08/27/97 AC36-1G Appendix 1 Appendix I. Notes Engines Equipped With P-36 Acoustical Treatment (McDonnell Douglas Aircraft).
Quiet Nacelle And Fan Case Double Acoustic Treatment (Boeing Aircraft).
Fan Case Double Acoustic Treatment (Boeing Aircraft).
Direct Lift Control Used On Approach.
Engine Acoustic Treatment Installed Per Appropriate STC.
DC-9-80 Normal Takeoff Power.
Equipped With Standard Hushkit.
Equipped With Learavia Engine Suppresser Nozzle (Gates Learjet).
Equipped With Learavia With ECR 936 (Gates Learjet).
Revised Forward Center Of Gravity On Approach.
16 Data Also Applies To JT8D-7A And JT8D-7B Engines.
17 Data Also Applies To JT8D-9A 18 Data Also Applies To JT8D-15A.
19 Data Also Applies To JT8D-17A.
20 Data Also Applies To JT8D-17AR.
21 Data Also Applies To JT3D-3B Derated To JT3D-1 Thrust.
22 Increased Takeoff Thrust Rating.
23 Equipped With JT8D-217C Outboard Engines.
24 Equipped With Fan Duct Acoustic Treatment (McDonnell Douglas).
25 Equipped With Thrust Reversers.
26 Equipped With 4% Leading Edge Extension.
27 Equipped With Heavyweight Hushkit 28 Equipped With Heavyweight Hushkit, Including 3% Nozzle Arca Increase 29 Equipped With -100 CN" Nacelle.
30 Equipped With -200 "CN" Nacelle.
31 Equipped With Modifications 2450 (Short Nozzle), 3305, And 3373.
33 Data Also Applies TPE731-3R-IH.
34 Equipped With Modification M3530.
35 Equipped With Lightweight Hushkit.
36 Date also applies to JT8D-9A/-15/-15A/-17/-17A Engines Derated To JT8D-9 Thrust.
37 Data also applies to JT8D-15A/-17/-17A Engines Derated To JT8D-15 Thrust.
38 Configuration APU With APS2000 , GTCP36-280(B), Or GTCP85-129 With Boeing Service Bulletin 737-49-1109 (Without APU Surge Bleed).
AC36-1G 08/27/97 Appendix 1 Appendix 1 Notes - continued 40 Date Also Applies To JT8D-7A/-9/-9A/-15/-15A/-17/-17A Engines Derated To JT8D-7 Thrust.
41 Data Also Applies To JT8D-15/-17 Engines Derated To JT8D-9 Thrust.
42 Data Also Applies To JT8D-17 Engine Derated to JT8D-15 Thrust.
Full Power Takeoff.
** 650 Meter Sideline.
1.10.
......
08/27/97 AC36-1G Appendix 1
EQUATIONS FOR THE CALCULATION OF NOISE CERTIFICATION LIMITS
AT TAKEOFF, SIDELINE, AND APPROACH STAGE 2 Takeoff Limits Sideline Limits Approach Limits (EPNdB) (EPNdB) (EPNdB) Up To And Including 75,000 lb. 93 102 102 W Over 75,000 Ib. To 600,000 Ib. 93 + 53 108 75,000 102 + 21 108 75,000 102 + 2 108 75,000 log 2 log 2 log 2 Over 600,000 lb. 108 108 108 Page 43
AC36-1G 08/27/97 Appendix 1
EQUATIONS FOR THE CALCULATION OF NOISE CERTIFICATION
LIMITS AT TAKEOFF STAGE 3-TAKEOFF (EPNdB) 4 ENGINES OR MORE Up To And Including 44,673 lb. 89 W Over 44,673 lb. To 850,000 lb. 89+43 10g- 44,673 log 2 Over 850,000 Ib. 106 3 ENGINES Up To And Including 63,177 lb. 89 W Over 63,177 To 850,000 lb. 89 + 42 108 63,177 log 2 Over 850,000 lb. 104 2 ENGINES OR LESS Up To And Including 106,250 1b. 89 W log - Over 106,250 To 850,000 Ib. 89 + 41 106,250 log 2 Over 850,000 lb. 101 Page 44
