APPENDIX 6 MODEL
MANUFACTURER
AEROSPATIALE ATR42-200 MTOW MLW 1000#
34.70
34.20
MFR, MODEL
ENGINE DATA SHPNO.
AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN
AIRPLANES IN THE TRANSPORT CATEGORY
RPM MFR, MODEL
PROPELLER BLADESDIAM (IN) PITCH PW 120 2 2000 1200 HAMILTON STD 14SF-1 156 4 V
PRATT&WHITNEY TO AP FLAPS 15 30
TO SL AP STAGE NOISE LEVEL (EPNdB)
82.1 83.8 96.8 3 NOTES
AEROSPATIALE ATR42-300
35.60
35.30 PW 120 PRATT&WHITNEY 2 2000 1200 HAMILTON STD 14SF-5 156 4 V 15 30 82.6 83.8 96.8 3
AEROSPATIALE ATR42-300
37.30
36.20 PW 120 PRATT&WHITNEY 2 2000 1200 HAMILTON STD 14SF-5 156 4 V 15 30 83.3 83.7 96.7 3
AEROSPATIALE ATR42-320
35.60
35.30 PW 121 PRATT&WHITNEY 2 2100 1200 HAMILTON STD 14SF-5 156 4 V 15 30 82.2 83.9 96.8 3
AEROSPATIALE ATR42-320
37.30
36.20 PW 121 PRATT&WHITNEY 2 2100 1200 HAMILTON STD 14SF-5 156 4 V 15 30 83.0 83.9 96.7 3
AEROSPATIALE ATR42-400
39.50
38.80 PW 121A PRATT&WHITNEY 2 2200 1200 HAMILTON STD 568F 155 6 V 15 35 77.2 80.9 93.1 3
AEROSPATIALE ATR42-400
40.10
39.50 PW 121A PRATT&WHITNEY 2 2200 1200 HAMILTON STD 568F 155 6 V 15 35 77.6 80.9 93.0 3
AEROSPATIALE ATR42-500
41.00
40.30 PW 127E PRATT&WHITNEY 2 2400 1200 HAMILTON STD 568F 155 6 V 15 35 76.6 80.7 92.4 3
AEROSPATIALE ATR42-500
44.05
42.95 PW 127E PRATT&WHITNEY 2 2400 1200 HAMILTON STD 568F 155 6 V 15 35 78.5 80.7 92.2 3
AEROSPATIALE ATR72-100
44.10
43.90 PW 124 PRATT&WHITNEY 2 2400 1200 HAMILTON STD 14SF11 156 4 V 15 30 85.2 84.8 94.1 3
AEROSPATIALE ATR72-200
48.50
47.10 PW 124 PRATT&WHITNEY 2 2400 1200 HAMILTON STD 14SF11 156 4 V 15 30 86.9 84.7 91.1 3
AEROSPATIALE ATR72-200
47.40
47.10 PW 124 PRATT&WHITNEY 2 2400 1200 HAMILTON STD 14SF11 156 4 V 15 30 86.5 84.7 94.1 3
AEROSPATIALE ATR72-210
47.40
47.10 PW 127 PRATT&WHITNEY 2 2450 1200 HAMILTON STD 247F 156 4 V 15 33 80.2 84.8 92.7 3
AEROSPATIALE ATR72-210
47.40
47.10 PW 127 PRATT&WHITNEY 2 2450 1200 HAMILTON STD 14SF11 156 4 V 15 33 86.1 86.1 94.2 3 Page 1
APPENDIX 6 MODEL
MANUFACTURER
AEROSPATIALE ATR72-210 MTOW MLW 1000#
48.50
48.20
MFR, MODEL
ENGINE DATA SHPNO.
AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN
AIRPLANES IN THE TRANSPORT CATEGORY
RPM MFR, MODEL
PROPELLER BLADESDIAM (IN) PITCH PW 127 2 2450 1200 HAMILTON STD 14SF11 156 4 V
PRATT&WHITNEY TO AP FLAPS 15 33
TO SL AP STAGE NOISE LEVEL (EPNdB)
