ac 36-3g eslimatedmaximuma … · eslimatedmaximuma-wrightedsoundlbvbls measured in accordance with...
TRANSCRIPT
AC 36-3G APPENDIX1
ESlIMATEDMAXIMUMA-WRIGHTEDSOUNDLBVBLS MEASURED IN ACCORDANCE WITH PART-36 APPENDIX-G PROCEDURES
MANUFACTURER AmPLAm ENGINE TOGW
loo0 LBS EST DBA
CONCORDE CONCORDE 0393/M-602 400.00 112.9
BOEING B-747-100 JT=n 750.00 100.5
BOEING E747-loo v9D-m 750.00 1005
BOEING B-747-200 JIIpD3A 767.00 100.5
BOEING s747-100 r9D-m 750.00 loo.2
BOEUUG B-747-200 JLPD-S- 805.00 99.9
BOEING E747-200 JT9D-3AwET 773.00 99.6
BOEING B-747-200 IT=7 770.00 99.4
BOEING T&747-200 ~mf= 785.00 993
BOEING B-747-100 VP7 7lO.00 99.1
BOEING R747-200 JT9ITm 775.00 99.1
BOEING B-747-200/ 300 RB211-524C2 833.00 99.1
BOEING I&747-200/300 RB211524C2 833.00 99.1
MCDONNELL DOUG. DC-1030 CF6-5OCl 590.00 96.4
BOEING B-747- v9D-m 695.00 96.2
BOEING B747-w JT9lS7A 690.00 96.1
BOEING B-747-m RB211524B 800.00 96.0
BOEING f&747-200/300 RB211524C2 775.00 95.7
BOEING B-747-200/300 RB211-524C2 775.00 95.7
MCDONNELL DOUG. DC-1030 CF65OA 565.00 95.7
MCDONNELL DOUG. DC-1030 CF65OCA 565.00 95.7
BOEING B747-w JT9D-7A 660.00 94.9
BOEING E747-sP IT9D-7F 660.00 94.9
MCDONNELL DOUG. DC-1030 CF65OCl 572.00 94.6
BOEING B-747-200 JT9D-70A 820.00 94.1
MCDONNELL DOUG. DC-1030 cF6-5oc 565.00 94.1
BOEING E7073OOB/C COMI’RAN QN IT3D3B 32230 94.0
BOEING B-747-2OQ/3QO RB211524D4 833.00 93.9
BOElNG B-747-200/300 RB211524D4 833.00 93.9
MCDONNELLDOUG. DC-la30 CF65OCl 562.00 93.9
BOEING B-747- JT9D7A 610.00 92.9
BOEING W27-200 JT8D-17RQN 208.00 92.6
BOEING w27-200 JT8DXRQN 208.00 92.6
BOEING B-727-200 JTlD17QN 203.10 92.2
BOEING B-727-200 JT8D-17QN 203.10 92.2
BOEING B-747-200/300 CF6-5OE 833.00 92.2
BOEING I&747-200/300 CFME 833.00 92.2
BOEING B-747-200/300 CF6SOE2 833.00 92.2
BOEING I&747-200/300 cF65oE2 833.00 92.2
BOEING B-747-100 cFu5A2 767.00 92.0
BOEING B-747-m CF6-45A2 767.00 92.0
BOEING B747-loo cFGoE2 750.00 92.0
BOEING B-747-100 cFGsoE2 750.00 92.0
BOEING &747-m CFtXOE2 750.00 92.0
BOEING &747-100 cFMoE2 750.00 92.0
FLAPS
10
10
10
10
10
10
10
10
10
10
10
10
6
10
10
10
10
10
8
8
10
10
10
10
10
14
10
10
10
10
5
5
5
5
10
10
10
10
10
10
10
10
10
10
NOTES
4/8
4,6
44
4/6
4/6
4/6
4/6
4/6
4/6
4th
416 15
15
15
4‘6
4,6 4
15
15
15
15
416
4,6
15
4
15
8
8,15
8,15
15
4/6 2,8,15
2hv5 2,8,14,15
2,8,14,15
8,15
8,15
8,lS
8,15
8,lS
8,15
8,15
8,15
8,lS
8,lS
PAGE 1T
AC 36-36 APPENDIX1
ESTIMATEDMAXIMUMA-WEIGHTEDSOUNDLWELS MEASURED IN ACCORDANCE WITH PART-36 APPENDIX-C- PROCEDURES
*“TAKEOFF”**
MANUFACTURER
MCDONNELL DOUG.
MCDONNELL DOUG.
MCDONNEUDOUG.
MCDONNEU DOUG.
MCDONNELL DOUG.
MCDONNELLDOUG.
MCDONNELL DOUG.
MCDO~DOUG.
MCDO~DOUG.
BOEING
BOEING
MCDONNELL DOUG.
MCDONNELLDOUG.
BAe
BAe
MCDONNELL DOUG.
BOEING
BOEING
BOEING
BOEING
MCDONNELL DOUG.
MCDONNELLDOUG.
BOEING
BOEING
BOEING
MCDONNELL DOUG.
MCDONNELL DOUG.
BAe
BOEING
BOEING
BOEJNG
BOEING
IAI
IM
BOELNG
BOEING
MCDONNELLDOUG.
BOEING
BOEING
BOEING
BOEING
MCDONNELLDOUG.
MCDCINNELLDOUG.
BOEING
PAGE 2T
AIRPLANE ENGINE TOGW .
. 1OOOLBS ESI’ DBA FLAPS NOTES
DC-1040 v9D-A 572.00 91.8
DC-lb40 PD-A 572.00 91.8
DC-O%63 W/ADC QN PD- 355.00 91.7
DC-104 PB2(J 530.00 91.7
DC-1w m20 530.00 91.7
DC-1040 CF63OA 519.60 91.4
DC-1030 CF6-5OA 519.60 91.4
DC-0842 (BACjBACII) PMB 348.00 91.1
DC-0843F W/AK QN P-7 355.00 91.0
B747-400 RB211-524G 875.00 90.8
B-747-400 RB2113524G 875.00 90.8
DC-l&IO JT9D39A 555.00 90.6
DC-lo-40 11PD59A 555.00 90.6
l-11400 SPEY-MK511 89.50 90.5
l-11500 SPEY-Mm2 104.50 905
DC-084 W/TNC QN PMB 350.00 90.5
B-727-200 JTsD-9QN 184.80 90.4
w27ao )TsD-9QN li4.80 90.4
B-7474MF RB211524G 875.00 90.4
B747-4OOF RB211524G 875.00 90.4
DC-08-50 W/QNC QN PD-= 309.80 903
DC484 W/QNC QN lTsD3B 309.80 903
B747-200/300 RB211524D4 775.00 90.2
&747-200/300 RB211524D4 775.00 90.2
B747-a JT9D-7A 570.00 90.0
DC-OS-62 (BAC/BAClI) rnD- 335.00 90.0
DC-OS62 (BAC/Rl) PMB 350.00 90.0
1-11-500 sPEYMK512 99.70 89.9
B-727-200 JTBD-17RQN 197.00 89.9
B-727-200 JT8D-17RQN 197.00 89.9
8-747-400 PW4056 PKG A (FBW 875.00 89.8
B-747a PW4056l’KGA(FEQT) 875.00 89.8
1121 COMMODORE CJ61M 18.50 89.7
1123WEIWlND CJ610-9 20.70 89.7
HFE32OHANSA CJ61@9 2030 89.7
I&747-200/300 cF6-5oE2 775.00 89.6
B-747-200/300 cFuoE2 775.00 89.6
DC4843 W/TNC QN PD-7 355.00 89.6
B747aOOpIO CFMOE 775.00 89.4
B-747-200/300 CFMOE 775.00 89.4
B-7474OOF PW4056PKGA(FB2T) 875.00 89.4
B-747-4ooF PW4056PKGA(FB2T) 875.00 89.4
DC-O&63 (BAC/BACII) JI3D-7 353.00 89.2
DC-OS-63 (BAC/Rl) rnD-7 355.00 89.2
w27ao(FedE%) PB9 189.20 89.1
10
10
12
10
10
8
8
12
12
10
10
10
10
8
8
12
5
5
10
10
-
10
10
10
12
12
8
5
5
10
10
10
10
12
10
10
10
10
12
12
15
15
8,15
15
15
15
15
8,15,16
8,15
8,15
8,15
15
15
8,15
4
8,15
2,8,14,15
2,8,14,15
8,lS
8,15
8,12
8,12
8,15
8,lS
4,6 8,15,16
8,15,16
4
2ku5
2m5
8,15
8,lS
4
4
13
8,15
8,lS
8,15
8,15
8,15
8,15
8,lS
8,15,16
8,15,16
8,15,25,28
AC 36-3G APPENDIX 1
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS MEASURED IN ACCORDANCE WITH PART-36 APPENDIX-C- PROCEDURES
MANUFA-ER AIRPLANE ENGINE TOGW
1OOOLBS EST DBA FLAPS NOTES
BOEING B-727-200 ITSD-1sQN 19050 89.0
BOEING B-727-200 P~15QN 190.50 89.0
BOEING B747-400 RB211524H 875.00 89.0
BOEING B747-400 RB211524H 875.00 89.0
BOEING 87474OOF RB211-524H 875.00 89.0
