Boeing 737 - PI.11 Performance Inflight -All Engines

737 Operations Manual
Performance Inflight - Chapter PI
All Engines Section 11
737-300/CFM56-3_22K
FAST-Doc PI/PD Template 9/1/99
Copyright © The Boeing Company. See title page for details.
D6-27370-400E-TBCE PI.11.1
PI.11 Performance Inflight --All Engines
All Engi nes
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 07, 2002