3 16.0 1.00 40 99.6 103.7 103.2 2,19 BOEING B-727-200 190.50 142.50 JT8D-17RQN 17.4 0.97 40 98.9 104.7 103.2 2 2,20 BOSING B-727-200 208.00 142.50 • 78D-17RQN 17.4 0.97 5 40 102.4 104.2 103.2 2 2,20 Page 5
APPENDIX 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 IQ AP TO SL AP STAGE NOTES BOEING B-727-200 172.50 142.50 JT&D-7FCD 3 14.0 1.10 15 40 100.0 100.4 106.3 2 3,16 BOEING B-727-200 177.60 142.50 JT8D-7FCD 14.0 1.to 5 40 99.8 99.8 106.3 2 3,16 BOEING B-727-200 172.50 142.50 JT8D-7QN 14.0 1.10 15 40 100.0 100.4 104.9 2,16 BOEING B-727-200 172.50 142.50 JT8D-9QN 3 14.5 1.03 15 40 99.0 100.4 103.2 2 2,17 BOEING B-727-200 184.80 142.50 IT&D-9QN 14.5 1.03 15 40 101.5 100.2 103.2 2,17 BOEING B-727-200 178.00 150.00 JT8D-9FCD 3 14.5 1.03 5 30 100.7 99.8 105.8 2 3,17 BOEING B-727-200 203.10 158.00 JT8D-17QN 16.0 1.00 40 102.0 103.5 I04.5 2,19 BOEING B-727-200 (FED EX;STC 172.60 150.00 JT8D-7 w/BOEING 3 14.0 1.10 30 96.0 97.4 99.0 35 SA4833NM) INLET+CHIN CSD BOEING B-727-200 (PED EX;STC 172.50 150.00 JT8D-7 w/BOEING 14.0 1.10 30 95.9 97.0 99.0 35 SA4833NM) INLET+FAN CSD BOEING B-727-200 (FED EX;STC 172.60 150.00 JT&D-7 w/BURBANK 14.0 1.10 30 95.7 96.5 98.9 35 SA4833NM) INLET+CHIN CSD BOLING B-727-200 (FED EX;STC 173.88 150.00 JT&D-9 ₩/BOEING 14.5 1.03 30 95.5 97.4 99.6 3 35 SA4833NM) INLET+CHIN CSD BOFING B-727-200 (FED EX;STC 167.85 150.00 IT&D-9 ₩/BOEING 14.5 1.03 30 94.2 98.3 99.6 35 SA4833NM) INLET+FAN CSD BOEING B-727-200 (FED EX;STC 175.00 150.00 JT&D-9 w/BURBANK 14.5 1.03 5 30 95.2 97.2 100.2 3 35 SA4833NM) INLET+CHIN CSD BOEING B-727-200 (FED EX;STC 170.48 150.00 JT8D-9 w/BURBANK 14.5 1.03 5 30 94.3 97.8 100.2 3 35 SA4833NM) INLET+FAN CSD BOEING B-727-200 (FED EX;STC 178.42 154.50 JT8D-7 w/BURBANK 14.0 I.10 30 97.0 96.0 99.1 35 SA4833NM) INLET+CHIN CSD BOEING B-727-200 (FED EX:STC 171.44 154.50 JT8D-9 w/BOEING 3 14.5 1.03 5 30 94.9 97.6 99.9 3 35 SA4833NM) INLET+CHIN CSD BOEING B-727-200 (FED EX;STC 165.60 154.50 JT&D-9 ₩/BOEING 14.5 1.03 30 93.7 98.4 99.9 3 35 SA4833NM) INLET+FAN CSD BOEING B-727-200 (FED EX;STC 172.96 154.50 IT8D-9 w/BURBANK 3 14.5 1.03 30 94.7 97.3 100.5 3 35 SA4833NM) INLET+CHIN CSD Page 6
APPENDIX 1
AIRCRAFT NOISE DATA FOR
UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES
MTOW MLW THRUST FLAPS NOISE LEVEL (EPNE) MANUTACTURER MODEL 1000E 1000฿ ENGINE MODEL 10008 BPR IQ AP IQ SL STAGE NOTES BOEING B-727-200 (FED EX;STC 178.00 161.00 ITID-7 P/BURBANK 14.0 1.10 30 96.9 96.6 99.4 35 SA4833NM) INLET+FAN CSD BOEING B-727-200 (FED EX;STC 135.00 150.00 JT8D-9 ₩/BOEING 3 14.5 1.03 5 30 89.2 97.9 97.4 27 SA5839NM) INLET+CHIN CSD BOEING B-727-200 (FED EX;STC 155.00 150.00 IT8D-9 ₩/BOEING 14.5 1.03 30 $9.2 98.4 97.4 3 27 SAS839NNI) INLET+FAN CSD BOEING B-727-200 (FED EX;STC 155.00 150.00 JT8D-9 w/BURBANK 3 14.5 1.03 5 30 38.5 97.6 98.0 27 SA5839NM) INLET +CHIN CSD BOEING B-727-200 (FED EX;STC 155.00 150.00 JT&D-9 w/BURBANK 14.5 1.03 30 $8.5 98.1 98.0 3 27 SAS839NM) INLET+FAN CSD BOEING B-727-200 (FED EX;STC 160.00 154.50 JT&D-15 w/BOEING 3 15.5 1.00 30 92.2 98.0 97.6 27 SA5839NM) INLET+CHIN CSD BOEING B-727-200 (FED EX;STC 160.00 154.50 SID-15 ₩/BOEING 15.5 1.00 30 92.2 98.2 97.6 27 SA5839NM) INLET+FAN CSD BOEING B-727-200 (FED EX:STC 178.90 154.50 J8D-15 W/BURBANK 3 15.5 1.00 30 94.3 97.3 98.2 27 SA5839NM) INLET+FAN CSD BOEING B-727-200 (FED EX;STC 184.20 154.50 JT8D-17 w/BOEING 16.0 1.00 30 95.3 98.8 97.6 27 SA5839NM) INLET : BOEING B-727-200 (FED EX;STC 184.20 154.50 JID-17 w/BURBANK 3 16.0 1.00 30 94.8 98.6 98.2 3 27 SA5839NM) INLET BOEING B-727-200 (FED EX;STC 189.20 160.00 1T8D-9 w/BOEING 3 14.5 1.03 30 97.3 95.9 97.9 3 27 SA5839NM) INLET+CHIN CSD BOEING B-727-200 (FED EX;STC 189.20 160.00 JTID-9 w/BOEING 14.5 1.03 5 30 97.3 96.5 97.9 27 SA5839NM) INLET+FAN CSD BOEING B-727-200 (FED EX;STC 191.20 160.00 JT8D-9 ₩/BURBANK 3 14.5 1.03 30 97.4 95.7 98.5 27 SA5839NM) INLET+CHIN CSD BOEING B-727-200 (FED EX;STC 191.20 160.00 JT&D-9 w/BURBANK 14.5 1.03 30 97.4 96.3 98.5 27 SA5839NM) INLET+FAN CSD BOEING B-727-200 (FED EX;STC 182.75 161.00 JT&D-15 w/BOEING 15.5 1.00 5 30 93.9 99.1 97.7 3 78 SA5839NM) INLET+CHIN CSD BOEING B-727-200 (FED EX;STC 202.00 164.00 JT&D-17 w/BURBANK 160 1.00 5 30 97.1 98.8 98.6 27 SA5B39NM) INLET BOEING B-727-200 (FED EX;STC 199.51 166.00 JT8D-15 w/BOEING 15.5 1.00 30 97.6 98,0 97 9 28 SA5839NM) INLET+CHIN CSD BOEING B-727-200 (FED EX;STC 199.05 166.00 JT8D-15 w/BOEING 15.5 1.00 30 97.6 98.0 98.1 3 27 SA5839NM) IN ET+CHIN CSD Page 7
APPENDIX 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 AP ÖI SL AP SALON SOVI BOEING B-727-200 (FED EX;STC 199.05 166.00 JT8D-15 /BOEING 15.5 1.00 30 97.6 98.2 98.1 3 27 SA5839NM) INLET+FAN CSD BOEING B-727-200 (FED EX;STC 201.00 166.00 JT8D-15 w/BURBANK 15.5 1.00 5 30 97.7 97.6 98.6 3 27 SA5839NM) INLET+FAN CSD BOEING B-727-200 (FED EX;STC 200.00 166.00 JT8D-17 w/BOEING 16.0 1.00 30 97.1 99.1 98.1 27 SA5839NM) INLET BOEING B-727-200RE(VALSAN) 190.50 148.00 JT8D-15/217C 30 91.5 99.3 98.8 6,23 'BOEING B-727-200RE(VALS AN) 198.50 159.00 JT8D-17/217C 30 92.2 99.5 99.0 6,23 BOEING B-727-200RE(VALSAN) 209.50 159.00 JT8D-17A/217C 30 94.5 99.6 99.0 6,23 HOEING B-727-200RE(VALSAN) 203.10 164.00 JT8D-17A/217C 30 93.4 99.6 99.3 3 6,23 BOEING B-737-200 (AVAERO:STC 128.10 88.00 JT8D-17 2 16.0 1.00 40 91.4 97.5 96.7 27 ST223CH) BOEING B-737-200 (AVAERO;STC 117.00 90.00 JT8D-15 2 15.5 1.00 40 89.7 96.7 98.1 35,42 ST223CH BOEING B-737-200 (AVAERO;STC 128.10 93.00 JT8D-15 2 15.5 1.00 40 92.1 96.5 97.1 27,42 ST223CH) BOEING B-737-200 (AVAERO-STC 100.80 95.00 JT8D-15 2 15.5 1.00 40 83.7 96.8 97.2 27,42 ST223 CH BOEING B-737-200 (AVAERO;STC 100.80 95.00 JT8D-9 2 14.5 1.03 40 85.2 95.5 97.2 3 27.41 ST223CH) BOEING B-737-200 (AVAERO;STC 100.50 98.00 JT8D-15 2 15.5 1.00 40 84.9 96.9 98.6 3 35.42 ST223CH) BOLING B-737-200 (AVAERO-STC 100.50 98.00 J8D-9 2 14.5 1.03 40 86.3 95.7 98.6 35.41 ST223CH) BOEING B-737-200 (AVAERO;STC 121.50 107.00 IT8D-15 2 15.5 1.00 30 91.3 96.9 96.3 35,42 ST223CH) BOEING B-737-200 (AVAERO;STC 128.10 107.00 JT8D-15 2 15.5 1.00 30 92.1 96.5 94.8 21.42 ST223CH) BOEING B-737-200 (AVAERO:STC 115.00 107.00 JT8D-17 2 16.0 1.00 40 87.6 97.5 98.0 3 27 ST223CH) BOEING B-737-200 (AVAERO-STC 128.10 107.00 JT8D-17 16.0 1.00 30 91.4 97.5 94.8 27 ST223CH) Page 8