BOEING B-747-F RB211524H 875.00 89.0
MCDONNELL DOUG. DC-1 (BAC/BAC II) Iz3D3B 325.00 88.8
MCDONNELL DOUG. DC-O&62 (BAC/Rl) PD- 335.00 88.8
MCDONNELL DOUG. DC-1030 cF6-6K 455.00 88.8
LOCKHEED 1329 JEI!XAR mu-8 42.00 88.7
BOEING B-727-200 J’IIID-17QN 190.50 88.5
BOEING B-727-200 J’IlDl7QN 190.50 88.5
BOEING E727-200 (Fed Et) JT8D17 199.50 88.5
MCDONNELL DOUG. DC-lo-10 CF6-6D 440.00 885
MCDONNELL DOUG. DC-lo-10 CF6-6D 440.00 885
MCDONNELL DOUG. DC-0950 pm-15 121.00 88.4
MCDONNELL DOUG. Dc-o9-50 JT8D-15 121.00 88.4
MCDONNELL DOUG. DC-1040 JT9Js20 484.00 88.4
MCDONNELL DOUG. DC-1040 pm-20 484.00 88.4
MCDONNELL DOUG. Dc-0930 pm-17 121.00 88.2
MCDONNELL DOUG. Dc-09-50 pm-17 121.00 88.2
MCDONNELLDOUG. Dc-09-50 JT8n17 121.00 88.2
BOEING B-727-200 JTsD-7QN 172.50 88.0
BOEING B-727-200 JTSD-7QN 172.50 88.0
BOEING B-727-200 (Fed Ex) ITSD-7 178.00 88.0
BOEING B-737-200 JT8D-15QN 117.00 88.0
BOEING B-737-200 IT8D-WN 117.00 88.0
BOEING B-737-200 IT8D-9QN 117.00 88.0
BOEING B-737-200 mD-9QN 117.00 88.0
BOEING B7474OOF CFHOC2BlF W/N1 MOD 875.00 88.0
BOEING B-747-F CF6-8OC2BlF W/N1 MOD 875.00 88.0
BOEING B-747-400F RB211-524G 830.00 88.0
BOEiNG B-7474OOF RB211-524G 830.00 88.0
BOEING B747-400 CF6-8OC2BlF 875.00 87.9
BOEING B-747400 CFk8OC2BlF 875.00 87.9
BOEING B-747400 CFb8OC2BlF W/Nl MOD 875.00 87.9
BOEING B-747-400 CF6-8OC2BlF W/Nl MOD 875.00 87.9
BOEING B-747400 RB211524G 820.00 87.9
BOEING B-747400 RB211524G 820.00 87.9
SABRELINER CORP. SABRE 70 ma-8 21.00 87.9
MCDONNELL DOUG. DC-OS-62 (BAC/BACJI) PD-7 335.00 87.8
MCDONNELL DOUG. DC-0862 (BAC/Rl) F=7 335.00 87.8
BOEING B-747400 PW4Q56 PHASE 3 (FB2B) 875.00 87.6
BOEING B-747400 PW4056 PHASE3 (FI32B) 875.00 87.6
BAe l-11-400 Mall-w/Husm 89.50 87.5
““*TAKEOFF’**
5
5
10
10
10
10
15
12
5
5
5
5
10
10
5
5
1
1
1
1
10
10
10
10
10
10
10
10
10
10
2,8,14,15
2,8,14,15
8,15
8,15
8,15
8,15
8,15,16
8,15,16
15
8,13
2,8,14,15
2,8,14,15
8,15,25,28
15
15
w5
1,8,15
15
15
Lw
w5 1,8,15
2ku5
2~~5
8,15,24,29
2JJ5
2h15
2,8,14,15
2,8,14,15
8,15
8,15
8,15
8,15
8,15
8,15
8,15
8,15
8,15
8,15
8,12
8,15,16
8,15,16
8,15
8,15
15
PAGE 3T
AC 36-36 APPENDIX 1
MANUFACTURER AIRPLANE ENGINE TOGW
1OOOLBS EST DBA
BOEING E727-200 ITSD-1sQN 184.20 875 BOEING E727-200 ITsITlsQN 184.20 87.5 BOEING B-747400 PW4056 PHASE l/PKG B 875.00 87-5 BOEING B-747-400 PW4056PHASE l/PKG B 875.00 87.5
BOEING B-747-F CF6-8OC2B!F 875.00 87.5
BOEING E7474OOF CF&8OC2BlF 875.00 87.5
MCDONNELL DOUG. Dc-0940 JT8D-11 114.00 873
BOEING E737-200 JT8D-17QN 122.50 873
BOEING B-737-200 JT8D-17QN 122.50 873
BOEJNG B-747-400 PW4056 PHASE 3 (FB2C) 875.00 87.3
BOEING B-747-400 PW4056 PHASE 3 (FB2C) 875.00 87.3
BOEING B-727-200 (Fed Ex) JT8D17 190.50 87.2
MCDONNELL DOUG. DC-XI-30 CF6-5OC2 590.00 87.2
LOCKHEED LlOll-1 RB211ZC 430.00 87.1
MCDONNELL DOUG. DC-0930 JTsIF7 108.00 87.1
BOEING E727-200 (Fed Ex) pm-15 19OSO 87.0
BOEING B-737-200 ITSPSQN 114.50 87.0
BOEING E737-200 IT8D-9QN 114.50 87.0
BOEING B-747-200/300 CF6-8OC2BlF 833.00 86.9
BOEING E747-200/300 CFHOC2BlF 833.00 86.9
LOCKHEED LlOll-1 RB211-22C 422.00 86.9
BOEING E727-100 (Fed E%) v-7 174.50 86.8
BOEING E747dOOD CFHOC2BlF W/N1 MOD 833.00 86.8
BOEING E747-QooD CF6-8OC2BlF W/N1 MOD 833.00 86.8
BOEING B-727-200 ITsD-9QN 172.50 86.7
BOEING E747-400 PW4056 PKG A (FB2T) 820.00 86.7
BOEING B-747400 PW4056 PKG A (FBm 820.00 86.7
BOEING B-747-F PW4056 PKG A (FB2’I’) 830.00 86.7
BOEING E747-4OOF PW4056 PKG A (FB2T) 830.00 86.7
BOEING E7474OOF RB211-524H 830.00 86.7
BOENG E747-4ooF RB211-524H 830.00 86.7
MCDONNELL DOUG. DC-1030 CF6-5OC2B 590.00 86.7
BOEING B-727-200 (Fed Ex) F=7 172.60 86.6
MCDONNELL DOUG. Dc-0930 ITSD-9 108.00 86.5
BOEING B-747-400 RB211-524H 820.00 86.3
BOEING E747400 RB211524H 820.00 863
BOEING B-747- CF6-8OCZBlF 833.00 8693
BOEING E747-4OOD CF6-8OCZBlF 833.00 863
BOEING E747-4ooF PW4056 FB2B/2C 875.00 86.3
BOEING E747-4OOF PW4056 F02B/2C 875.00 86.3
MCDONNELL DOUG. Dc-0930 mJ=9 110.00 86.3
BOEING B-727-100 JT8DncD 169.50 86.1
BOEING E747-200/300 CF6-8OC2BlF 820.00 86.1
BOEING E747-200/300 CF6-8KZBlF 820.00 86.1
BOEING B-747-400 PW4056 PHASE 3 (FB2C) 875.00 86.1
.
PAGE 4T
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS MEASURED IN ACCORDANCE WITH PART-36 APPENIjIX-C- PROCEDURES
“**TAKEOFF”**
FtApS
5
5
10
10
10
10
1
1
10
10
15
10
1
1
10
10
10
10
10
5
10
10
10
10
10
10
-
10
10
10
10
10
10
l m
5
10
10
10
NOTES
2,8,14,15
2,8,14,15
8,15
8,lS
8,15
8,15
1m5 2,8,14,15
2,8,14,15
8,15
8,15
8,15,25,28
8,15
8,15
8,15,25
2,8,14,15
2,8,14,15
8,15
8,lS
8,15,16,28
8,15
8,lS
2,8,14,15
8,15
8,15
8,lS
8,15
8,lS
8,15
8,lS
8,15,24,29
8,15
8,15
8,15
8,15
8,15
8,lS
8,15
1,8,15
3f8,14‘15
8,15
8,lS
8,15,23
AC 36-3G APPENDIX 1
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS MEASURED IN ACCORDANCE WITH PART-36 APPENDIX -Co PROCEDURES
BOEING
BOEING
GENERALDYNAMICS
MCDONNELL DOUG.
BAe
BOEING
MCDONNELL DOUG.
MCDONNELL DOUG.
BOEING
BOEING
MCDONNELL DOUG.
MCDONNELL DOUG.
BOEING
MCDONNELL DOUG.
MCDONNELL DOUG.
LOCKHEED
MCDONNELL DOUG.
RAYTHEON
BOEING
BOEING
BOEING
BOEING
BOEING
BOEING
BOEING
BOEING
BOEING
BOEING
LOCKEEED
MCDONNELL DOUG.
MCDONNELL DOUG.
LOCKHEED
LOCKHEED
BOEING
BOEING
DOUGLAS
MCDONNELL DOUG.
BOEING
BOEING
MCDONNELL DOUG.
RAYTHEON
RAYTHEON
mm SABRELlNER CORP.
