8/27197 AC 36-1G APPENDIX 1
AIRCRAFT NOISE DATA FOR
UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES
MTOW MLW THRUST FLAPS NOISE LEVEL (EPNIB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL 1000* BPR IQ IQ SL AL STAGE NOTES MCDONNELL DOUGLAS MD-11 A-1 630.50 481.50 CF6-80C2DIF 61.5 5.30 10 50 94.5 96.3 104.5 MCDONNELL DOUGLAS MD-11 A-! 630.50 481.50 PW4460 (-3) 50.0 5.00 10 50 95.6 98.0 104.4 MCDONNELL DOUGLAS MD-11 4-1 630.50 481.50 PW4462 (-3) 3 62.0 5.00 10 50 95.0 96.5 104.4 3 MCDONNELL DOUGLAS MD-80 140.00 128.00 JT$D-209 2 19.2 1.83 40 88.9 94.7 92.8 3 10 MCDONNELL DOUGLAS MD-80 140.00 128.00 ST$D-219 2 21.7 1.70 40 86.7 97.3 92.8 3 10 MCDONNELL DOUGLAS MD-80 149.50 130.00 J8D-209 2 19.2 1.83 40 91.1 94.5 92.9 10 MCDONNELL DOUGLAS MD-80 142.00 130.00 ST$D-217 2 20.8 1.80 40 88.2 96.1 92.9 3 10 MCDONNELL DOUGLAS MID-80 149.50 130.00 JT&D-217 2 20.8 1.80 40 89.7 95.8 92.9 10 MCDONNELL DOUGLAS MID-80 149.50 130.00 IT&D-219 2 21.7 1.70 40 88.6 97.1 92.9 3 10 MCDONNELL DOUGLAS MD-80 160.00 150.00 JT&D-217A 2 20.8 1.80 40 92.0 95.9 93.7 3 10 MCDONNELL DOUGLAS MD-80 160.00 150.00 JT8D-217C 2 20.8 1.70 2 40 91.5 96.3 93.7 10 MCDONNELL DOUGLAS MD-80 160.00 150.00 JT&D-219 2 21.7 1.70 2 40 90.8 97.2 93.7 3 10 MCDONNELL DOUGLAS MD-87 125.00 120.00 JT8D-217A 2 20.8 1.80 40 84.3 96.4 92.9 3 10 MCDONNELL DOUGLAS MD-87 125.00 120.00 JT8D-217C 2 20.8 1.70 40 84.1 96.5 92.9 3 10 MCDONNELL DOUGLAS MD-87 140.00 128.00 JT8D-219 21.7 1.70 40 86.5 97.1 93.3 3 10 MCDONNELL DOUGLAS MD-87 149.50 130.00 JT8D-217A 2 20.8 1.80 40 89.7 95.9 93.3 3 10 MCDONNELL DOUGLAS MID-87 149.50 130.00 JTXD-217C 2 20.8 1.70 40 89.2 96.2 93.3 3 10 MCDONNELL DOUGLAS MD-87 149.50 130.00 JT&D-219 2 21.7 1.70 40 88.5 97.1 93.3 10 Page 38
APPENDIX 1
AIRCRAFT NOISE DATA FOR
UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES
MTOW MLW THRUST ELAPS NOISE LEVEL (EPNJB) MANUFACTURER MODEL 1009% 1000# ENGINE MODEL 1000# SL STAGE NOTES MCDONNELL DOUGLAS MID-90-30 135.00 130.00 V2525-DS 2 25.0 4.80 40 78.3 $9.2 91.7 MCDONNELL DOUGLAS MD-90-30 135.00 130.00 V2528-DS 2 28.0 4.80 5 40 77.2 91.4 91.7 MCDONNELL DOUGLAS MD-90-30 166.00 142.00 V2525-D5 2 25.0 4.80 5 40 84.2 $8.7 91.8 MCDONNELL DOUGLAS MD-90-30 166.00 142.00 V2528-DS 2 28.0 4.80 5 40 82.6 90.9 91.8 3 MITSUBISIG MU-300 (DIAMOND I) 14.10 13.20 2 2.6฿ 2.50 10 30 86.3 88.0 85.8 MITSUBISHI MU-300 (DIAMOND I) 15.50 13.20 JT15D-4D 2 2.68 2.50 30 $1.2 88.4 85.