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
APPENDIX 3 ** STAGE 3*74
TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEVEL (EPNdB) MANUFACTURER MODEL 1000# 1000# ENGINE MODEL NO. 1000# BER IQ IQ SL STAGE NOTES AIRBUS A319-131 158.73 149.91 V2522-A5 2 22.0 4.90 10 40 85.3 91.4 94.5 3 AIRBUS A320-211 149.90 142.20 CFM56-5A1 2 25.0 35 85.3 94.4 96.4 AIRBUS A320-211 162.00 142.20 CFM56-5A1 25.0 35 87.8 94.3 96.4 AIRBUS A320-231 162.00 142.20 V2500.A1 2 25.0 40 86.6 92.8 96.6 AIRBUS A320-231 149.90 142.20 V2500.A1 2 25.0 40 84.0 93.0 96.6 AIRBUS A330-301 396.83 361.56 CF6-80E1A2 2 87.0 97.9 98.5 AIRBUS A330-301 507.06 418.88 CF6-80E1A2 2 94.2 97.2 98.7 AIRBUS A330-321 396.83 330.69 PW4164 2 88.5 98.0 97.3 AIRBUS A330-321 507.06 418.88 PW4164 2 95.6 97.5 98.0 AIRBUS A330-322 396.83 330.69 PW4168 2 87.6 98.6 97.3 AIRBUS A330-322 507.06 418.88 PW4168 2 94.3 98.3 98.0 AIRBUS A340-212 485.01 363.76 CFM56-5C3 2 88.1 95.8 97.3 AIRBUS A340-212 595.25 440.92 CFM56-5C3 96.1 95.4 97.2 AIRBUS A340-312 485.02 363.76 CFM56-5C3 88.0 95.8 97.3 3 AIRBUS A340-312 595.24 440.92 CFM56-5C3 96.2 95.3 97.2 AVRO 146-RJ 85 80.00 77.50 LF 507-1F 18 33 79.0 89.1 96.9 AVRO 146-RJ 85 97.00 85.00 LF 507-1F 18 33 84.3 88.4 97.3 BAc 146-100A 76.00 72.35 ALF502R-3 6.70 5.90 18 33 80.7 87.2 95.1 BAc 146-100 A 76.00 72.35 ALF502R-3A 6.97 5.70 18 33 79.0 88.0 94.9 BAc 146-100A 82.25 73.35 ALF502R-3A 6.97 5.70 18 33 82.3 87.6 95.2 3 BAe 146-100 A 82.25 73.35 ALF502R-5 4 6.97 5.70 18 33 82.3 87.6 95.2 BAC 146-100 A 84.00 77.50 ALF502R-5 6.97 5.70 18 33 81.8 87.7 95.6 3 Page 2
APPENDIX 3 ***STAGE 3***
TURBOJET POWERED AIRPLANES
MTOW MLW THRUST FLAPS NOISE LEVEL (EPNJB) MASUE REK -MODEL 1000% 1000# ENGIE MODEL NO. 1000# BPR IO TO AP SALON OVI BAc 146-200A 90 50 77.50 ALF502R-3 4 6.70 5.90 18 33 85.9 86.6 95.6 BAe 146-200A 89.50 77.50 ALF502R-3A 6.97 5.70 18 33 84.9 87.3 95.6 3 BAc 146-200 A ฿9.50 77.50 ALF502R-5 6.97 5.70 18 33 84.9 87.3 95.6 BAe 146-200A 93.00 81.00 ALF502R-5 6.97 5.70 18 33 85.2 87.3 95.8 BAc 146-300 95.00 83.00 LF 507-1H/-1F 4 18 33 84.0 87.9 97.2 3 BAe 146-300 101.50 88.50 LF 507-1H/-1F 18 33 86.3 87.6 97.6 BAe 146-300A 95.00 83.00 ALF 502R-5 6.97 5.70 18 33 86.0 87.0 96.0 BAe 146-300A 97.50 84.50 ALF502R-5 4 6.97 5.70 18 33 86.5 86.7 95.6 3 BAe C-29 A 28.00 23.35 TFE731-5R-1H 2 4.30 3.30 45 81.4 87.3 95.8 BEECH BEECHJET 400 15.78 14.22 JT15D-5 2.88 10 30 88.6 93.7 91.4 BOEING B-727-100 (Dee Howard) 169.50 137.50 TAY 651-54 3 40 92.1 92.3 98.4 3 BOEING B-727-100 (Dee Howad) 169.50 142.50 TAY 651-54 3 30 92.1 92.3 95.3 3 BOEING B-727-100 (FED EX;3TC 160.50 137.50 JT&D-7 w/BOEING 3 30 92.5 96.6 97.8 35 SA3993NM) INLET+CHIN CSD BOEING B-727-100 (FED EX;STC 163.50 137.50 JT8D-7 ₩/BOEING 30 93.2 97.4 97.8 35 SA3993NM) INLET+FAN CSD BOEING B-727-100 (FED EX:STC 169.50 137.50 J8D-9 w/BOEING 3 30 93.9 97.5 98.1 3 35 SA3993NM) INLET+CHIN CSD BOEING B-727-100 (FED EX:STC 174.50 142.50 JT8D-7 w/BOEING 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 3 30 94.1 96.6 98.2 35 SA3993NM) INLET+CHIN CSD BOEING B-727-100 (FED EX;STC 169.50 142.50 JT8D-7 ₩/BURBANK 3 30 94.1 97.2 98.2 3 35 SA3993NM) INLET+FAN CSD BOEING B-727-100 (FED EXSTC 169.50 142.50 JT8D-9 w/BOEING 3 30 93.9 98.0 98.4 3 35 SA3993NM) INLET+FAN CSD BOEING B-727-100 (FED EX,STC 174.50 142.50 JT8D-9 w/BURBANK 30 94.9 97.1 98.8 SA3993NM) INLET+CHIN CSD BOEING B-727-100 (FED EX:STC 169.50 142.50 JT&D-9 w/BURBANK 30 94.0 97.3 98.8 3 35 SA3993NM) INLET+CHIN CSD BOEING B-727-200 (FED EX;STC 172.60 150.00 JT&D-7 w/BOEING 3 30 96.0 97.4 99.0 3 35 SA4833NM) INLET+CHIN CSD Page 3
8/27197 AC 36-1G APPENDIX 3 **STAGE 3***
TURBOJET POWERED AIRPLANES MTOW MLW THRUST ELAPS NOISE LEVEL (EPNdB) MANUFASTURER MOREL 1000฿ 1000# ENGINE MODEL NO. 1000# IQ IQ SL STAGE NOTES BOEING B-727-200 (FED EX;STC 172.50 150.00 J18D-7 w/BOEING 3 30 95.9 97.0 99.0 3 35 SA4833NM) INLET+FAN CSD BOEING B-727-200 (FED EX;STC 172.60 150.00 JT&D-7 m/BURBANK 3 30 95.7 96.5 98.9 • 3 35 SA4833NM) INLET+CHIN CSD BOEING B-727-200 (FED EX:STC 173.88 150.00 JT&D-9 w/BOEING 3 30 95.5 97.4 99.6 35 SA4833NM) INLET+CHIN CSD BOEING B-727-200 (FED EX;STC 167.85 150.00 JT&D-9 W/BOEING 3 30 94.2 98.3 99.6 3 35 SA4833NM) INLET+FAN CSD BOEING B-727-200 (FED EX;STC 175.00 150.00 JT8D-9 w/BURBANK 30 95.2 97.2 100.2 3 35 SA4833NM) INLET+CHIN CSD BOFING B-727-200 (FED EX;STC 170.48 150.00 JTSD-9 W/BURBANK 3 30 94.3 97.8 100.2 3 35 SA4833NM) INLET+FAN CSD BOEING B-727-200 (FED EX;STC 172.96 154.50 JTSD-9 ₩/BURBANK 3 30 94.7 97.3 100.5 35 SA4833NM) INLET+CHIN CSD BOFING B-727-200 (FED EX;STC 155.00 150.00 JT8D-9 w/BOEING 3 30 $9.2 97.9 97.4 3 27 SAS839NM) INLET+CHIN CSD BOEING B-727-200 (FED EX;STC 155.00 150.00 JT8D-9 w/BOEING 3 30 $9.2 98.4 97.4 27 SA5839NM) INLET+FAN CSD BOEING B-727-200 (FED EX;STC 155.00 150.00 JT8D-9 w/BURBANK 3 30 $8.5 97.6 98.0 3 27 SA5839NM) INLET+CHIN CSD BOEING B-727-200 (FED EX;STC 155.00 150.00 JT8D-9 w/BURBANK 30 88.5 98.1 98.0 3 27 SA5839NM) INLET+FAN CSD BOEING B-727-200 (FED EX;STC 160.00 154.50 JT&D-15 w/BOEING 3 30 92.2 98.0 97.6 27 SAS839NM) INLET+CHIN CSD BOEING B-727-200 (FED EX;STC 150.00 154.50 JT8D-15 w/BOEING 3 30 92.2 98.2 97.6 3 27 SA5839NM) INLET+FAN CSD BOEING B-727-200 (FED EX;STC 178.90 154.50 JT8D-15 3 30 94.3 97.3 98.2 3 27 SAS839NM) w/BURBANK BOEING B-727-200 (FED EX;STC 184.20 154.50 JT&D-17 w/BOEING 3 30 95.3 98.8 97.6 3 27 SAS839NM) INLET BOEING B-727-200 (FED EX;STC 184.20 154.50 JT8D-17 3 30 