BOEING
AIRPLANE ENGINE TOGW
1000 LBS EST DBA FLAPS NOTES
B-747-400 PW4056 PHASE 3 (FB2C) 875.00 86.1
B-727-200 (Fed Ex) v-9 173.88 86.0
cv440 R-2800 48.00 86.0
Dc-09-50 pm-17 115.00 85.9
l-11-200 SPEY-m 80.00 85.8
B-737-200 ITsD-7QN 109.00 85.8
Dc-owo pm-15 114.00 85.8
DGQ9-40 JnD-15 114.00 85.8
B747-4OOF CFHOCZBlF W/N1 MOD 830.00 85.6
B-747-4OOF CF680C2BlF W/N1 MOD 830.00 85.6
DC-0872 cFMs6-2-Cl 362.50 85.6
DC4833 cFM562-a 362.50 85.6
B-727-200 (Fed Ex) JTSD-9 165.60 85.5
Dc-0930 ITSD-7 108.00 85.5
Dc-0930 PD-9 108.00 85.4
LlOll-1 RB211-22C 416.00 853
DC-lo-10 CFb6Dl 440.00 85.3
HAWKER12540OA VIPER-522 23.60 853
B-727-100 (Fed Ex) ITSD-7 160.50 85.2
B-727-200 (Fed Ex) P=9 175.00 85.2
B-737-200 P=lsQN 115.50 85.2
E737-200 JTSD-15QN 11550 85.2
B747-400 CF6-8OC2BlF 820.00 85.2
B-747400 CF6-8OC2BlF 820.00 85.2
B-747400 CFb8OC2BlF W/N1 MOD 820.00 85.2
B-747400 CF6-8OC2BlF W/N1 MOD 820.00 85.2
B-7474OOF CF6-8OC2BlF 830.00 85.2
B-7474OOF CF6-8OC2BlF 830.00 85.2
LlOll-1 RB211-22C 396.00 85.2
DC-lo=10 CFG6D 410.00 85.2
DC-lo-10 CF6-6D 410.00 85.2
LlOll RB211-22B 430.00 85.1
LlOll RB211-22B 430.00 85.1
B-727-100 JT8D9FCD 169.50 85.0
B-727-100 JT8D-9FCD 169.50 85.0
DC3 R-1830-90C 25.20 85.0
DC-lo-40 JTm-20 430.00 85.0
B-737-200 F=9QN 109.00 84.8
B-737-200 PD-SQN 109.00 84.8
Dc-0940 JTSD-11 107.00 84.8
HAWKER 125 3A/R VIPER-522 22.70 84.8
HAWKER US- 3A/RA VIPER322 22.70 84.8
L-w=3 CJ610-1 12.50 84.7
SABRE 60 P-A-8 20.10 84.7
B-737-200 JT8D47QN 115.50 84.5
“**TAKEOFF”**
10
8
1
10
10
12
12
10
8
1
1
10
10
10
10
10
10
10
14
14
14
14
5
5
10
1
1
1
8,15,23
8,15,24,28
5
LW
15
2hl4
ml5 l,S,lS
. 8,lS
8,lS
8,15,24,28
vu5 1,8,15
8
15
8,15
8,15,16,28
8,15,24,29
2m5 2,8,15
8,lS
8,15
8,15
8,15
8,lS
8,15
43 15
15
43
4/5
3m5
3,8,15
5
15
2,8,14,15
2,8,14,15
w5
8,15
8,15
4/8 8,12
2,8,14,15
PAGE ST
AC 36936 APPENDIX1
?/w
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS MEASURED IN ACCORDANCE WITH PAR-36 APPENDIX-C- PROCEDURES
MANUFACIWRER
BOEING
BOEING
MCDONNELL DOUG.
BOEING
BOEING
MCDONNELL DOUG.
BAe
BOEING
,BOENG
MCDONNELL DOUG.
SABRELINER CORP.
BOEING
BOEING
BOEING
BOEING
MCDONNELL DOUG.
MCDONNELL DOUG.
MCDONNELL DOUG.
SABRELTNER CORP.
BOEING
BOEING
MCDONNELL DOUG.
MCDONNELL DOUG.
MCDONNELL DOUG.
MCDONNELL DOUG.
RAYTHEON
MCDONNELL DOUG.
BOEING
BOEING
BOEING
BOEING
BOEING
LEARJET LOCKHEED
MCDONNELLDOUG.
MCDONNELLDOUG.
BOEING
PAGE 6T
AIRPLANE
B-747-m
B-747400
DC-1030
s747-400
B-747-400
Dc-09-50 -II l-11-200
B-747400
B-747400
DC-awl SABRE 60A
B-727-100
B-727-100
B7474OOF
B747-400F
DC-lo-30
SABRE 40A
B747-400
B747-400
HAWKER 125- 1A
-lIB/GIII
-lxB/GnI
-mwc
~767300/3OOER
B-767-300/3OOER
-II -II DC-1030
B-727-100
B-737-200
B-737-200
&767-200
B-767-200
IXARJET 25 B/C/D/F XR 1329-25 JEISI’AR
B-737-200 (AVAERO)
““TAKEOFF”*
ENGINE TOGW
1000 LBS EST DBA FLAPS NOTES
PW4056 PHASE 3 (FB2B) 820.00 84.5
PW4056 PHASE 3 (FBZB) 820.00 84.5
CF65OC2 555.00 84.4
PW4056PHASEl/PKGB 820.00 843
PW4056PHASE l/PKG B 820.00 843
pm-15 110.00 843
SPEY MK511-8 65.50 84.2
MK5Oi%W~HUSHClT 80.00 84.1
Pw4056 PHASE 3 (FB2C) 820.00 84.1
PW4056 PHASE 3 (FB2C) 820.00 84.1
cFM56-2-a 337.00 84.1
I?rzA-s 22.70 83.8
JTBWFCD 160.50 83.7
JTBWFCD 160.50 83.7
PW4056 FB2B/2C 830.00 83.7
PW4056 FB2B/2C 830.00 83.7
JTSD-217A 160.00 83.7
J’ID217A 160.00 83.7
CF&5OC2B 555.00 83.6
JT12A-8 19.60 83.4
PW4056 PHASE 3 (FB2C) 820.00 83.2
PW4056 PHASE 3 (FBZC) 820.00 83.2
JTm-209 149.50 83.2
JTaD-209 149.50 83.2
JT8D-217C 160.00 83.1
JT8D217C 160.00 83.1
vPER-522 21.20 83.1
SPEY MK511-8 69.70 82.8
SPEY MK511-8 69.70 82.8
CJ610-6 15.00 82.8
RB211524G 407.00 82.6
RB211-524G 407.00 82.6
SPEY Mull-8 62.00 82.6
SPEY MK511-8 62.00 82.6
CF6-6K 410.00 82.6
J’IID9FCD 160.50 82.4
ITgp7QN 100.50 82.4
ITSD-TQN 100.50 82.4
JT9n7R4E 360.00 82.3
JmMR4E 360.00 82.3
CJ610=6/8A 16.30 82.3
TFE7313lE 43.80 823
JT8D219 160.00 82.1
pm-219 160.00 82.1
JnD15 12350 81.9
10
10
10
10
10 m
10
8
10
10
15 -
5
5
10
10
2
2
5
10
10
0
0
2
2
10
10
20
5
5
20 B
m
5
1
1
1
1
10
20
2
2
1
8,15
8,15
8,15
8,15
8,15
1,8,15
8,15,16
15
8,15
8,15
8,12
3#,14,15
3,8,14,15
8,15
8,15
8,15
8,15
8,15
8,12
8,15,23
8,15,23
8,15
8,lS
8,15
8,15
8,15
8,15,16
8,15,16
4Al8
8,15
8,15
8,15,16
8,15,16
8,15
3Al5
2m4
2m4 8,15
8,lS
8,13
4
8,15
8,15
8,15,32
AC 36-3G APPENDIX1
ESTIMATEDMAXIMUM A-WEIGHTED SOUNDLEVELS MEASURED IN ACCORDANCE WITH PART-36 APPENDIX -C- PROCEDURES
MANUFACTURER
BOEING RAYTHEON BOEING BOEING BOEING BOEING BOEING BOEING BOEING BOEING BOEING BOEING BOEING MCDOIWELL DOUG.
MCDONNELL DOUG.
BOEING
BOENG
BOEING
BOEING
LOCKEEED
MCDONNELL DOUG.
MCDONNELL DOUG.
BOEING
BOEING
BOEING
MCDONNELL DOUG.
MCDONNELL DOUG.
MCDONNELL DOUG.
MCDONNELL DOUG.
NIHON
MCDONNELL DOUG.
MCDONNELL DOUG.
MO~AULNIER
BOEING
BOEING
BOEJNG
BOEING
BOEING
TlEARJET
-w MCDONNELL DOUG.
MWON?YELLDOUG.
SABRELINER CORP.
BOEING
BOEING
AmmANE
B-737-200 ADV (AVAERO)
HAWKER1256WA
B-737-200 (AVAERO)
B-737-200 (AVAERO)
B-737-200 ADV (AVAERO)
B-737-200 ADV (AVAERO)
B-767300
B-767300
B-727-100 (Dee Hwd)
B-727-100 (Dee Hwd)
B-737-200 (AVAERO)
~767300/3OOEEt
E767300/3OOER
B-727-100 (Fed Ex)
E737-100 (AVAERO)
B-737-200 (AVAERO)
B-737-200 ADV (AVAERO)
L188
DC-0930 w/ABS SIC165CH
DC~w/ABSSI’CWCH
W37-200 ADV (AVAERO)
&767300/3OOER
lb767300/3OOER
MD-87
DC-0930 w/ABS!ZCNCH
DC4930 w/ABS SK1613GL
YS-ll A-200
DC-lo-10
DC-lo-10
MS76OB(PARJSn)
B767300
B-767300
E737-200 ADV (AVAERO)
B-767300
B-767300
LEARJEr24D
lEARJEr24D
SABRE 8OA
B-737-4QO
w37aIo
“‘TAKEOFF’+*
ENGINE TOGW
1000 LBS EST DBA
F-9 121.50 81.9
VIPER 601-22 2550 81.9
P-9 120.50 81.8
pm-15 124.50 81.7
JTsD-15 12350 81.7
pm-15 124.50 81.6
IT9p7R4Do 351.00 81.6
IT9IT7R4Do 351.00 81.6
TAY65l-s1: 169.50 81.5
TAY6515Q 169.50 81.5
JT8p9 117.50 81.5
RB211524H 407.00 81.5
RB211524H 407.00 81.5
JT8TX217 149.50 81.4
JTSD-217 149.50 81.4
ITSD-9 160.50 81.3
JTSD-7 11450 81.3
ITSD-7 11450 81.3
JTsp9 11750 81.3
501-D13 116.00 81.3
ITsp9 111.70 81.3
JT8D-9 111.70 81.3
JT8D-7 11450 81.2
PW4Q56 407.00 81.2
Pw4056 407.00 81.2
J’IIID-217A 149.50 81.2
Jl’8D217A 149.50 81.2
JTsD-7 108.50 81.1
P-7 105.00 81.0
DARTMK542 54.00 81.0
CF6-6Dl 386.50 80.9
CF6-6Dl 38650 80.9
MARBOREMC2 8.65 80.9
JT9Dm4E 351.00 80.8
JT9n7R4E 351.00 80.8
PD-9 11550 80.6
CF64OA 351.00 80.6
CF64OA 351.00 80.6
CJ610-6 13.50 80.6
CJ610-6 13.50 80.6
JT8D217C 149.50 80.6
JT8D217C 149.50 SO.6
cF700-2D-2 2550 803
CFM5&3-Bl 142.5Q 80.4
CFM56+Bl 142.50 80.4
FLAPS
1
1
1
1
1
5
5
1
5
5
0
0
1
1
1 -
0
0
1
5
5
1
1
0
0
15
15
10
5
5
1
5
5
20
-
1
1 -
5
NOTES
8,15,31
8,15,16
8,15,31
8,15,31
8,15J2
8,15,31
8,15
8,15
8,lS
8,lS
8,153 8,15
8,15
8,15
8‘15
8,15,16,29
8,15,30
8,153
8,15~
43
8,15,16
8,15,16
8,153
8,15
8,15
8,15
8,15
8,15,16
8,15,16
5
15
15
19
8,15
8,lS
8,153
8,15
8,15
4m7 8
8,15
8,15
12
8,15
8,lS
PAGE 7T
AC 3&3G APPENDIX1
ESTIMATEDMAXIMUM A-WRIGHTED SOUNDLEVELS MEASURED IN ACCORDANCE WITH PART-36 APPENDIX -C- PROCEDURES
MANUFACIURER
BOEING
BOEING
MCDONNELL DOUG.
