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
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
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
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
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
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
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
AC36-1H
Appendix 2
11/15/01 Appendix 2 Notes 1 Equipped With Standard Hushkit
2 Equipped With Modifications 3305 And 3373
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
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
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
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