86.5 86.0 94.2 3 NOTES
AEROSPATIALE ATR72-210
50.66
49.56 PW127 PRATT&WHITNEY 2 1200 HAMILTON STD.
247F 156 4 V 15 33 82.2 84.7 92.4 3 BAE SYSTEMS (BAe) 748-2A
44.50
43.00 DART 532-2 ROLLS-ROYCE 2 2470 1394 DOWTY ROTOL CR212/4-30-4/22 144 4 V 15 28 92.5 96.8 103.8 2 BAE SYSTEMS (BAe) 748-2B
46.00
43.00 DART 535-2 ROLLS ROYCE 2 2470 1394 DOWTY ROTOL CR212/4-30-4/22 144 4 V 15 28 92.5 96.8 103.4 2 BAE SYSTEMS (BAe) 748-2B
46.00
43.00 DART 536-2 ROLLS ROYCE 2 2470 1394 DOWTY ROTOL CR212/4-30-4/22 144 4 V 8 28 88.7 93.3 92.8 3 1 BAE SYSTEMS (BAe) ATP
50.55
49.05 PW124A PRATT&WHITNEY 2 2160 1200 HAMILTON STD.
6/5500/F 165 6 V 7 22 80.7 82.1 96.5 3 BAE SYSTEMS (BAe) ATP
50.55
49.05 PW126A PRATT&WHITNEY 2 2396 1200 HAMILTON STANDARD 6/5500/F 165 6 V 7 20 79.5 82.7 97.0 3 BAE SYSTEMS (BAe) ATP
50.55
49.05 PW126A PRATT&WHITNEY 2 2396 1200 HAMILTON STD.
6/5500/F.1 165 6 V 7 15 79.5 82.7 97.9 3
BAE SYSTEMS (JETSTREAM) JETSTREAM 4100
23.00
22.30 TPE-331-14G(H)R-801 ALLIEDSIGNAL 2 1500 1552 MCCAULEY B/C5JFR36C1101/2L114G 114 5 V 9 15 85.8 83.5 87.8 3 *
BAE SYSTEMS (JETSTREAM) JETSTREAM 4100
24.00
23.30 TPE-331-14G(H)R-801 ALLIEDSIGNAL 2 1500 1552 MCCAULEY B/C5JFR36C1101/2L114G 114 5 V 9 15 86.4 83.4 87.8 3 *
BAE SYSTEMS (JETSTREAM) JETSTREAM 4100
24.00
23.30 TPE-331-14G(H)R-805 ALLIEDSIGNAL 2 1650 1552 MCCAULEY B/C5JFR36C1103/4L114H 114 5 V 9 15 86.5 84.3 87.8 3 *
BAE SYSTEMS (JETSTREAM) JETSTREAM 4100
24.00
23.30 TPE-331-14G(H)R-901 ALLIEDSIGNAL 2 1650 1552 MCCAULEY B/C5JFR36C1103/4L114H 114 5 V 9 15 86.7 84.3 87.9 3 *
BOMBARDIER DHC-7-101
43.00
41.01 PT6A-50 PRATT&WHITNEY 4 1017 1210 HAMILTON STD.
24PF-305 135 4 V 25 25 80.1 83.3 91.6 3 *
BOMBARDIER DHC-7-103
44.00
42.00 PT6A-50 PRATT&WHITNEY 4 1120 1210 HAMILTON STD.
24PF-305 135 4 V 25 25 80.5 84.0 91.4 3 * Page 2
APPENDIX 6 MODEL
MANUFACTURER
BOMBARDIER DHC-8 MTOW MLW 1000#
33.00
32.40
MFR, MODEL
ENGINE DATA SHPNO.
AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN
AIRPLANES IN THE TRANSPORT CATEGORY
RPM MFR, MODEL
PROPELLER BLADESDIAM (IN) PITCH PW 120 2 1800 HAMILTON STD.
