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
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
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
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
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
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
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
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
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
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