MCDONNELL DOUG.
MCDONNELL DOUG.
GUUSREAM
MCDONNELLDOUG.
BOEING
BOEING
BOEING
BOEING
BOElNG
BOEING
BOEING
MCDONNELL DOUG.
AIRBUS
MCDONNELL DOUG.
BOEING
BOEING
MCDO- DOUG.
AVRO
AVRO
BOEING
BOEING
BOEING
mm
LEARJET MCDONNELL DOUG.
MCDONNEJL DOUG.
MCDONNELL DOUG.
SABRELINER CORE?
AIRBUS
BOEING
BOEING
MCDONNELL DOUG.
FOIXER
FOKKER
AIRBUS
BOEING
BOEING
AIRBUS
AIRBUS
MCDONNELL DOUG.
BOEING
BOEING
PAGE 8T
AIRPLANE
E767300/3OOER
E767300/3OOER
DC-0930 u/ABS SIC1613GL
-II
DC-O%40w/ABSSICl65CH
E737-200 (AVAERO)
B-747-100
E747-100
E767300/3OOER
E767300/3OOER
E777-200
E777-200
DC-0930 w/ABS SK1613GL
A310322
DC-09-30 w/ABSSK165CH
E767300/3OOER
E767300/3OOER
DC-0930 w/ABS SIC165CH
14bRJ 85
l&RJ 85
B-737-200 ADV (AVAERO)
E767300
E767-300
=&mm LEARJIT25F
Da%10
SABRE 80
A30084-2C
E777-200
B-777-200
DC-0930 w/ABS SIC1613GL
F-28 MKlooO
F-28 MKlOOO
A3ooB
E767300/300EiR
B-767300/ 3ooER
A&322
A310304
DC-0930 w/ABS SKl65C.H
E767300/3OOER
8-767300/B
*‘*TAKEOFF-+
ENGINE TOGW
1000 LBS EST DBA
CF6dHK34F W/NIMOD 41200 803
CFW W/NlMOD 41200 803
JTID-209 140.00 803
pm-209 140.00 803
mD-7 103.00 80.2
SPEY MK511-8 62.00 80.1
JIXlHl 111.00 80.1
pD-15 118.50 80.0
cF645A2 570.00 80.0
CFMA2 570.00 80.0
Pw4060 408.00 80.0
Pw4060 408.00 80.0
RRTRENT875 535.00 80.0
RR@rRENT875 535.00 80.0
JIzID-9 105.00 80.0
pD-7R4El 33730 79.9
JT8D-11 111.00 79.9
CF6-80C2B4 407.00 79.8
CF6-8OC2B4 407.00 79.8
lT8D-7 105.00 79.8
LF507-1F 97.00 79.7
~50701F 97.00 79.7
pm-15 118.50 79.7
CF6-80A2 351.00 79.7
CF6-8OA2 351.00 79.7
CJ6lOd 15.00 79.7
CJ610-6 15.00 79.7
JT8D-7 90.70 79.7
JnD219 14950 79.7
JTsn219 149.50 79.7
cF7mm-2 2330 79.6
cF6-5oc 346.50 79.4
RRTRENT877 535.00 793
RRTRENT877 535.00 793
lTsD-9 limo 793
SPEY MK55515 65.00 79.2
sPEYMK55s15 65.00 79.2
CFMOA 302.00 79.1
CF6-8oC2B6 412.00 79.1
CF6-80C2B6 412.00 79.1
JTYD7R4El a.69 79.0
CF6-8OC2A2 346.12 78.9
PD-9 105.00 78.8
CF680C2B6F W/N1 MOD 408.00 78.7
CF6dK2B6F W/NlMOD 408.00 78.7
0
0
5
5
0
18
18
1
5
5
8
8
10
1
1
15
NOTES
8,15
8,lS
8,15
8,15
8,15,16
8,15,16
8,15,16
8,159 8,15
8,15
8,15
8,15
8,lS
8,15
8,15,16
8,15
8,15,16
8,lS
8,15
8,15,16
8,15,22
8,1522
8,15,30
8,lS
8,15
8,13
4J3 8,15
8,15
8,15
12
4,8,9
8,15
8,15
8,15,16
4
4
43
8,15
8,15
8,lS
8,15
8,15,16
8,15
8,15
AC 36-36 APPENDIX 1
ESTIMATEDMAXIMUM A-WEIGHTED SOUND LEVELS MEASURED IN ACCORDANCE WITH PART-36 APPENDIX-C- PROCEDURES
IMANUFA-ER
MCDONNELL DOUG.
MCDONNELLDOUG.
MCDONNELLDOUG.
MCDONNELL DOUG.
MCDONNELL DOUG.
AIRBUS
BOEING
BOEING
BOEING
BOEING
BOEING
BOEING
AER~ATLATIE
AIRBUS
AIRBUS
BAe
BAe
MCDONNELL DOUG.
MCDONNELL DOUG.
MCDONNELL DOUG.
AIRBUS
BOEING
BOEING
BOEING
BOEING
BAe
BOEING
BOEING
BAe
BAe
BOEING
FOKKER
FOKKER
AIRBUS
AIRBUS
BOEING
BOEING
BOEING
BOEING
BOEING
BOETNG
‘LEARJET BOEING
BOEING
BOEING
AIRPLANE
Dc-o9-10
A3ooB4-2C
E767300/3OQER
E767300/3OOER
B-737-400
B-737400
B-737-500
E737-500
NORD-262C
A3OOB2-1A
A3OOB2-1A
BAe-1-A
BAe-748 SERlEs 2B
DC-O9-20 w/ABS SK1613GL
A310324
B-737-300
E737300
E767300/30OER
E767300/3OOER
wscouNT745
E777-200
E777-200
BAE-748 SERB 2A
BAe-748 SERIES 2B
E767300/3OOEJX
F-27-200
F-27-500/600
A3OOB4-2C
A3OOBkZC
E737-500
E737-500
E767300/3OOEX
E767300/3OOER
8777-200
E777-200
LEARF 24B/D W/RAISBECK
E737400
E737400
E767-200/2OOER
**“TAKEOFF-*
ENGINE TOGW
1000 CBS EST DBA FLAPS NOTES
JTIiD-217 140.00 78.7
JT8D-217 140.00 78.7
JTl!D-217A 140.00 78.7
JIItD-217A 140.00 78.7
JTSD-7 90.70 78.6
cF6-5oc 336.60 78.5
CF6-8OC2B6F 408.00 78.5
CFHOCZB6F 408.00 785
CFMSNE2 150.00 78.4
CFM563E2 Eo.00 78.4
CFM!%i&Bl(R) 132.80 78.4
CFM!%%Bl(R) 132.80 78.4
BASTAN-VIIA 22.90 78.3
CFk5OA 312.40 78.3
CF6-5OA 312.40 78.3
ALF-502R-S 97.50 783
RR-DART&K535 4630 78.3
JTSD-9 100.00 783
Jl”8D-217C 140.00 78.3
JT8D-217C 140.00 78.3
PW4152 346.12 78.2
CFM56+Bl 139.50 78.2
CFM563Bl 139.50 78.2
CF6-8OC2B7F 412.00 78.2
CF6-8OC2B7F 412.00 78.2
RRDART6h4K510 72.50 78.1
RRTRENT875 506.00 78.1
RRlxENT875 506.00 78.1
RR DART MK532-2L 44.50 78.0
hK535W/HUSHKlT 46.50 78.0
Pw4060 PHASE 3 (FB2C) 412.00 78.0
MK532-7 43.50 78.0
h&532-7R 43.50 78.0
CF650C 330.00 77.9
CF65OC 330.00 77.9
CFM563-Bl 139.00 77.9
CFM563-Bl 139.00 77.9
CFHOC2B7F 407.00 77.8
CF6-8OC2B7F 407.00 77.8
Pw4m 535.00 77.8
Pw4077 535.00 77.8
CJ610-6 1350 77.8
C-B1 138.50 77.7
C-B1 13850 77.7
cF6ac2B4 387.00 77.7
8,15
8,15
8,15
8,15
1,8,15
4319 8,15
8,15
8,15
8,15
8,15
8,15
4,8
l&9 4A9
8,15,22
8,15
8,15,16
8,15
8,15
8,15
8,15
8,lS
8,15
8,lS
11
8,15
8,15
8,15
8,15
8,15,23
5
5
4,8#9
4kV 8,15
8,15
8,15
8,lS
8,15
8,lS
8,13
8,15
8,15
8,15
PAGE 9T
AC 36-3G APPENDIX1
?lwj -
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS MEASURED IN ACCORDANCE WITH PART-36 APPENDIX-C- PROCEDURES
MANUFACINRER
SABRELINER CORP.
BAe
MCDONNELLDOUG.
