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150
64
150
68
150
72
160
75
170
FLAP POSITION WEIGHT (1000 KG)
32 40 48 56 64
FLAPS 15 PITCH ATT 4.5 4.5 4.5 4.5 4.5
(VREF 15+10) %N1 43 48 52 56 60
KIAS 123 138 151 163 173
FLAPS 30 PITCH ATT 2.0 2.0 2.0 2.5 2.5
(VREF 30+10) %N1 48 53 58 62 65
KIAS 116 129 141 152 162
FLAPS 40 PITCH ATT 0.5 0.5 0.5 0.5 0.0
(VREF 40+10) %N1 54 60 65 69 73
KIAS 113 125 137 150 161
June 3, 2005
737 Flight Crew Operations Manual
Performance Inflight -
General
737-300/CFM56-3_22K
Copyright © The Boeing Company. See title page for details.
PI.20.28
Intentionally
Blank
June 3, 2005
737 Flight Crew Operations Manual
Performance Inflight - Chapter PI
All Engines Section 21
737-300/CFM56-3_22K
FAST-Doc PI/PD Template 9/1/99
Copyright © The Boeing Company. See title page for details.
 PI.21.1
PI.21 Performance Inflight --All Engines All Engines Long Range Cruise Maximum Operating Altitude
Max Cruise Thrust
ISA + 10°C and Below
ISA + 15°C
ISA + 20°C
WEIGHT
(1000 KG)
OPTIMUM
ALT (FT)
TAT
(°C)
MARGIN TO INITIAL BUFFET 'G' (BANK ANGLE)
1.20 (33°) 1.25 (36°) 1.30 (39°) 1.40 (44°) 1.50 (48°)
64 30800 -10 34100 33200 32300 30700 29200
62 31500 -11 34700 33800 33000 31400 29900
60 32200 -13 35400 34500 33700 32100 30600
58 32900 -14 36100 35300 34400 32800 31400
56 33700 -16 36900 36000 35200 33600 32100
54 34400 -18 37000 36700 35900 34400 32900
52 35200 -19 37000 37000 36700 35200 33700
50 36100 -21 37000 37000 37000 36000 34500
48 36900 -21 37000 37000 37000 36800 35400
46 37000 -21 37000 37000 37000 37000 36300
44 37000 -21 37000 37000 37000 37000 37000
WEIGHT
(1000 KG)
OPTIMUM
ALT (FT)
TAT
(°C)
MARGIN TO INITIAL BUFFET 'G' (BANK ANGLE)
1.20 (33°) 1.25 (36°) 1.30 (39°) 1.40 (44°) 1.50 (48°)
64 30800 -4 34100 33200 32300 30700 29200
62 31500 -6 34700 33800 33000 31400 29900
60 32200 -7 35400 34500 33700 32100 30600
58 32900 -9 36100 35300 34400 32800 31400
56 33700 -10 36900 36000 35200 33600 32100
54 34400 -12 37000 36700 35900 34400 32900
52 35200 -14 37000 37000 36700 35200 33700
50 36100 -16 37000 37000 37000 36000 34500
48 36900 -16 37000 37000 37000 36800 35400
46 37000 -16 37000 37000 37000 37000 36300
44 37000 -16 37000 37000 37000 37000 37000
WEIGHT
(1000 KG)
OPTIMUM
ALT (FT)
TAT
(°C)
MARGIN TO INITIAL BUFFET 'G' (BANK ANGLE)
1.20 (33°) 1.25 (36°) 1.30 (39°) 1.40 (44°) 1.50 (48°)
64 30800 1 33600* 33200 32300 30700 29200
62 31500 0 34400* 33800 33000 31400 29900
60 32200 -2 35300* 34500 33700 32100 30600
58 32900 -3 36100 35300 34400 32800 31400
56 33700 -5 36800* 36000 35200 33600 32100
54 34400 -7 37000 36700 35900 34400 32900
52 35200 -8 37000 37000 36700 35200 33700
50 36100 -10 37000 37000 37000 36000 34500
48 36900 -10 37000 37000 37000 36800 35400
46 37000 -10 37000 37000 37000 37000 36300
44 37000 -10 37000 37000 37000 37000 37000
*Denotes altitude thrust limited in level flight, 100 fpm residual rate of climb.
June 7, 2002
737 Flight Crew Operations Manual
Performance Inflight -
All Engines
737-300/CFM56-3_22K
Copyright © The Boeing Company. See title page for details.
PI.21.2
All Engines Long Range Cruise Control
WEIGHT
(1000 KG)
PRESSURE ALTITUDE (1000 FT)
21 23 25 27 29 31 33 35 37
62
%N1 81.1 82.2 83.3 84.3 85.2 86.4 88.2 91.0
MACH .698 .718 .734 .744 .745 .745 .745 .744
KIAS 317 313 308 299 287 275 263 251
FF/ENG 1499 1479 1452 1419 1372 1337 1329 1356
58
%N1 79.7 81.0 82.1 83.1 84.1 85.1 86.3 88.4 92.3
MACH .682 .703 .722 .737 .744 .745 .745 .745 .742
KIAS 309 306 302 296 287 275 263 251 239
FF/ENG 1413 1396 1376 1348 1313 1271 1244 1244 1293
54
%N1 78.1 79.5 80.7 81.8 82.8 83.8 84.8 86.3 89.0
MACH .665 .685 .707 .725 .740 .745 .745 .745 .745
KIAS 301 298 295 291 285 275 263 251 240
FF/ENG 1328 1311 1295 1274 1248 1211 1174 1154 1169
50
%N1 76.5 77.8 79.1 80.4 81.5 82.5 83.4 84.5 86.5
MACH .646 .667 .688 .709 .728 .741 .745 .745 .745
KIAS 292 289 287 284 280 274 263 251 240
FF/ENG 1244 1227 1210 1195 1175 1150 1114 1081 1073
46
%N1 74.9 76.1 77.4 78.7 79.9 81.0 82.1 83.0 84.5
MACH .625 .647 .668 .689 .710 .729 .742 .745 .745
KIAS 282 280 278 276 273 269 262 251 240
FF/ENG 1160 1144 1128 1112 1098 1079 1055 1021 997
　
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