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°)
80 75 70 31000 32400 33900 -8 -11 -14 34400* 35900* 37300* 34400* 35900* 37300* 34400* 35900* 37300* 33500 34800 36300 32100 33500 34900
65 60 55 35500 37100 39000 -18 -19 -19 38700* 40200* 41000 38700* 40200* 41000 38700* 40200* 41000 37800 39500 41000 36500 38100 39900
50 45 40 40900 41000 41000 -19 -19 -19 41000 41000 41000 41000 41000 41000 41000 41000 41000 41000 41000 41000 41000 41000 41000
35 30 41000 41000 -19 -19 41000 41000 41000 41000 41000 41000 41000 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°)
80 75 70 31000 32400 33900 -2 -5 -8 33100* 34900* 36400* 33100* 34900* 36400* 33100* 34900* 36400* 33100* 34800 36300 32100 33500 34900
65 60 55 35500 37100 39000 -12 -13 -13 37900* 39400* 40900* 37900* 39400* 40900* 37900* 39400* 40900* 37800 39400* 40900* 36500 38100 39900
50 45 40 40900 41000 41000 -13 -13 -13 41000 41000 41000 41000 41000 41000 41000 41000 41000 41000 41000 41000 41000 41000 41000
35 30 41000 41000 -13 -13 41000 41000 41000 41000 41000 41000 41000 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°)
80 75 70 31000 32400 33900 4 0 -3 30800* 33300* 35200* 30800* 33300* 35200* 30800* 33300* 35200* 30800* 33300* 35200* 30800* 33300* 34900
65 60 55 35500 37100 39000 -6 -8 -8 36800* 38300* 39800* 36800* 38300* 39800* 36800* 38300* 39800* 36800* 38300* 39800* 36500 38100 39800*
50 45 40 40900 41000 41000 -8 -8 -8 41000 41000 41000 41000 41000 41000 41000 41000 41000 41000 41000 41000 41000 41000 41000
35 30 41000 41000 -8 -8 41000 41000 41000 41000 41000 41000 41000 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.
March 29, 2004 PD.21.1
Performance Dispatch
737-700/CFM56-7B22 Enroute
FAA Category A 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
275 544 812 256 508 759 239 475 712 224 447 670 212423633 200 400 600 190 381 573 181 364 548 173 349 524 166 334 503 159322484
1081 1348 1614 1011 1262 1512 948 1184 1419 893 1116 1338 8441055 1266 80010001200 764 956 1147 731 914 1098 700 876 1052 672 842 1011 647810973
1880 2145 2409 1761 2011 2259 1654 1889 2123 1560 1782 2004 1476 1687 1897 140016001800 1338 1530 1721 1281 1464 1648 1228 1404 1580 1180 1349 1518 113612991462
2673 2936 3198 2507 2755 3002 2357 2591 2824 2225 2446 2667 2107 2317 2528 200022002400 1913 2104 2295 1831 2015 2198 1756 1932 2108 1688 1857 2026 162517881952
3460 3721 3982 3248 3495 3741 3057 3289 3522 2888 3109 3329 2738 2947 3157 260028003000 2487 2678 2870 2382 2565 2749 2285 2461 2637 2196 2365 2535 211522782442
4242 4501 4760 3986 4232 4477 3754 3987 4219 3550 3770 3991 3367 3577 3787 320034003600 3062 3253 3445 2933 3117 3301 2814 2991 3167 2705 2875 3045 260627702933
5019 5278 5536 4721 4966 5210 4451 4682 4914 4211 4431 4651 3996 4206 4416 380040004200 3637 3828 4020 3485 3668 3852 3344 3521 3697 3215 3385 3555 309732613425
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