$ 3 MITSUBISHI MU-300-10 (DIAM. II) 15.78 14.22 STISD-S 2 2.88 2.10 10 30 88.6 93.7 91.4 RAYTHEON HAWKER 125- IA 21.20 19.60 TFE731-3-1H 2 3.70 Ż.7û 45 83.4 90.1 96.0 3 RAYTHEON HAWKER 125- IA 21.70 19.60 TFE731-3-IH 2 3.70 2.70 45 $4.2 90.0 96.0 RAYTHEON HAWKER 125- 3A 21.70 20.00 TFE731-3-1H 2 3.70 2.70 45 84.2 90.0 96.3 RAYTHEON HAWKER 125- JARA 23.60 20.00 TFE731-3-1H 2 3.70 2.70 45 85.5 89.8 95.7 RAYTHEON HAWKER 125- 400A 23.60 20.00 TFE731-3-1H 2 3.70 2.70 45 85.5 89.8 95.7 3 RAYTHEON HAWKER 125-600 A 25.50 22.00 TFE731-3-1H 2 3.70 2.70 45 88.0 89.2 96.3 RAYTHEON HAWKER 125- 600A 25.50 22.00 VIPER 601-22 2 3.65 0.00 45 92.3 99.2 102.9 12 RAYTHEON HAWKER 125- 700A 25.50 22.00 155731-3-14 2 3.70 2.70 45 91.6 92.1 96.0 25,33 RAYTHEON HAWKER 125- 700A 25.50 22.00 TFE731-3-1H 2 3.70 2.70 45 88.0 89.2 96.3 3 33 RAYTHEON HAWKER 125- 800 27.40 23.35 TFE731-5R-IH 2 4.30 3.30 45 80.9 87.2 96.5 3 RAYTHEON HAWKER 125- 800A 27.40 23.35 TFE731-5R-IH 2 4.30 3.30. 45 80.9 89.6 96.5 3 25 Page 39
APPENDIX 1
AIRCRAFT NOISE DATA FOR
UNITED STATES CERTIFICATED TURBOJET POWERED AIRPLANES
MTOW MLW THRUST FLAPS NOISE LEVEL (EPNIB) MANUFACTURER MODEL 1000* 1000# ENGINE MODEL NO. 1000₴ BPR IQ AR TQ SL AP STAGE NOTES RAYTHEON HAWKER 125-1000 31.00 25.00 PW305 5.20 4.50 25 81.8 85.9 91.6 RAYTHEON HAWKER 125-1000 35.50 28.50 PW305 2 5.20 4.50 25 85.7 85.3 92.0 SABRELINER SABRELINER 40 17.50 14.00 JT12A-8 3.30 25 89.7 100.4 97.5 SABRELINER SABRELINER 40 20.20 17.50 JT12A-8 2 3.30 25 94.5 100.1 98.4 SABRELINER SABRELINER 60 20.20 JT12A-8 3.30 24 95.0 100.3 98.5 2 SABRELINER SABRELINER 60A/60SC 22.70 20.60 JT12A-8 2 3.30 94.4 100.0 102.2 2 SABRELINER SABRELINER 65 24.00 21.80 TFE731-3R 3.70 2.80 84.0 93.0 90.6 SABRELINER SABRELINER 65 22.70 21.80 TFE731-3R 3.70 2.80 0 36 82.3 93.1 90.6 SABRELINER SABRELINER 75A 23.00 CF700-2D-2 2 4.30 2.00 15 25 90.7 91.3 100.2 • 2 SABRELINER SABRELINER 80 23.30 22.00 CF700-2D-2 4.32 2.00 90.7 91.3 100.2 2 SABRELINER SABRELINER SONSOSC 25.50 22.00 CF700-2D-2 • 2 4.30 2.00 91.2 91.4 101.1 2 Page 40
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|