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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