737-800/CFM56-7B26 Takeoff
FAA Category C Brakes
737 Flight Crew Operations Manual
Takeoff Obstacle Limit Weight Flaps 5 Sea Level 30°C & Below, Zero Wind Based on engine bleed for packs on and anti-ice off Wind Adjustments
WIND (KTS) OAT & ALT ADJUSTED OBSTACLE LIMIT WEIGHT (1000 KG)
40 50 60 70 80 90
15 T W 10 T W 5 T W -6.0 -4.0 -2.0 -6.2 -4.1 -2.1 -6.4 -4.3 -2.1 -6.6 -4.4 -2.2 -6.9 -4.6 -2.3 -7.1 -4.7 -2.4
0 10 H W 20 H W 0 1.3 2.6 0 1.1 2.2 0 1.0 1.9 0 0.8 1.6 0 0.6 1.2 0 0.5 0.9
30 H W 40 H W 3.9 5.2 3.4 4.6 2.9 3.9 2.4 3.2 1.9 2.5 1.4 1.8
With engine bleed for packs off, increase weight by 550 kg.
With engine anti-ice on, decrease weight by 250 kg.
With engine and wing anti-ice on, decrease weight by 1300 kg (optional system).
Copyright . The Boeing Company. See title page for details.
737-800/CFM56-7B26 FAA Category C Brakes 737 Flight Crew Operations Manual
Long Range Cruise Maximum Operating Altitude Max Cruise Thrust ISA + 10°C and Below
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°)
85 80 75 30300 31600 33000 -5 -8 -11 32800* 34400* 35900* 32800* 34400* 35900* 32800* 34400* 35900* 32100 33400 34800 30700 32000 33400
70 65 60 34500 36000 37700 -15 -18 -18 37300* 38700* 40200* 37300* 38700* 40200* 37300* 38700* 40200* 36200 37800 39400 34900 36400 38100
55 50 45 40 39500 41000 41000 41000 -18 -18 -18 -18 41000 41000 41000 41000 41000 41000 41000 41000 41000 41000 41000 41000 41000 41000 41000 41000 39900 41000 41000 41000
ISA + 15°C
WEIGHT OPTIMUM TAT MARGIN TO INITIAL BUFFET 'G' (BANK ANGLE)
(1000 KG) ALT (FT) (°C) 1.20 (33°) 1.25 (36°) 1.30 (39°) 1.40 (44°) 1.50 (48°)
85 80 75 30300 31600 33000 0 -3 -6 30600* 32900* 34800* 30600* 32900* 34800* 30600* 32900* 34800* 30600* 32900* 34800 30600* 32000 33400
70 65 60 34500 36000 37700 -9 -13 -13 36300* 37800* 39200* 36300* 37800* 39200* 36300* 37800* 39200* 36200 37800 39200* 34900 36400 38100
55 50 45 40 39500 41000 41000 41000 -13 -13 -13 -13 40800* 41000 41000 41000 40800* 41000 41000 41000 40800* 41000 41000 41000 40800* 41000 41000 41000 39900 41000 41000 41000
ISA + 20°C
WEIGHT OPTIMUM TAT MARGIN TO INITIAL BUFFET 'G' (BANK ANGLE)
(1000 KG) ALT (FT) (°C) 1.20 (33°) 1.25 (36°) 1.30 (39°) 1.40 (44°) 1.50 (48°)
85 80 75 30300 31600 33000 6 3 0 27500* 30000* 32800* 27500* 30000* 32800* 27500* 30000* 32800* 27500* 30000* 32800* 27500* 30000* 32800*
70 65 60 34500 36000 37700 -3 -7 -7 34900* 36500* 38000* 34900* 36500* 38000* 34900* 36500* 38000* 34900* 36500* 38000* 34900 36400 38000*
55 50 45 40 39500 41000 41000 41000 -7 -7 -7 -7 39500* 41000 41000 41000 39500* 41000 41000 41000 39500* 41000 41000 41000 39500* 41000 41000 41000 39500* 41000 41000 41000
*Denotes altitude thrust limited in level flight, 100 fpm residual rate of climb.
Copyright . The Boeing Company. See title page for details.
September 27, 2004 PD.41.1
Performance Dispatch
737-800/CFM56-7B26 Enroute
FAA Category C Brakes
737 Flight Crew Operations Manual
Long Range Cruise Trip Fuel and Time Ground to Air Miles Conversion
AIR DISTANCE (NM) GROUND DISTANCE (NM) AIR DISTANCE (NM)
HEADWIND COMPONENT (KTS) TAILWIND COMPONENT (KTS)
100 80 60 40 20 20 40 60 80 100
279 554 829 259 515 771 241 480 720 226 450 675 212 424 636 200 400 600 190 382 573 181 365 548 173 349 525 166 335 504 160 322 485
1103 1376 1649 1027 1282 1536 958 1197 1435 899 1123 1348 847 1059 1270 800 1000 1200 764 956 1147 732 915 1098 701 877 1053 673 843 1012 648 811 974
1921 2192 2463 1791 2044 2297 1673 1911 2148 1571 1795 2019 1482 1693 1904 1400 1600 1800 1339 1530 1721 1282 1465 1648 1229 1405 1581 1181 1351 1520 1138 1301 1465
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