MCDONNELLDOUG.
BOEING
BOEING
MCDONNELL DOUG.
MCDONNELL DOUG.
AIRBUS
AIRBUS
BOEING
FAIRCHILD
AIRBUS
AlRBUS
BOEING
BOEING
AIRBUS
AIRBUS
BOEING
BOEING
BOEING
DASSAULT
DASSAULT
AIRBUS
AIRBUS
AIRBUS
AIRBUS
AIRBUS
BAe
BAe
BOEING
BOEING
AIRBUS
MCDONNEUDOUG.
AIRBUS
BOEING
RAYTHEON
RAYTHEON
AER~PATIALE
AIRBUS
AIRBUS
FOISKER
FOISKER
PAGE TOT
AIRPIANE
SABRE 75A
BAe-1-A
w77-200
B-777-200
MD-87
A310221
A310308
B-767-200/2OOER
F-27-F
A310-203
A310-203C
B-737400
B-737400
A3OOB2-1C
A3ooB2-1C
B-767-200
B767300/3OOER
B767300/3OOER
FALCON 20
FALCON 20
A310-222
A3OOBl
A3OOBl
A3OOB2-1A
A3OOB2-1A
BAe-146-200A
BAe-146-200A
B767300/3OOER
B7673OOf 300ER
A310-203C
DC-0940 w/ABS S’K1563GL
A310324
E767-200/2OOER
HAWKER 125- 700A
HAWKER 125- 700A
MOHAWK 298
A3OOB2-1C
A-3OOB2-1C
F-27 MK500/600
F-27-100
A-3OOB2-K3C
““*TAKEOFF-+
ENGINE TOGW
loo0 LBS EST DBA
cF700-2D-2 23.00 77.7
ALF-502R-5 95.00 77.6
JTBD-219 140.00 775
JT8D-219 140.00 77.5
RRTRENT877 506.00 77.4
RRTRENT877 506.00 77.4
pm-219 140.00 77.4
JT8D219 140.00 77.4
JIYDJR4Dl 313.05 773
CF6-8OC2AS 36155 77.3
Pw4056 PHASE 3 (FB2C) 395.00 77.3
RRDARTMK529 38.50 773
CF68OA3 313.05 77.2
CF6-8OA3 313.05 77.2
cFM563C-1 150.00 77.2
cFM563C~1 150.00 77.2
CF6-5OC 312.40 77.1
CF65OC 312.40 77.1
JT9DJR4D 315.00 77.1
CF6-8OC2B4 380.00 77.1
CF6-8OC2B4 380.00 77.1
CmO-2D-2 28.60 77.0
cF700-2D-2 28.60 77.0
JT9D7R4El 313.05 76.9
CF65OA 302.00 76.8
CF6-5OA 302.00 76.8
CF6-50A 301.40 76.8
CF65OA 301.40 76.8
ALF-502R-5 93.00 76.7
ALF-502R3Al-5 89.50 76.5
RB211524G 340.00 76.4
RB211-524G 340.00 76.4
CF6-8OA3 305.55 76.3
ITSD-7 90.70 763
PW4152 330.69 76.2
PW4052 351.00 76.2
TFE7313R-1H 25.50 76.1
TFE7313R-1H 2550 76.1
PT6A-45A 23.40 76.0
CFMoc 302.90 76.0
cF6-5oc 302.00 76.0
MK552-7R 45.90 76.0
RRDART6MK514 39.00 76.0
10540-ElB5 6.80 76.0
CF6-5OC 31240 75.9
FLAPS
18
0
0
0
0
5
5
18
18
5
5
10
1
0
NOTES
4
8,15,22
8,15
8,15
8,lS
8,15
8,15
8,15
8,15
8,15
8,15,23
11
8,15
8,15
8,15
8,15
4/v
WV
8,15
8,15
8,15
8,15
8,15
8,15
4,8,9
4M
u&g
uv 8,15,22
8,15,22
8,lS
8,15
8,15’
8,15,16
8,15
8,15
8,15,20,26
8,15,20,26
4
43tg
4A9
15,16
11
10
QAV
ESTIMATEDlkMXMUM A-WEIGHTED SOUND LEVELS MEASURED IN ACCORDANCE WITH PART-36 APPENDIX -C-PROCEDURES
MANUFACKJRER
AIRBUS
AIRBUS
BOEING
BOEING
BOEING
BOEING
BOEING
BOEING
BAe
BOEING
RAYTHEON
RAYTHEON
RAYTHEON
RAYTHEON
AVRO AVRO
BOEING
BOEING
AIRBUS
BOEING
BOEING
BOEING
BOEING
BOEING
BOEING
FOIXER
RAYTHEON
RAYTHEON
BOEING
BOEING
BOEING
BOEING
FOKKER
BEECH
BEECH
BOEING
BOEING
LOCKHEED BOEING BOEING
MWONNELL DOUG. MCDONNELLDOUG. AIRBUS -JET
AIRPLANE
A3OOB2X3c
A-310-222
B-757-200
8757-200
8-757-200
B-757-200
E767300/3OOER
E767300/3OOER
BAe-14MOOA
E767-200/2OOER
HAWKER125 60OA
HAWKER125-600A
HAWKER 125 700A
HAWKER 125 700A
14GRJ 100
l&RJ 100
B-767300
B-767300
A310308
E737300
8737300
E747-4OOD
E747-400D
E767300/3OOER
E767300/3OOER
F-28 MK4000
HAWKER 125 700A
HAWKER 125- 700A
B-737-400
B-737400
E7474OOD
E7474OOD
F-27MK500/600
c35
E35
E757-200
E757-200
1329-25 JEISMR w/STAR 3
E767-300
E767-300
1329-23 JEISMR w/STAR 3
A310-204
LEARJR 24F
*“*TAKEOFF”*”
ENGINE
CF6-5OC
JTmJR4El
PW2037
PW2tU7
RB21163SC
RB211-535C
CF6-8OCZBzF
CF6-8OCZB2F
CFMOC2B2
TFE731-MH
TFE731-NH
TFE7313-1H
TFE731-S1H
LF507-1F
L.F507-1F
P~7RQDo
J?pD-7RQDo cF&8oc2A8
CFM56-3E2
CFM563E2
CFMOC2BlF W/N1 MOD
CFMOC2BlF W/N1 MOD
RB211-524H
RB211-524H
SPEY MK555-15H
TFE73l&lH
TFE7313-1H
CFM563E2
CFM563E2
CFMOC2BlF
CF6-8OC2BlF
MK552-7R
E-18511
E-225-8
PW2037(BG3)
PW2037(BG3)
TFE7313
JlYDJR4E
pDJR4E
nE7313
JT8D-217A
JTh217A
CFMOC2A2
CJ610-6
TOGW loo0 LBS EST DBA FLAPS NOTES
312.40 75.9
30555 75.9
25550 75.9
255.50 75.9
240.00 75.9
240.00 75.9
351.00 75.9
351.00 75.9
101.!50 75.8
351.00 75.8
25.50 75.8
25.50 75.8
25.50 75.8
25.50 75.8
101.50 75.7
101.50 75.7
300.00 75.7
300.00 75.7
346.12 75.6
139.50 75.6
139.50 75.6
600.00 75.6
600.00 75.6
340.00 75.5
340.00 75.5
73.00 75.5
24.20 75.4
24.20 75.4
138.50 75.3
138.50 75.3
600.00 753
600.00 75.3
45.00 75.3
2.70 75.0
2.70 75.0
250.00 75.0
250.00 75.0
4430 75.0
300.00 74.8
300.00 74.8
44.25 74.7
125.00 74.7
125.00 74.7
313.05 74.6
12.90 74.6
5
5
1
18
18
5
5
1
1
10
10
5
5
15
5
5
10
10
0
m
5
5
20
5
5
20
0
0
20
AC 36-3G APPENDIX 1
4M 8,15
8,15
8,15
8,15
8,15
8,15
8,15
8,15,22
8,15
8,15
8,15
8,15,26
8,15,26
8,15,22
8,15,22
8,15
8,15
8,15
8,15
8,15
8,lS
8,15
8,lS
8,15
8,15,26
8,15,26
8,15
8,15
a,15
8,15
15,16
11
11
8,15
8,15
811534
8,15
8,15
8S5t33
8,15
8,15
8,15
4t8
PAGE 11T
AC 3636 APPENDIX 1
ESTIMATKDMAXIMUM A-WEIGHTED SOUNDLNELS MEASURED IN ACCORDANCE WITH PART-36 APPENDIX-C- PROCEDURES
MANUFAcZlTJRER
wE3NG
BOEING
BOEING
BOEING
MCDONNELL DOUG.
MCDONNELL DOUG.