94.8 98.6 98.2 3 27 SA5839NM) w/BURBANK INLET BOEING B-727-200 (FED EX;STC 189.20 160.00 JT8D-9 w/BOEING 3 30 97.3 95.9 97.9 3 27 SA5839NM) INLET+CHIN CSD BOEING B-727-200 (FED EX:STC 189.20 160.00 JT&D-9 w/BOEING 3 30 97.3 96.5 97.9 3 27 SA5839NM) INLET+FAN CSD BOEING B-727-200 (FED EX;STC 182.75 161.00 JT&D-15 w/BOEING 3 30 93.9 99.1 97.7 3 28 SA5839NM) INLET+CHIN CSD BOEING B-727-200 (FED EX;STC 199.05 166.00 JT&D-15 w/BOEING 30 97.6 98.0 98.1 3 27 SA5839NM) INLET+CHIN CSD BOEING B-727-200 (FED EX;STC 199.51 166.00 JT8D-15 w/BOEING 30 97.6 98.0 97.9 3 28 SA5839NM) INLET+CHIN CSD BOEING B-727-200 (FED EX;STC 199.05 166.00 IT8D-15 w/BOEING 30 97.6 98.2 98.1 27 SAS839NM) INLET+FAN CSD Page 4
APPENDIX 3
TURBOJET POWERED AIRPLANES MTOW MLW THRUST FLAPS NOISE LEYEL (EPNdB) MANDFACTOREK MODEL 1000# 1000# - ENGINE MODEL NO. 1000# BPR TO AP TO SL AP STAGE NOTES BOEING B-727-200RE(VALSAN) 190.50 148.00 JT8D-15/217C 30 91.5 99.3 98.8 £Z'9 BOEING B-727-200RE(VALSAN) 209.50 159.00 ST8D-17A/217C 3 30 94.5 99.6 99.0 6,23 BOEING B-737-200 (AVAERO;STC 128.10 88.00 JT8D-17 2 40 91.4 97.5 96.7 27 ST223CH) BOEING B-737-200 (AVAERO;STC 100.80 95.00 JT8D-15 2 40 83.7 96.8 97.2 27.42 ST223CH) BOEING B-737-200 (AVAERO;STC 100.80 95.00 J8D-9 2 40 85.2 95.5 97.2 3 27.41 ST223CH) BOEING B-737-200 (AVAERO;STC 100.50 98.00 JT8D-15 2 40 84 9 96.9 98.6 35,42 ST223CH) BOEING B-737-200 (AVAERO;STC 100.50 98.00 JT8D-9 2 40 ฿6.3 95.7 98.6 35,41 ST223CH) BOEING B-737-200 (AV AERO,STC 121.50 107.00 JT8D-15 2 30 91.3 96.9 96.3 35,42 ST223CH) BOEING B-737-200 (AVAERO;STC 128.10 107.00 ST8D-17 2 30 91.4 97.5 94.8 3 27 ST223CH) BOEING B-737-200 (AVAERO;STC 118.50 107.00 ST8D-9 30 91.5 94.9 96.3 3 35,41 ST223CH) BOEING B-737-200 (AVAERO;STC 121.50 107.00 JT8D-9 2 40 91.5 94,8 98.0 3 27.41 ST223CH) BOFING B-737-200 (NORDAM;STC 119.50 103.00 J8D-15 w/LGW 2 30 91.1 97.0 95.8 3 37 ST00131SE) HUSHKIT BOEING B-737-200 (NORDAM;STC 119.50 103.00 JT8D-15 w/LGW-L 2 30 90.2 96.8 95.8 3 37 ST00131SE) HUSHKIT BOEING B-737-200 100.80 95.00 ST8D-15 2 40 83.7 96.9 96.9 3 27,42 ADV(AVAERO:STC BOEING B-737-200 100.80 95.00 JT8D-9 2 40 85.3 95.7 96.9 3 27.41 ADV(AVAERO;STC BOEING D-737-200 100.50 98.00 TT8D-9 2 40 86.4 95.8 98.3 3 35,41 ADV(AVAERO;STC BOEING B-737-200 124.50 107.00 JT8D-15 2 30 91.8 96.7 96.3 35,42 ADV(AVAERO;STC BOEING B-737-200 128.10 107.00 JTSD-17 30 91.2 97.7 94.8 27
ADVIAVAERO STC BOEING B-737-200 121.50 107.00 JT8D-9 2 40 91.5 95.0 97.7 27.41 ADV(AVAERO;STC BOEING B-737-200 110.20 98.00 JT8D-9 40 87.3 94.7 98.2 3 27.41 ADV(NORDAM;STC BOFING B-737-200 105.60 103.00 ST8D-15 2 40 84.6 96.3 98.4 3 27,42 ADV/NORDAM;STC BOEING B-737-200 115.50 103.00 JT8D-17 2 40 86.8 97.0 98.4 3 27 ADV(NORDAM;STC Page 5