14SF-1 156 4 V
PRATT&WHITNEY TO AP FLAPS 15 35
TO SL AP STAGE NOISE LEVEL (EPNdB)
80.7 86.3 95.1 3 NOTES
BOMBARDIER DHC-8-102
34.50
33.90 PW 120 PRATT&WHITNEY 2 1800 1150 HAMILTON STD 14SF-7 156 4 V 15 35 80.8 86.3 90.7 3
BOMBARDIER DHC-8-102
34.50
33.90 PW 120 PRATT&WHITNEY 2 1800 1200 HAMILTON STD 14SF-7 156 4 V 15 35 80.8 86.3 94.8 3
BOMBARDIER DHC-8-103
34.50
33.90 PW 121 PRATT&WHITNEY 2 1945 1150 HAMILTON STD 14SF-7 156 4 V 15 35 79.8 85.3 90.7 3
BOMBARDIER DHC-8-103
34.50
33.90 PW 121 PRATT&WHITNEY 2 1945 1200 HAMILTON STD 14SF-7 156 4 V 15 35 79.8 86.1 94.8 3
BOMBARDIER DHC-8-103
34.50
33.90 PW 121 PRATT&WHITNEY 2 1945 1100 HAMILTON STD 14SF-7 156 4 V 15 35 77.8 82.9 91.0 3
BOMBARDIER DHC-8-106
36.30
33.90 PW 121 PRATT&WHITNEY 2 1945 1100 HAMILTON STD 14SF-7 156 4 V 15 35 79.9 84.0 94.8 3
BOMBARDIER DHC-8-106
36.30
33.90 PW 121 PRATT&WHITNEY 2 1945 1200 HAMILTON STD 14SF-7 156 4 V 15 35 80.5 85.6 94.8 3
BOMBARDIER DHC-8-201
36.30
33.90 PW 123 PRATT&WHITNEY 2 1945 1100 HAMILTON STD 14SF-7 156 4 V 15 35 79.9 84.0 94.8 3
BOMBARDIER DHC-8-201
36.30
33.90 PW 123 PRATT&WHITNEY 2 1945 1200 HAMILTON STD 14SF-7 156 4 V 15 35 80.5 85.6 94.8 3
BOMBARDIER DHC-8-202
36.30
33.90 PW 123 PRATT&WHITNEY 2 1945 1100 HAMILTON STD 14SF-7 156 4 V 15 35 79.9 84.0 94.8 3
BOMBARDIER DHC-8-202
36.30
33.90 PW 123 PRATT&WHITNEY 2 1945 1200 HAMILTON STD 14SF-7 156 4 V 15 35 80.5 85.6 94.8 3
BOMBARDIER DHC-8-300
41.10
40.00 PW123 PRATT&WHITNEY 2 1200 HAMILTON STD.
14SF-15 156 4 V 5 15 84.3 87.4 98.9 3
BOMBARDIER DHC-8-311
41.10
40.00 PW123 PRATT&WHITNEY 2 2142 HAMILTON STANDARD 14SF-15 156 4 V 5 35 79.5 87.0 93.3 3 Page 3
APPENDIX 6 MODEL
MANUFACTURER
BOMBARDIER DHC-8-311 MTOW MLW 1000#
43.00
42.00
MFR, MODEL
ENGINE DATA SHPNO.
AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN
AIRPLANES IN THE TRANSPORT CATEGORY
RPM MFR, MODEL
PROPELLER BLADESDIAM (IN) PITCH PW 123 2 2142 1200 HAMILTON STD 14SF-15 156 4 V
PRATT&WHITNEY TO AP FLAPS 5 35
TO SL AP STAGE NOISE LEVEL (EPNdB)
80.0 86.8 93.3 3 NOTES
BOMBARDIER DHC-8-314
41.10
40.00 PW123 PRATT&WHITNEY 2 2249 1200 HAMILTON STANDARD 14SF-15 156 4 V 5 35 79.9 87.3 93.3 3
BOMBARDIER DHC-8-314
41.10
40.00 PW123 PRATT&WHITNEY 2 2249 1100 HAMILTON STANDARD 14SF-15 156 4 V 5 35 80.7 84.7 93.3 3
BOMBARDIER DHC-8-314
43.00
42.00 PW123 PRATT&WHITNEY 2 2249 1200 HAMILTON STANDARD 14SF-15 156 4 V 5 35 80.7 87.2 93.3 3
BOMBARDIER DHC-8-314
43.00
42.00 PW123 PRATT&WHITNEY 2 2249 1100 HAMILTON STANDARD 14SF-15 156 4 V 5 35 81.7 84.6 93.2 3
BOMBARDIER DHC-8-315
41.10
40.00 PW123E PRATT&WHITNEY 2 2142 1200 HAMILTON STANDARD 14SF-15 156 4 V 5 35 79.5 87.0 93.3 3
BOMBARDIER DHC-8-315
43.00
42.00 PW123E PRATT&WHITNEY 2 2142 1200 HAMILTON STANDARD 14SF-15 156 4 V 5 35 80.0 86.9 93.3 3
BOMBARDIER DHC-8-400 (Q400)
61.70
60.50 PWC 150A PRATT&WHITNEY 2 5070 1020 DOWTY R408/6-123-F/17 162 6 V 5 15 77.1 84.1 94.9 3
BOMBARDIER DHC-8-400 (Q400)