AVRO
AVRO
BOEING
BOEING
BOEING
CESSNA
GENERALDYNAMICS
BOEING
AIRBUS
BOEING
BOEING
BOEING
BOEING
BOEING
BOEING
BOEING
BOEING
BAe
BOElNG
AEROSPA’IUKE
BOEING
BOEING
BOEING
LEARJET BEECH
CESSNA
AIRBUS
AVRO
AVRO
BOEING
BOEING
BOEING
BOEING
BOEING
AIRBUS
BOEING
BOEING
PAGE 12T
AIRPIANE
B-767300
E767300
B-777-200
B-777-200
146-RJ 100
146-RJ 100
w37400
B-737400
E767-200/2OOER
207
cv-580
B-767-200/2OOER
A320-211
B-757-200
B-757-200
B-757-200
B-757-200
B-767300
B767300
B-737300
E7373a)
BAe-1-A
I&767-200/2OOER
ATR72-200
8-757-200
B-777-200
B-777-200
LEARJEr 24E
B55
T21OL
A320231
14kRJ 70
l&RJ 70
B-767-200
B757-200
B-757-200
B767300/3OOER
R767300/3OOER
A310221
w77-200
B-777-200
-4100
A310-203
*“*TAKEOFF”**
ENGINE - TOGW
looo LBS EST DBA FJAPS NOTES
CFMOA 300.00 745
CF6-8OA 300.00 74.5
GE9&76B 535.00 745
GE90-76B 535.00 74.5
JT8D-217C 125.00 74.5
JI’8D217C 125.00 74s
LF507-1F 97.50 74.3
LF507-1F 97.50 74.3
CFM563C-1 138.50 743
cFM563G1 13850 743
PM052 335.00 74.3
10-520-F 3.80 743
501-D13 54.60 74.3
Cw8oC2B4 351.00 73.8
CFM56-5Al 162.00 73.7
Pw2040 25550 73.7
PW2040 255.50 73.7
RB211-535E4 255.50 73.7
RB211-535E4 25550 73.7
CFMOA2 300.00 73.7
CF6-8OA2 300.00 73.7
CFM5hSBl 124.50 73.6
CFMS-SBl 124.50 73.6
LF507 95.00 73.4
Pw4056 340.00 733
PW124/HS 14SFll 4830 73.2
PW-2037(BG3) 240.00 73.2
PM74077 447.50 73.1
Pw4077 447.50 73.1
CJ610-6 12.90 73.1
10470-L 5.10 73.0
lSIO-520-R 3.80 73.0
V25OO.Al 162.00 72.9
LF507-1F 95.00 72.9
LF507.IF 95.00 72.9
JT9MR4D 282.00 72.9
RB211-535C 220.00 72.8
RB211-535C 220.00 72.8
CF6-8OC2B6F 345.00 72.7
CF6-8OC2B6F 345.00 72.7
JIYIMR4Dl 27557 72.6
GE90-76B 506.00 72.6
GE%76B 506.00 72.6
TPE331-148OlH/802H/805 24.00 72.5
cF6-8oA3 275.57 72.4
5
5
0
0
18
18
5
5
1 -
1
1
15
5
20
18
18
1
8,15
8,15
8,15
8,15
8,15
8,15
8,15,22
8,15,22
8,lS
8,15
8,15
11
10
8,15
8,15
8,15
8,15
8,153
8,15,35
8,lS
8,15
8,15
8,15
8,15,22
8,15
15
8,15
8,15
8,15
4/8
11
11
8,15
8,35,22
8,15,22
8,15
8,15
8,15
8,15
8,15
8,15
8,15
8,15
1515
8,lS
AC 36-36 APPENDIX 1
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS MEASURED IN ACCORDANCE WITH PART-36 APPENDIX-G PROCEDURES
MANUFACTURER
AJRBUS AIRBUS
BAe
BOEING
BOEING
BOEING
BOEING
RAYTHEON
RAYTHEON
RAYTHEON
RAYTHEON
AEROSPAIUUE
AVRO
AVRO
BOEING
BOEING
BOEING
BOEING
IAI
DASSAULT
FOKKEX
-IsHi
AERO6PATIALE
BEECH
MrmJBIsHI
RAYTHEON
RAYTHEON
DASSAULT
IAI
LEARjET
mm SHORTS
BOEING
BOENG
BOEING
-A
DASSAULT
DASAULT
BOEING
DASAULT
RAYTHEON
RAYTHEON
RAYTHEON
AIRPLANE
A31&204
A310304
BAe-146-1OOA
B-757-200
B-757-200
B757-200
B-757-200
HAWKER 125 3A/RA
HAWKER 125- 3A JRA
HAVVKER125400A
HAWICER12MOOA
ATR72-210
14kRJ 85
146-RJ 85
B-757-200
B-757-200
B-737-500
B-737-500
1125AsrRA .
FALCON 2K5/D5/E5
Floo
PA-28235
MU3OODIAMONDI
ATR72-210
BEECHJET
MU300-10 DIAMOND II
HAWKER 1251OOOA
HAWKER 125-1OOOA
FALCON 200
1124Iw vMmwIND Iw
JEmREAM4100
LXARJEWA
LEARJET36A
SICYVAN
B-737300
B-737300
W57-200
210
FALCON 20
FALCON 20-D
E767-200/2OOER
FALCON 900
HAWKER 125 1A
HAWKER 125- 1A
HAWKER 125 3A
“‘TAKEOFF”“’
ENGINE
CF6aOaA2
CF6-8OC2A2
ALF502R3A/S
RB211535E4
RB211535E4
RB211-535E4B
RB211-535E4B
TFE73lslH
TFE7313-lH
TFE731-3-1H
TFE7313-1H
PWl27/HS 14SFll
LF507-1F
LF507-1F
RB211535E4B
RB211-535E4B
CFM56+Bl(R)
-WW TFE731-3A-200G
TFE7315AR-2c
RR TAY MK620-15
oam4B5
P-D-4 PVV127/HS 14SFll
ln5D-5
D-D-5
ATF3-6AX
TFE7313-1G
TPE331-14-8OlH/802H
TFE731-2
TFE731-2
TPE331-201
cFM563B-2
cFM563B-2
PW-2037(BG3)
10-520-L
CF700-2D2Q
CF700-2D-2 w/GE CID 654
CFMOA *
TFE731-5AR-1c
TFE7313-1H
TFE7313-1H
TFE731-MH
TOGW 1000 LBS EST DBA FLAPS NOTES
295.41 72.4
295.41 72.4
84.00 72.4
25530 72.4
25530 72.4
255.50 72.4
255.50 72.4
23.60 72.4
23.60 72.4
23.60 72.4
23.60 72.4
48.50 72.3
93.00 72.3
93.00 72.3
255.50 72.3
255.50 723
115.50 72.2
11550 72.2
24.65 72.1
29.10 72.0
95.00 72.0
3.00 72.0
14.10 71.9
47.40 71.8
15.80 71.8
15.80 71.8
31.00 71.8
31.00 71.8
32.00 71.7
23.50 71.7
23.00 71.6
18.00 71.6
18.00 71.6
12.50 71.6
124.50 7ls
124.50 71.5
230.00 71.4
3.80 71.4
28.60 71.4
28.66 71.4
279.90 7l3
45.50 71.2
21.70 71.2
21.70 71.2
21.70 71.2
18
5
15
18
18
12
15
15
5
12
0
1
20
8,lS
8,15
8,15,22
8,15,36
8,15,36
8,15,36 . 2. 8,15,36
8,15
8,15
8,15
8,15
15
8,15,22
8,15,22
8,15,35
8S5t35
8,15
8,lS
8,15
8,lS
8,15
11
12
15
15
15
8,15
8,15
8,15
15
1515
15
15
8,15
8,15
8,15
10,ll
8,15
8,15
8,15
8,15
8,15
8,15
8,15
PAGE 13T
AC 36-3G APPENDIX1
ESTIMATEDMAXIMUM A-WEIGHTED SOUND LEVELS MEASURED IN ACCORDANCE WITH PART-36 APPENDIX-C- PROCEDURES
lblANUFA=ER
RAYTHEON
SHORTS
BEECH
MCDONNELL DOUG.
AIRBUS
AIRBUS
BEECH
BEECH
BEECH
BEECH
BOEING
BOEING
CESSNA
CESSNA
EMBRAER
FAIRCHILD
FAIRCHILD
FAIRCHLLD
GULFSRUM
PIER
DASSAULT
DASSAULT
BOEING
BOEING
SABRELJNER CORP.
AEROSPATLALE
AIRBUS
DMAULT
DASSAULT
UP
UP RAYTHEON
RAYTHEON
Amus
BOEING
BOEING
BOEING
IAI
IN
-A
CASA AIRCRAFT
PAGE 14T
AIRPLANE
HAWKER 125 3A
C99AELlNER
MD-9030
A32Mll
A32Mll
35333
A36
B36’KBONANZA
=WBLW B-737500
B-737-500
T2lOM
TU206G
Em llw2
SA226-AT
SA.226T
SA226-‘ICMEIRO II
GWXIREAMI
PA31350
PA32300
PA32R300
PA32RT300
FALCON 50
FALCON 50
B767300/3OOER
E767300/3OOER
SABRE 65
ATR72-200
A320-211
FALCON 20-F5
FALCON 20-F5
LEARJETS
LEARJETS HAWKER 12% 1A
HAWKER 125- 1A
A320231
B767=200/2OOER
B=767300/3OOER
E767300/3OOER
1124A VVBWIND II
1125 ASIRA
PA42 CHEYENNE
206
CNa5-200
‘++TAKEOFF”+
ENGINE TOGW
1000 CBS EST’ DBA FLAPS NOTES
TFE731alH 21.70 71.2
PT6A45A 2240 71.2
PT6A-34 1130 71.1
V2525D5 156.00 71.1
CFM565Al 149.90 71.0
CFM56-5Al 149.90 7x0
Io47Mc 3.00 71.0
10-520-BA 3.69 71.0
TS10-520u 3.85 71.0
10-470-L 5.10 71.0
CFM563-Bl 11550 71.0
CFM56-3Bl 115.50 71.0
TSIO-520-R 3.80 71.0
TsIo520-M 3.60 71.0
FT6A-34 1250 71.0
‘IPE3313U3@G 12.50 71.0
TPE3313U3O3G 12.50 71.0
TPE-331-3UW-30% 12.50 71.0
RRDARTMK529 35.10 . 71.0
TiM4@J2BD 7.00 71.0
10-54MclG5D 3.40 71.0
1054OXlG5D 3.60 71.0
IO54OxlA5D 3.60 71.0
TFE731-3-1c 38.80 70.9
TFE731-31c 38.80 70.9
CF68OC2BZF 300.00 70.8
CF6-8OC2B2F 300.00 70.8
TFE7313R-1D 24.00 70.8
PWl24/HS 14SFll 44.07 70.7
CFM56-5Al 149.90 70.7
TFEmJAR-2c 29.10 70.6
TFE7315AR-2c 29.10 70.6
TFEm-2 17.00 70.6
TFE731-2 17.00 70.4
TFE731alH 21.20 70.4
TFE731alH 21.20 70.4
V25OO.Al 149.90 703
CF6-8OC282 300.00 703
Pvv4060 315.00 703
Pw4060 315.00 703
TFE7313-1G 23.50 703
TFE7313A-200G 23.50 703
FIbA- 1050 703
IO-S20-A 330 70.2
cm9c 34.80 70.1
5
20
20
5
5
15
10
10
8
8 m
a
1
5
5
12
12 e
10
8,15
8,15
5,ll
8,lS
8,15
8,15
10,ll
11
11
11
8,lS
8,15
11
11
4
4
4
4
15
11
11
11
8,15
8,15
8,lS
8,lS
8,12
15
8,15
8,15
8,15
4
4
8,15
8,15
8,15
8,15
8,15
8,15
15
8,15
10,ll
11
15
AC 36-36 APPENDIX 1
ESTIMATEDMAXIMUM A-WEIGHTED SOUND LEVELS
MANUFACTURER
BEECH
BEECH
BEECH
CESSNA
CBSNA
CESSNA
BOEING
DASSAULT
FOKKER
FOKKER
AVRO
AVRO
RAYTHEON
RAYTHEON
RAYTHEON
RAYTHEON
BEECH
BOEING
BOEING
FATRCHILD
(TF,CSNA
DASSAULT
DASGAULT
CESSNA
CESSNA
CESSNA
DASSAULT
DASSAULT
FAJRCHILD
FAIRCHILD
FOKKER
BAe
BEECH
BOEING
BOEING
-A
=A
DEHAVILLAND
MCDONNELL DOUG.