08/27/97 AC36-1G Appendix 1
EQUATION FOR THE CALCULATION OF NOISE CERTIFICATION LIMITS
AT SIDELINE AND APPROACH STAGE 3-SIDELINE (EPNdB) Up To And Including 77,200 lb. 94 W Over 77,200 Ib. To 882,000 lb. 94 + 2.563. 108.77,200 log 2 Over 882,000 lb. 103 STAGE 3-APPROACH (EPNdB) Up To And Including 77,200 Ib. 98 Over 77,200 To 617,300 1b. 98 + 2.331 10877,200 Iog 2 Over 617,300 lb. 105 Page 45
AC36-1G 08/27/97 Appendix 1
NOISE CERTIFICATION REQUIREMENTS - JET AND TRANSPORT AIRPLANES TAKEOFF - 2 ENGINE 110 Cutback Thrust:
One Engine Out Level Flight 108 Or 4 Percent Climb Gradient Whichever Is Greater 105 104 101 100 EPNL Stage 2 Cutback Alt = 1,000 ft (305 m) 93 92 67-60 Stage 2 Derivatives With BPR ≥ 2 Cutback Alt = 984 ft (300 m) 90 89 Stage 3 Cutback Alt = 984 ft (300 m) 85 10 100 1000 Takeoff Weight (1,000 Ibs) Page 46
08/27/97 AC36-1G Appendix 1
NOISE CERTIFICATION REQUIREMENTS - JET AND TRANSPORT AIRPLANES TAKEOFF - 3 ENGINE 110 108 107 Cutback Thrust: One Engine Out 105 Level Flight Or 4 Percent Climb Gradient Whichever Is Greater 104 100 EPNL 95 Stage 2 Cutback Alt. = 1000 Ft. (305M) 93 92 Stage 2 Derivatives With BPR ≥ 2 Cutback Alt. = 853 Ft. (260m) 89 Stage 3 Cutback Alt. =853 Ft. (260m) 85 10 100 1000 Takeoff Weight (1,000 Ibs) Page 47_
AC36-1G 08/27/97 Appendix 1
NOISE CERTIFICATION REQUIREMENTS - JET AND TRANSPORT AIRPLANES TAKEOFF - 4 ENGINE TIO 108 Cutback Thrust:
One Engine Out Level Flight -Or 4 Percent Climb Gradient 106 105 Whichever Is Greater 100 EPNL 95 Stage 2 Cutback Alt = 700 ft (214 m) 93 92 Stage 2 Derivatives With BPR ≥ 2 Cutback Alt. = 689 Ft. (210m) 90 89 Stage 3 Cutback Alt = 689 ft (210 m) 85 10 Takeoff Weight (1,000 1bs) 100 1000 Page 48
08/27/97 AC36-1G Appendix 1
NOISE CERTIFICATION REQUIREMENTS - JET AND TRANSPORT AIRPLANES
SIDELINE 110 108 106 105 103 102 Stage 2 100 97 Stage 2 Derivatives With BPR ≥2 95 94
- Stage 3 90 85 10 100 1000 Takeoff Weight (1,000 Ibs) Page 49|
AC36-1G 08/27/97 Appendix 1
NOISE CERTIFICATION REQUIREMENTS - JET AND TRANSPORT AIRPLANES
APPROACH 110 108 105 105 Stage 2 102 101 Stage 2 Derivatives With BER ≥ 2 100 98 _ Stage 3 EPNL 95 90 10 100 1000 Takeoff Weight (1,000 Ibs) Page 50
APPENDIX 2
AIRCRAFT NOISE DATA FOR
FOREIGN CERTIFICATED TURBOJET POWERED AIRPLANES