61.70
60.50 PWC 150A PRATT&WHITNEY 2 5070 1020 DOWTY R408/6-123-F/17 162 6 V 5 35 77.1 84.1 93.0 3 3
BOMBARDIER DHC-8-400 (Q400)
65.20
62.00 PWC 150A PRATT&WHITNEY 2 5070 1020 DOWTY R408/6-123-F/17 162 6 V 5 35 78.6 84.0 93.1 3 3
BOMBARDIER DHC-8-400 (Q400)
65.20
62.00 PWC 150A PRATT&WHITNEY 2 5070 1020 DOWTY R408/6-123-F/17 162 6 V 5 15 78.6 84.0 94.8 3
BOMBARDIER DHC-8-401 (Q400)
61.70
60.50 PWC 150A PRATT&WHITNEY 2 5070 1020 DOWTY R408/6-123-F/17 162 6 V 5 35 77.1 84.1 93.0 3 3
BOMBARDIER DHC-8-401 (Q400)
61.70
60.50 PWC 150A PRATT&WHITNEY 2 5070 1020 DOWTY R408/6-123-F/17 162 6 V 5 15 77.1 84.1 94.9 3
BOMBARDIER DHC-8-401 (Q400)
65.20
62.00 PWC 150A PRATT&WHITNEY 2 5070 1020 DOWTY R408/6-123-F/17 162 6 V 5 15 78.6 84.0 94.8 3 Page 4
APPENDIX 6 MODEL
MANUFACTURER
BOMBARDIER DHC-8-401 (Q400) MTOW MLW 1000#
65.20
62.00
MFR, MODEL
ENGINE DATA SHPNO.
AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN
AIRPLANES IN THE TRANSPORT CATEGORY
RPM MFR, MODEL
PROPELLER BLADESDIAM (IN) PITCH PWC 150A 2 5070 1020 DOWTY R408/6-123-F/17 162 6 V
PRATT&WHITNEY TO AP FLAPS 5 35
TO SL AP STAGE NOISE LEVEL (EPNdB)
78.6 84.0 93.1 3 NOTES 3
BOMBARDIER DHC-8-402 (Q400)
61.70
60.50 PWC 150A PRATT&WHITNEY 2 5070 1020 DOWTY R408/6-123-F/17 162 6 V 5 15 77.1 84.1 94.9 3
BOMBARDIER DHC-8-402 (Q400)
61.70
60.50 PWC 150A PRATT&WHITNEY 2 5070 1020 DOWTY R408/6-123-F/17 162 6 V 5 35 77.1 84.1 93.0 3 3
BOMBARDIER DHC-8-402 (Q400)
65.20
62.00 PWC 150A PRATT&WHITNEY 2 5070 1020 DOWTY R408/6-123-F/17 162 6 V 5 35 78.6 84.0 93.1 3 3
BOMBARDIER DHC-8-402 (Q400)
65.20
62.00 PWC 150A PRATT&WHITNEY 2 5070 1020 DOWTY R408/6-123-F/17 162 6 V 5 15 78.6 84.0 94.8 3 CASA C-212-CB
14.33
13.80 TPE 331-5-251C ALLIEDSIGNAL 2 750 1591 HARTZELL HC-B4TN-5CL/LT10282H 107 4 V 10 20 87.3 84.0 91.2 3 * CASA C-212-CC
16.98
16.42 TPE 331-10/10R-501C/ ALLIEDSIGNAL 2 900 1591 HARTZELL HC-B4MN-5AL 110 4 V 10 15 85.9 85.1 90.9 3 * CASA C-212-CD/CE
16.98
16.42 TPE331-10R-502C/512 ALLIEDSIGNAL 2 900 1591 DOWTY-ROTOL (C)R.334/4-82-F/13 110 4 V 10 40 82.9 83.0 93.2 3 * CASA C-212-CF
16.98
16.42 TPE 331-10R-501C/511 ALLIEDSIGNAL 2 900 1591 HARTZELL HC-B4MN-5AL 110 4 V 10 15 85.9 85.1 90.9 3 * CASA C-212-DE
16.98
16.42 PT6A-65B PRATT&WHITNEY 2 1000 1700 MCCAULEY 4HFR34C756 106 4 V 10 40 84.1 84.7 88.0 3 * CASA C-212-DF
16.98
16.42 TPE331-10R-502C/512 ALLIEDSIGNAL 2 900 1591 DOWTY-ROTOL (C)R.334/4-82-F/13 110 4 V 10 40 82.9 83.0 93.2 3 * CASA C-295
46.30
45.63 PW127-G PRATT&WHITNEY 2 2645 1200 HAMILTON STANDARD HS E568F 155 6 V 10 15 87.1 88.2 93.9 3 * CASA CN-235
31.75
31.30 CT7-7A GENERAL ELECTRIC 2 1700 1384 HAMILTON STD.
14RF-21 132 4 V 8 23 84.5 86.5 87.2 3 * CASA CN-235-100
31.75
31.30 CT7-9C GENERAL ELECTRIC 2 1750 1384 HAMILTON STANDARD 14RF-21 132 4 V 10 23 84.8 86.7 87.2 3 * Page 5
APPENDIX 6 MODEL
MANUFACTURER CASA CN-235-100 MTOW MLW 1000#
33.29
32.85
MFR, MODEL
ENGINE DATA SHPNO.
AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN
AIRPLANES IN THE TRANSPORT CATEGORY
RPM MFR, MODEL
PROPELLER BLADESDIAM (IN) PITCH CT7-9C 2 1750 1384 HAMILTON STANDARD 14RF-21 132 4 V
GENERAL ELECTRIC TO AP FLAPS 10 23
TO SL AP STAGE NOISE LEVEL (EPNdB)
85.3 87.8 87.2 3 NOTES * CASA CN-235-200
34.83
34.39 CT7-9C GENERAL ELECTRIC 2 1750 1384 HAMILTON STANDARD 14RF-21 132 4 V 10 23 80.5 87.4 92.4 3 * CASA CN-235-300
34.83
34.39 CT7-9C3 GENERAL ELECTRIC 2 1750 1384 HAMILTON STANDARD 14RF-37 144 4 V 10 15 85.0 87.8 93.3 3 *
CONVAIR 580 (Aeroprod.)
58.16
52.00 501-D13H ALLISON 2 3460 1020 AEROPRODUCTS A6441FN-606A 162 4 V 10 28 87.4 91.1 98.3 3
DORNIER 328-100/MOD 10
30.84
29.17 PW119B PRATT&WHITNEY 2 2180 1300 HARTZELL HD-E6C-3B 142 6 V 12 12 82.1 83.8 94.8 3 2,*
DORNIER 328-100/MOD 20
30.84
29.17 PW119C PRATT&WHITNEY 2 2180 1300 HARTZELL HD-E6C-3B 142 6 V 12 12 82.7 83.8 94.8 3 2,*
DORNIER 328-100/MOD 30
30.84
29.17 PW119C PRATT&WHITNEY 2 2180 1300 HARTZELL HD-E6C-3B 142 6 V 12 12 82.7 83.8 94.8 3 2,*
EMBRAER EMB-120
21.17
21.17 PW 115 PRATT&WHITNEY 2 1500 HAMILTON STD.
14RF-9 126 4 V 15 25 76.6 81.6 92.5 3
EMBRAER EMB-120
25.40
24.80 PW118 PRATT&WHITNEY 2 HAMILTON STD.
14RF-9 126 4 V 15 25 81.2 83.5 92.3 3 * FOKKER 50
45.86
41.83 125B PRATT&WHITNEY 2 V 8 26 81.0 85.0 96.8 3 FOKKER F27 MK500
45.00
42.00 DART 7/MK535-7R ROLLS ROYCE 2 DOWTY ROTOL R193-4-30-4 138 4 V 0 40 90.6 92.2 100.3 2 FOKKER F27 MK500
45.00
43.50 DART 7/MK535-7 ROLLS ROYCE 2 DOWTY ROTOL R193-4-30-4 138 4 V 0 40 86.9 90.1 94.3 3 1 FOKKER F27 MK500
45.00
43.50 DART 7/MK535-7R ROLLS ROYCE 2 DOWTY ROTOL R193-4-30-4 138 4 V 0 40 87.4 89.8 94.3 3 1 FOKKER F27 MK500
45.90
43.50 DART 7/MK551-7R ROLLS ROYCE 2 DOWTY ROTOL R193-4-30-4 138 4 V 0 40 87.6 89.8 94.3 3 1 Page 6
APPENDIX 6 MODEL
MANUFACTURER FOKKER F27 MK500/600 MTOW MLW 1000#
45.00
41.00
MFR, MODEL
ENGINE DATA SHPNO.
AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN
AIRPLANES IN THE TRANSPORT CATEGORY
RPM MFR, MODEL
PROPELLER BLADESDIAM (IN) PITCH DART 7/MK552-7R 2 2307 DOWTY ROTOL R193-4-30-4 138 4 V
ROLLS ROYCE TO AP FLAPS 0 40
TO SL AP STAGE NOISE LEVEL (EPNdB)
87.4 89.8 94.1 3 NOTES 1 FOKKER F27 MK500/600
45.90
43.50 DART 7/MK552-7R ROLLS ROYCE 2 2307 DOWTY ROTOL R193-4-30-4 138 4 V 0 40 87.6 89.8 94.3 3 1 FOKKER F27 MK600
45.00
42.00 DART7 MK532-7R ROLLS ROYCE 2 DOWTY ROTOL R193-4-30-4 138 4 V 0 40 90.6 92.2 100.3 2
LOCKHEED L382G
155.00
135.00 501-D22A ALLISON 4 4050 1020 HAMILTON STD.
54H60 162 4 V 18 35 94.8 96.7 98.1 3 *
MCDONNELL DOUGLAS DC3C (BTC STC)
28.75
28.75 PT6A-67R PRATT&WHITNEY 2 HARTZELL HC-B5MA-3/M11276 115 5 V 0 45 82.4 84.4 91.9 3 SAAB 2000(w/PECS mod)
50.20
48.50 AE2100A ALLISON 2 DOWTY ROTOL R381/6-123-F/5 15 35 78.4 87.5 87.9 3 SAAB 340B
28.50
28.00 CT7-9B GENERAL ELECTRIC 2 1384 DOWTY ROTOL R354/4-123-F/13/20 132 4 V 15 20 78.0 85.9 91.6 3 SAAB 340B
28.50
28.00 CT7-9B GENERAL ELECTRIC 2 1384 HAMILTON STD.
14RF-19 132 4 V 15 20 77.7 86.1 90.1 3 SAAB 340B
28.50
28.00 CT7-9B GENERAL ELECTRIC 2 1384 DOWTY ROTOL R375/4-123-F/21 132 4 V 15 20 78.0 85.9 91.6 3 SAAB SF340A
28.00
27.20 CT7-5A2 GENERAL ELECTRIC 2 1384 DOWTY ROTOL R375/4-123-F/21 132 4 V 15 20 78.2 85.8 84.4 3 SAAB SF340A
28.00
27.20 CT7-5A2 GENERAL ELECTRIC 2 1384 DOWTY ROTOL R354/4-123-F/13/20 132 4 V 15 20 78.2 85.8 84.4 3
SAAB FAIRCHILD 340
27.00
26.50 CT7-5A GENERAL ELECTRIC 2 1210 DOWTY ROTOL R320/4-123-F/1 126 4 V 15 35 79.3 87.6 89.6 3
SAAB FAIRCHILD 340
27.00
26.50 CT7-7E GENERAL ELECTRIC 2 1210 DOWTY ROTOL R320/4-123-F/1 126 4 V 15 35 79.5 87.4 89.6 3
SAAB-SCANIA 340A W/APU
27.28
26.50 CT7-5A2 GENERAL ELECTRIC 2 1735 DOWTY ROTOL R354/4-123-F13 132 4 V 35 77.5 86.2 86.3 3 Page 7
APPENDIX 6 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN
AIRPLANES IN THE TRANSPORT CATEGORY MTOW MODEL
MANUFACTURER MLW 1000# MFR, MODEL
ENGINE DATA NO. SHP RPM MFR, MODEL
PROPELLER DIAM (IN) BLADES
PITCH TO AP FLAPS
TO SL AP STAGE NOISE LEVEL (EPNdB) NOTES SHORT BROS. 22.00 PRATT&WHITNEY 2 1120 1675 HARTZELL 111 5 8 35 88.5 83.9 92.8 3 * SD3-30 21.61 PT6A-45 HC-35MP-34/M10282B-6 V SHORT BROS. 26.00 PRATT&WHITNEY 2 1327 HARTZELL 111 5 5 30 84.4 83.7 89.9 3 ** SD3-60 25.70 PT6A-65R HC-B5MP-3C/M10876K V SHORT BROS. 27.10 PRATT&WHITNEY 2 1700 HARTZELL 108 6 15 15 80.0 82.7 94.3 3 SD3-60-300 25.70 PT6A-67R HC-A6A-3/A1046E V Page 8