PIPER
AIRPLANE
“‘TAKEOFF’*
ENGINE TOGW
1000 LBS EST DBA
SC33A 10520-B 330 70.0
F33A IM20-B 3.40 70.0
WA= 10-470-c 3.00 70.0
182P 040-s 3.00 70.0
320C TSIO-470-D 5.20 70.0
337H 1036&G 4.60 70.0
6olP 1054oslA5 6.00 70.0
PA31325 TIM40-F2BD 6.50 70.0
PA32R3Ol 10540-IclaD 3.60 70.0
PA4631P htfALIBU TBIO520-BE 4.10 70.0
w57ao PVV-2037@G3) 220.00 69.9
FALCON 900 TFE731-5BR-1C 46.50 69.9
Floe RRTAY MK65M5 98.00 69.9
Floo RR TAY MK650-15 98.00 69.9
l&RJ 70 LF507-1F 84.00 69.8
146RJ 70 LF507-1F 84.00 69.8
HAWICER125-800A TFE7315R-1H 27.40 69.7
HAWKER125-8OOA TFE731-SR-1H 27.40 69.7
HAWKER12MOOA TFE7315R-1H 27.40 69.7
HAWKER125-8OOA TFE73MR-1H 27.40 69.7
?Il8 R-985AN-14B 9.90 69.6
B-757-200 PW2037 220.00 69.6
B-757-200 PW2037 220.00 69.6
SA227-AT MERIM III C TPE331-1ou 13.20 69.5
CITATION V (560) JT1WA 16.30 69.4
FALCON 10 TFE731-2 1930 69.4
FALCON 10 TFml-2 1930 69.4
CiTA’TTONIU(65O) TFE7313B-loos 22.00 69.3
CITA’IlONllI(650) TFE7313Bloas 22.00 69.3
ClTA‘ITONVI(650) TFE7313Cloos 22.00 69.3
FALCON 2O-C5/DS/E5 TFE731-5AR-2c 29.10 69.2
FALCON 900 TFE73MAR-1c 45s 69.2
SA226-AC MEI’RO III TpE331-1lU 14.50 69.2
SA227-ATMERLINNC TPE331-1lU 14.50 69.2
F70 RR TAY MK620-15 92.00 69.2
BAe-146-100A ALF-502R3A/5 76.00 69.1
V35B (3BLD) 10-520-B 3.40 69.0
E767300/3OOEJX CF63OC2B4F W/N1 MOD 295.00 69.0
B-767300/ 300ER CF68OC2B4F W/N1 MOD 295.00 69.0
180 047@J 2.80 69.0
182Q 0470-u 3.00 69.0
DHC-7 PT6A-50 45.50 69.0
MD-9030 V2528-D5 156.00 69.0
PA31310 TIO-54MUC 6.50 69.0
PA32R3OlT TIO54O-SlAD 3.60 69.0
FLAPS
5
20
11
11
11
10,ll
11
11
11
11
11
11
8,15
8,15
8,lS
a
18
18
8,lS
8,15,22
8,15,22
8,15,20
8,15
8,15
8,15,20
11
8,15
15
15
7
7
8,15
5,ll
8,15
8,15
8,15
m5 7,8,15
8,15
8,15,27
7 8,15
10,ll
10,ll
18
8,15
8,15,22
11
8,15
8,15
11
10,ll
15
8,15
11
11
PAGE 15T
AC 36-3G APPENDIX1
ESTIMATEDMAXIMUM A-WEIGHTED SOUNDLEVELS MEASURED IN ACCORDANCE WITH PART-36 APPENDIX-C- PROCEDURES
MANUFACZURER
BOEING
BOEING
FAIRCHILD
-ET BEECH
BEECH
BEECH
CASAAIRCRAFI’
CESSNA
CESSNA
AEROSPATIALE
=J= SHORTS
RAYTHEON
BOEING
BOEING
DASSAULT
BEECH
B--NORMAN
CASAAIRCRAm
CESSNA
CESSNA
CESSNA
PIPER
BOEING
BOEING
SHOKIS
BEECH
BOENG
BOEING
AEROSPATIALE
BOEING
BOEING
BOEING
BOEING
CANADAIR
CESSNA
IAI
CESSNA
CANADAIR
BOEING
BOEING
CESSNA
DEHAVILLAND
PAGE 16T
R767-3oOpOoER
l%767300/3OOER
sA22q3)MERLlNIuB
LEARJEr31
SWERKlNGAIR200
SUPER KINGAIR B200
SUPERKINGAIRB2(WIT/CC
CN-23!XOO
CITATIONlII(650)
560
ATR42-300
=F=
HAwKER2258ooxP
B-757-200
B-757-200
FALCON 2&F5
C90
ISLANDER BN-2B
C-212-DE
1708
3104
402c
PA-23-250
PA-28-236
B-757-200
B-757-200
A36BoNANzA
B-757-200
E757-200
ATM2320
B767-300/3OOER
B-767-300/3OOER
E767300/3OOER
E767300/3OOER
CHALLENGERCLUW
ClTATIONII(550)
1124 WElWIND
CTI’ATIONI
RJ (CL60@2B19)
E757-200
B-757-200
CITATIONULTRA (560)
DHC-8 314
“*TAKEOFF++
ENGINE TOGW
1000 LBS ESI’ DBA
Pw4056 295.00 68.9
Pw4056 295.00 68.9
wE331-1ou 1250 68.9
lTE731-23B 17.00 68.9
Pr6A-41 12.50 68.8
PT6A-41 12.50 68.8
PT6A-42 12.50 68.8
cm9c 3330 68.8
TFE7313B1oa 2150 68.8
JT1WA 15.90 68.7
PW12O/HS 14SF5 37.26 68.4
TFE7313A-2B 21.50 68.4
PT6AmR 27.10 68.3
TFE7315BR-1H 28.00 68.2
RB211-535E4 220.00 68.1
RB211-535E4 220.00 68.1
TFE731-5AR-2c 29.10 68.1
PT6A-21 9.70 68.0
o-540-E4c5 6.20 68.0
PT6AsB 16.98 68.0
c-1452H 2.20 68.0
10-47@VO 5.20 68.0
TsIo-52~VB 6.90 68.0
ICM4K4B5 5.20 68.0
O-540-J3ASD 3.00 68.0
PW2040 220.00 67.9
rW2040 220.00 67.9
PT6A-65R 26.40 67.9
10-550-B 3.65 67.8
RB211-535E4 220.00 67.8
RB211-535E4 220.00 67.8
PW121/H!S 14SF5 37.26 67.7
CF6-8OC2B6 288.70 67.6
cF6-8Oc2B6 288.70 67.6
CF6-8OC2B6F W/Nl MOD 288.70 67.6
CFMOCZB6F W/N1 MOD 288.70 67.6
ALF502L 41.25 67.5
In- 14.60 67.4
-13-1G 22.90 67.4
JIXD-1A 11.90 67.3
CF3MAl 53.00 67.2
RB211-535E4B 220.00 67.1
RB211-535E4B 220.00 67.1
In- 16.30 67.1
Pwl23 43.00 67.1
FLAPS
5
5
10
7
7
15
15
0
5
10
15
5
5
5
5
20
20
15
20
5
NOTES
8,15
8,15
5,ll
13,15
11
10,ll
5,ll
15
8,15
8,15
15
13
8,15
8,15,36
8,15,36 8,15,27
10
11
15
11
10,ll
11
11
11
8,15
8,15
8,15
11
8,15,35
8,15,35 15
8,15
8,15
8,15
8,15
15
8,15
8,15
15
15
8,153
8,15,36 8,15
8,lS
AC 36-36 APPENDIX 1
ESTIMATED MAXIMUM A-WEIGHTED SOUNDLEVELS MEASURED IN ACCORDANCE WITH PART-36 APPENDIX-C- PROCEDURES
MANUFACIURER
AERO6PATIALE
BEECH
BEECH
BEECH
CANADAIR
CESSNA
CESSNA
CESSNA
DEHAVILLAND
DEHAVILLAND
=Alw PIPER
CANADAIR
AERO6PATIALE
BOEING
BOEING
DEEUVILUND
AEROSPATIALE
BEECH
CANADAIR
AEROSPATIALE
CANADAIR
DEHAVILLAND
DEESAVILLAND
DORNIER
BEECH
BEECH
BEECH
BEECH
CESSNA
CESSNA
BEECH
CASA AIRCRAFT
CASA AIRCRAFT
DEEiAVUAND
mm
=mFT CESSNA
DEHAVILLAND
FOKKER
AIRPLANE
ATR72-210
58 (2BLD)
ES5 (2 BLD)
CHALLENGERCL-601
401
414A
500
DHC-6
DHC-6
=m= PA-28RT-201(2BLD)
PA-28RS201~3BLD)
CHALLENGERCL-6OO
ATR42320
B-757-200
B757-200
DHC-8 102
ATR42300
1900/19OOC
CHALlENGERCL6O1
ATR72-210
CHAILENGERCL6O1
DHC-8 106
DHC-8 201/202
DoRNIER228
B2OO/T/a/C,C-12(4 BLD)
58P
99A
185F
340A
6908
MU-2B36A
PA-60-600
PAdO2P
65QUEENAIR
c-212-a
c-212-m
DHC-8 l@
LEARJEr35W/cENTuRYm
LEARp36w/CENTURYIII
ClTATIONVII(650)
DHC-8 311
F70
“‘TAKEOFF++