MTOW MLW THRUST NOISE LEVEL (FPNIE) MODEL 10000 10004 ENGHE MODEL NO. 1000€ BER IQ SL AP CHAPTER NOTES AEROSPATIALE CARAVELLE 10-BIR 119.00 109.00 14.0 1.10 5 35 93.7 98.1 105 1 2 AEROSPATIALE CARAVELLE 10-BIR 114.50 109.00 JT&D-7 2 14.0 1.10 35 92.3 98.2 105 1 2 AEROSPATIALE CARAVELLE 10-B3 119.00 109.00 2 14.0 1.10 45 94.4 97.7 105 2 AEROSPATIALE CARAVELLE 10-B3 125.60 109.00 JT8D-9 2 14.2 1.10 45 95.7 98.2 106.2 2 AEROSPATIALE CARAVELLE 11R 114.50 109.00 JT&D-7 14.0 1.10 35 92.3 97.9 105 1 AFROSPATIALE CARAVELLE 12 119.00 109.00 2 14.2 1.10 45 94.0 98.4 105.9 AEROSPATIALE CARAVELLE 12 123.40 109.00 JT8D-9 2 14.2 1.10 45 95.3 98.3 105.9 2 AEROSPATIALE CARAVELLE 12 127.00 109.00 2 14.2 1.10 5 45 96.6 98.2 105.9 2 AIRBUS A300B1 302.03 268.96 CF6-SOC2R 2 50.4 4.30 • 25 90.8 97.4 102.9 AIRBUS A300B1 302.10 269.00 CF6-SOA 2 48.4 4.60 25 $7.9 90.7 101.1 2 AIRBUS A300B2 KIC 313.10 286.70 CF6-50C 2 50.4 4.30 25 $7.0 92.6 101.7 2 AIRBUS A300B2-1A 302.10 2$1.10 CF6-50A 43.3 4:60 25 37 0 90.7 101.1 AIRBUS A300B2-1C 291.01 268.96 CF6-50C 2 50.4 4.30 25 $9.9 97.5 102.9 3 AIRBUS A300B2-1C 313.05 286.70 CF5.50C 2 50.4 4.30 25 91.8 97.4 103.1 3 AIRBUS A300B2-202 313.00 287.00 CF6-50C1 2 51.7 4.60 25 89.3 93.5 102.0 AIRBUS A300B2-320 330.80 293.30 IT9D-59 A 2 50.3 4.90 15 90.3 98.5 100.5 AIRBUS A300B4-102 347.30 294.80 CF6-SOC1 2 51.7 4.60 25 90.1 93.3 101.9 AIRBUS A300B4-120 313.07 286.60 TT9D-59 A 25 90.0 98.0 101.9 3 AIRBUS A300B4-120 363.78 295.43 ST9D-59A 2 75 93.5 97.6 103.2 3 AIRBUS A300B4-120 347.24 295.43 ST9D-59 A 2 25 92.2 97.7 103.2 AIRBUS A300B4-120 363.78 299.84 JT9D-59 A 5Z 93.6 97.5 102.3 AIRBUS A30084-203 302.04 275.59 CF650.C2 SZ 6 62 01 3 · 201
8/27/97 APPENDIX 3 ***STAGE 3***
TURBOJET POWERED AIRPLANES
MTOW MLW THRUST ELAPS NOISE LEVEL (EPNIB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BPR IQ AP IQ SL AP SALON JONES AEROSPATIALE SN601 CORVETTE 13.90 12.40 J15D4 2 2.50 2.50 15 35 80.4 85.4 89.5 3 AEROSPATIALE SN601 CORVETTE 14.60 13.20 J15D-4 2.52 2.50 15 35 74.0 81.0 90.0 AIRBUS A300 B4-60SR 330.40 290.00 CF6-80C2ASF 2 40 87.4 98.8 99.5 3 AIRBUS A300 B4-60SR 385.46 319.38 CF6-80C2ASF 40 91.5 98.5 100.0 AIRBUS A300B2-1C 291.00 268.00 CF6-50C/2R 25 89.9 97.5 102.9 AIRBUS A300B2-1C 313.00 286.60 CF6-50C/2R 2 25 91.8 97.4 103.1 AIRBUS A300B2-203 313.10 286.60 CF6-50-C2 2 51.8 4.31 16 25 91.1 97.9 103.1 AIRBUS A300R4-103 347.20 295.40 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 51.8 4.31 25 90.5 97.3 102.4 31 AIRBUS A300B4-203 363.70 299.83 CF6-50-C2 2 51.8 4.31 25 94.0 96.9 102.4 31 AIRBUS A300B4-622R 330.00 275.00 PW-4158 2 58.0 40 83.0 98.3 101.3 AIRBUS A300B4-622R 385.00 304.50 PW-4158 2 58.0 40 93.1 97.9 101.9 3 AIRBUS A310-221 305.60 267.90 STOD-TRADI 2 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 40 85.7 96.5 98.5 AIRBUS A310-304 352.74 286.60 CF6-80C2A2 2 53.5 40 92.9 96.1 98.8 AIRBUS A310-324 330.69 271.16 PW-4152 2 52.0 15 40 90.6 97.2 100.2 3 AIRBUS A319-112 123.46 121.25 CFM56-SB6 w/SAC 2 23.5 6.00 10 40 78.6 93.3 92.4 AIRBUS A319-112 158.73 149.91 CFM56-5B6 w/SAC 2 23.5 6.00 10 40 85.4 92.6 93.1 AIRBUS A319-113 123.46 121.25 CFM56-5A4 2 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-AS 2 22.0 4.90 10 40 79.2 92.5 94.0 3 Page 1