11/15/01 AC36-1H Appendix 6 Appendix 6 Notes 1 Equipped With Standard Hushkit
2. APU On For Approach
3. Mod Sup 39; Propeller RPM limited to 850 for approach.
* Full Thrust Takeoff ** 650 Meter Sideline See Appendix 1 For Charts And Equations For The Calculation Of Noise Certification Limits Page 9
APPENDIX 7 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CFR PART 36, APPENDIX F) MANUFACTURER MTOW ENGINE DATA PROPELLER DATA NOISE LEVEL (dBA)
MODEL MLW (1000#) MFR, MODEL NO. SHP EXH MFR, MODEL DIAM (IN) BLADES PITCH RPM MdBA PC CdBA NOTES AEROTECH/AUST. 9.10 ALLISON 2 HARTZELL 91 3 2071 78.00 -2.10 75.9 N22S 250-B17E HC-A3VF-7B/V10133N ANDERSON GREEN 3.15 AVCO LYCOMING 1 250 3 HARTZELL 77 2 2575 75.20 -1.50 73.7 WOOD 51 3.15 O-540-A4D5 HC-E2YR-1S/8465-7R V BEECH 12.50 PRATT&WHITNEY 2 847 1 HARTZELL 98 3 2000 82.80 -3.60 79.2
(200) 12.50 PT6A-41 HC-B3TN-3G/T10178H V BEECH 16.60 PRATT&WHITNEY 2 1100 2 HARTZELL 110 4 1700 80.50 3.00 77.4 1 1900/1900C 16.10 PT6A-65B HCB4MP-3A/M10877K V BEECH 14.40 PRATT & WHITNEY 2 1200 McCAULEY 104 5 1700 84.28 -5.47 79.3 2000 XPT6A-67 D-L104DSZ-O V BEECH 5.50 TCM 2 300 MCCAULEY 77 3 80.65 -3.26 77.4 58/58A 5.40 IO-550-C 3AF32C512/82-NEA-5 V BEECH 3.60 TELEDYNE 1 260 5 MCCAULEY 80 3 2700 78.80 -0.60 78.2 A36 3.60 I0-520-B 3A32C760/82 NB-2 V BEECH 3.60 TELEDYNE 1 228 5 MCCAULEY 84 2 2550 78.00 -0.60 77.4 A36 3.60 I0-520-N 2A36C23/84B-0 V BEECH 3.65 TCM 1 300 MCCAULEY 80 3 78.24 -1.57 76.7 A36 3.65 IO-550-B 3A32C406/82NDB-2 V BEECH 3.65 TELEDYNE 1 300 5 MCCAULEY 80 3 2700 79.50 -0.30 79.2 A36TC 3.65 TSI0-520-U 3A32C760/82 NB-2 V BEECH 11.80 AIRESEARCH 2 715 1 HARTZELL 90 4 2000 80.20 -2.90 77.3 B100 11.20 TPE331-6-252B HC-B4TN-5C/T10173F V BEECH 12.50 PRATT&WHITNEY 2 845 1 HARTZELL 99 3 1996 82.80 -3.60 79.2 B200 12.50 PT6A-41 HC-B3TN-3G/T10178H V BEECH 12.50 PRATT&WHITNEY 2 850 1 HARTZELL 98 3 2000 82.80 -3.60 79.2 B200/B200C 12.50 PT6A-42 HC-B3TN-3G/T10178H V Page 1
APPENDIX 7 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CFR PART 36, APPENDIX F) MANUFACTURER MTOW ENGINE DATA PROPELLER DATA NOISE LEVEL (dBA)
MODEL MLW (1000#) MFR, MODEL NO. SHP EXH MFR, MODEL DIAM (IN) BLADES PITCH RPM MdBA PC CdBA NOTES BEECH 12.50 PRATT&WHITNEY 2 850 2 MCCAULEY 98 3 2000 79.32 -3.93 75.4 B200/B200C 12.50 PT6A-42 3GFR34C702/100LA-2 V BEECH 12.50 PRATT&WHITNEY 2 850 MCCAULEY 94 4 80.68 -3.93 76.8 B200/B200C/C12F 12.50 PT6A-42 4HFR34C754/94LA-0 V BEECH 12.50 PRATT&WHITNEY 2 845 1 HARTZELL 99 3 1996 82.80 -3.30 79.5 B200CT 12.50 PT6A-42 HC-B3TN-3G/T10178H V BEECH 12.50 PRATT&WHITNEY 2 850 1 MCCAULEY 98 3 2000 79.32 -3.84 75.5 B200T/B200CT 12.50 PT6A-42 3GFR34C702/100LA-Z BEECH 12.50 PRATT&WHITNEY 2 850 MCCAULEY 94 4 80.68 -3.84 76.8 B200T/B200CT 12.50 PT6A-42 4HFR34C754/94LA-O V BEECH 15.00 PRATT&WHITNEY 2 1050 2 HARTZELL 105 4 1700 75.90 -3.80 72.1 1 B300 PT6A-60A HC-B4MP-3/M10476K BEECH 3.86 TELEDYNE 1 293 MCCAULEY 78 3 2700 78.70 0.50 79.2 B36TC 3.86 TS10-520-U 82NDA-4 V BEECH 5.10 TELEDYNE 2 221 2 HARTZELL 76 3 2550 77.70 -3.00 74.7 B55 5.10 I0-470-L PHC-C3YF-2/FC7663-2 V BEECH 5.10 TELEDYNE 2 223 2 HARTZELL 78 2 2550 81.00 -3.00 78.0 B55 5.10 IO-470-L BHC-C2YF-2CH/FC846 V BEECH 5.40 TELEDYNE 2 254 2 HARTZELL 78 2 2550 82.00 -3.10 78.9 B58 5.40 10-520-C BHC-J2YF-2C/FC8475 V BEECH 5.40 TELEDYNE 2 256 2 HARTZELL 76 3 2650 81.90 -3.10 78.8 B58 5.40 I0-520-C PHC-J3YF-2/FC7663-D V BEECH 5.50 TCM 2 300 HARTZELL 4 2700 78.48 -3.08 75.4 B58 5.40 IO-550-C4B FC-7063Q V BEECH 6.10 TELEDYNE 2 301 2 HARTZELL 78 3 2600 80.60 -1.50 79.1 B58P 6.10 TSIO-520-L PHC-J3YF-2/FC7663-D V Page 2
APPENDIX 7 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CFR PART 36, APPENDIX F) MANUFACTURER MTOW ENGINE DATA PROPELLER DATA NOISE LEVEL (dBA)
MODEL MLW (1000#) MFR, MODEL NO. SHP EXH MFR, MODEL DIAM (IN) BLADES PITCH RPM MdBA PC CdBA NOTES BEECH 6.20 CONTINENTAL 2 294 4 HARTZELL 78 3 2600 78.20 -2.10 76.1 B58P 6.20 TS10-520-WB PHC-J3YF-2UF/FC7663 V BEECH 6.10 TELEDYNE 2 294 4 HARTZELL 78 3 2600 78.20 -2.10 76.1 B58TC 6.10 TS10-520-WB PHC-J3YF-2UF/FC7663 V BEECH 6.20 CONTINENTAL 2 301 2 HARTZELL 78 3 2600 80.60 -1.50 79.1 B58TC 6.20 TS10-520-L PHC-J3Y-2F/FC7663-D V BEECH 6.78 LYCOMING 2 296 2 HARTZELL 74 3 2750 82.10 -2.50 79.6 B60 6.78 TIO-541-E1C4 HC-F3YR-2UF/FC7479 V BEECH 9.02 PRATT&WHITNEY 2 700 4 HARTZELL 93 3 1900 76.20 -5.80 70.4 B65-90 8.55 PT6A-135 HC-B3TN-2(B)/T10173 V BEECH 3.98 LYCOMING 2 165 1 HARTZELL 76 2 2700 79.50 -2.30 77.2 B76 O-360-A1G6D HC-M2YR-2CLUF/FC7 V BEECH 3.90 LYCOMING 2 165 2 HARTZELL 76 2 2700 80.20 -1.50 78.7 B76 3.90 O-360-A1G6D HC-M2YR-2CEUF/FC7 V BEECH 1.68 LYCOMING 1 115 8 SENSENICH 72 2 2700 65.10 -1.30 63.8 B77 1.68 0-235-L2C 72CKS12-0-52 F BEECH 5.30 TCM 2 300 2 HARTZELL 74 4 2700 78.48 -3.08 75.4 B95-C55 5.30 IO-550-C FC-7063Q V BEECH 2.45 LYCOMING 1 163 2 SENSENICH 76 2 2700 73.30 0.00 73.3 C23 2.45 0-360-A4J 76EM8S5-0-60 F BEECH 2.75 LYCOMING 1 202 2 HARTZELL 76 2 2700 73.00 -1.30 71.7 C24R 2.75 0-360-A1B6 HC-M2YR-1BF/FC7666 V BEECH 9.66 PRATT&WHITNEY 2 550 HARTZELL 93 3 2200 78.70 -4.40 74.3 C90 9.17 PT6A-21 HC-B3TN-2B/T10173B V BEECH 10.10 PRATT&WHITNEY 550 4 HARTZELL 93 3 2200 78.69 -4.44 74.3 C90A PT6A-21 HC-B3TN-2(B) Page 3