ENGINE TOGW
1000 LBS EST DBA
PWW/HS 247F 48.50 67.0
1&52o-c 5.40 67.0
lsn520-WB 6.20 67.0
Io-52o-c 530 67.0
CF34-1A 45.10 67.0
TSIO52tLE 630 67.0
TSI0-520-N 6.80 67.0
JTISD-1 10.90 67.0
Pr6A-27 12.50 67.0
Pr6A-27 1250 67.0
TFE7313B 20.50 67.0
1036KlC6 2.80 67.0
lsm36o-FB 2.90 67.0
ALF502L 40.40 66.9
PWl2l/HS 14SF5 35.60 66.7
RB211-535E4B 220.00 66.7
RB211-535E4B 220.00 66.7
PWl20 34.50 66.7
PWl2O/HS 14SF5 34.72 665
l?r6A-65B 16.60 663
CF3&3A/ Al/A2 45.10 665
PW127/HS 247F 47.40 66.4
CF34-1A 43.10 66.4
Pwl21 3630 66.4
mm3 3630 66.4
TPEa1-5252D 13.10 66.3
PT6A-42 12.50 66.1
Tsm52oWB 6.20 66.0
PT6A-27 10.40 66.0
IGSb540-AID 8.80 66.0
10-520-D 3.40 66.0
TsIo-52OMB 6.00 66.0
IPE-331~251K 10.30 66.0
TPE-331~252M 11.00 66.0
Io-54OxlJ5 550 66.0
10540-AAlA 6.00 66.0
IGSO480-AlB6 7.70 65.9
TPE 331-i0/10R501c/511 16.98 65.7
TPE 331~lOR5OlC/511C 16.98 65.7
PWl21 3450 65.7
TFEm-2 17.00 65.6
TFE731-2 17.00 65.6
TFE7314RS 22.45 65.4
Pwl23 43.00 65.4
RR TAY MK620=15 81.00 65.4
FLAPS
15
20
15 -
20
15
15
20
15
-
NOTES
8,lS
11
10,ll
11
15
11
11
15
4
4
15
11
11
12
15
811535
8,15,35 15
15
10
15
8,lS
15
15
15
10,ll
4
11
11
11
10
4
11
11
11
15
15
15
8,15
8,15
8,lS
8,15
8,15
PAGE 17T
AC 36-36 APPENDIX 1
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS MEASURED IN ACCORDANCE WITH PART-36 APPENDIX-C- PROCEDURES
MANUFA-ER
SAAB FAIRCHILD
BEECH
-m BEECH
BELLANCA
CESSNA
CESSNA
MOONEY
CESSNA
GULFSEWM
CESSNA
MOONEY
BEECH
CASA AIRCRAFT
CASA AIRCRAFT
CASA AIRCRAFT
GULEIEAM
SAAB
SAAB
DASSAULT
GULFSRUM
MrIsuBIsHI
PIPER
PIPER
MOONEY
AEROSPATIALE
SAAB
SAAB
SAAB
EMBRAER
MAW
BEECH
BEECH
BEECH
BEECH
BNA
CESSNA
CESSNA
PIPER
SAAB
CANADAIR
AIRPLANE
“**TAKEOFF’**
ENGINE TOGW
1000 LBS EST’ DBA
SF340 GE CI7-5A2 2730 653
58/58A BARON (3 BLD) 10550-C 550 65.1
LEARJET 35A/36A TFE731-2 18.30 65.1
A24R 10360-AlB6 2.80 65.0
173OA 10540-T4B5D 330 65.0
177RG 1&36@Allk 2.80 ’ 65.0
310R ‘IXO-52(FBB .5al 65.0
Imoc O-360-AlD 2.60 65.0
PA-24260 10540-BlA5 3.20 65.0
CARAVAN1 PT6A-114 730 64.9
G-IV-SP RRTAY 611-8 74.60 64.9
s550 0 JTl5D4B 15.10 64.8
MZOM ‘HO-540-AFlA 337 64.8
300/3OOCKlNGAJR M’6A-6OA 14.00 64.7
c-212-a TPE 331-lOR312C/502C 16.98 64.7
c-212-a TPE 331-lOR-512C/502C . 16.98 64.7
C-212-DF TPE 331-lOR502C/512C/5 16.98 64.7
G-IV RR TAY 611-8 73.20 64.2
SF34OB (HSXRF-19 props) GE CT%9B 29.00 64.2
SF34oB @ow!Y P’W) GE CT7-9B 29.00 64.1
FALCON 2000 CFE73&1-1B 36.50 64.0
680FL IGSO-5WBlA 8.50 64.0
MU-2B-26A TPE-331~5-252M 10.00 64.0
PA34-200T TSIO-360-E 4.80 64.0
PA34ZUT TSIO-36OXB 4.75 64.0
M2OM lW540-AFlA 3.20 63.9
SN601 CORVEPI’E mm 13.90 63.8
-31 TPE331-lOU-501H 15.20 63.7
2000 AE21OOA 49.60 63.5
SF34OB (HS14RF-19 props) GE C’l7-9B 2850 63.5
sF3m @owty Pq=) GE CI7-9B 2850 63.4
EMB-120 BRASILIA Pwll5 21.20 63.2
Mx7-235 0540-JIA5D 250 63.2
58 (3BLD) 10-520-C 5.40 63.0
B60 TIosQl-ElC4 6.80 63.0
c24R 10360-AlB6 2.80 63.0
E55 (3BLD) 10-520-C 530 63.0
172N 032OH2AD 230 63.0
CONQUEST1 PT6A-112 8.20 63.0
CONQUESNI TPE331-8 9.80 63.0
112 10360-cm6 2.70 63.0
GA-7 O-320-DlD 3.80 63.0
PA-2&200 1O36w1c 2.70 63.0
SF34oA @owty P’OPS) GEcI7-5A2 28.00 62.9
RJ (CL60@2B19) CF343Al 4750 62.7
15
8
10
20
7
10
10
10
10
15
15
20
m
15
15
15
15
15
m
8,15
8,15
11,21
15
15
8,15
8,15
8,15
11
4
11
11
11,21
4
15
8,15
8,15
8,15
12
11
11
10,ll
11
11
10
10,ll
5,ll
11
4
15 8,15
20 15
NOTES
PAGE 18T
AC 36-3G APPENDIX 1
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS MEASURED IN ACCORDANCE WITH PART-36 APPENDIX -C- PROCEDURES
MANUFA-ER
SAAB
CESSNA
BEECH
BEECH
BEECH
CESSNA
-A
CESSNA
BELLANCA
BELLANCA
AIRPLANE
SF34oA @owty props) CII’ATIONII(550)
76
Al00
FWCINGAIR
695
695 COMMANDER 980
PA31T
PA*180
PAd&lm2BLD)
690D COMMANDER 900
695ACOMMANDER 1000
BloO KINGAIR
69occoMMANDER84o
172
404
421C
‘LEARJElr@ CITATIONJET (525)
AA-SA
PA-28-140
PA-%151
PA-28-181
PAdHm3BLD)
C23
560E
PA-28-161
A-23
D95ATRAVELAIR
moJ WACO CLASSIC F-5
AA-SBTEER
AA-IB
cmYENNE4ooLs
77
150
PA40 TWIN COMANCHE PA-38412 15oM 152 PA-18450 7GCAA
+++TAKEOFF”“+
ENGINE TOGW
loo0 CBS EST DBA
GE CI7-5A2 27.27 62.7
v* 13BO 62.6
1036bAlG6D 3.90 62.0
PT6A-28 1150 62.0
P’I6A-135 10.90 62.0
TPE331-10 1030 62.0
TPE331:10 1030 62.0
Fr6A-28 9.00 62.0
036&ElA6D 3.80 62.0
‘I036@ElA6D 3.90 62.0
TPE331-5 10.70 61.7
TPE331-10 11.20 61.6
TPE331-6 11.80 61.5
TPE331-5 1030 61.3
032OX2D 2.30 61.0
GTSIo-52~M 8.40 61.0
GTsIo=520-L 7.50 61.0
PVV305A 23.10 60.9
FJ44-1A 10.40 60.3
032~E2G 2.20 60.0
0-32~E3D 2.20 60.0
032M3D 2.20 60.0
0360-A4M 2.55 60.0
IO360-ElA6D 3.90 60.0
036O-A4K 2.50 59.0
GO48O-ClB6 6.50 59.0
032OmG 2.40 59.0
10360-A 2.40 58.0
1032@BlB 4.20 58.0
0360-C2E 2.20 58.0
IO-36O-AlB6D 2.70 58.0
R-755-B2 2.70. 57.8
0360-A4K 2.20 57.4
o-235 1.60 57.1
TPE331-14 12.05 57.0
O-235L2C 1.70 56.0
0-20&A ’ 1.60 56.0
10320-B 3.60 56.0
o-235-L2C 1.70 56.0
02WA 1.60 55.0
O-2354X 1.70 55.0
O-320-A2B 1.80 53.0
0=32&A2B 1.70 51.0
NOTES
8,lS
15
11
4
5,ll
5,15
5,ll
4
11
11
10
5,ll
11
5,ll
11
11
11
8,lS
8,15
11
11
11
11
11
11
11
11
11
11
11
4
11
10,ll
11
11
11
11
11
11
11
11
11 4
PAGE 19T
