This table includes 5% additional fuel for holding in a racetrack pattern.
Copyright . The Boeing Company. See title page for details.
September 27, 2004 PD.51.5
Performance Dispatch
737-800/CFM56-7B27 Enroute
FAA Category C Brakes
737 Flight Crew Operations Manual
Flight Crew Oxygen Requirements Required Pressure (PSI) for 76 Cu. Ft. Cylinder
BOTTLE TEMPERATURE NUMBER OF CREW USING OXYGEN
°C °F 2 3 4
50 45 40 122 113 104 735 725 715 1055 1040 1020 1360 1340 1320
35 30 25 95 86 77 700 690 680 1005 990 975 1300 1280 1255
20 15 10 68 59 50 670 655 645 960 940 925 1240 1215 1195
5 0 -5 -10 41 32 23 14 635 620 610 600 910 890 875 860 1175 1150 1130 1110
Required Pressure (PSI) for 114/115 Cu. Ft. Cylinder
BOTTLE TEMPERATURE NUMBER OF CREW USING OXYGEN
°C °F 2 3 4
50 45 40 122 113 104 530 520 510 735 725 715 945 930 915
35 30 25 95 86 77 505 495 485 700 690 680 900 885 870
20 15 10 68 59 50 480 470 460 670 655 645 860 840 830
5 0 -5 -10 41 32 23 14 455 445 440 430 635 620 610 600 815 800 785 770
Copyright . The Boeing Company. See title page for details.
PD.51.6 September 29, 2005
737-800/CFM56-7B27
Performance Dispatch
FAA
Enroute
Category C Brakes
737 Flight Crew Operations Manual
MAX CONTINUOUS THRUST
Net Level Off Weight
PRESSURE ALTITUDE (1000 FT) LEVEL OFF WEIGHT (1000 KG)
ISA + 10°C & BELOW ISA + 15°C ISA + 20°C
30 28 26 42.5 46.3 50.3 41.3 44.9 48.8 43.5 47.3
24 22 20 54.7 59.4 64.4 52.9 57.4 62.2 51.3 55.5 60.1
18 16 14 69.4 74.2 78.1 66.9 71.8 76.3 64.4 69.4 74.3
12 10 83.4 86.1 81.1 85.4 78.2 81.8
Anti-Ice Adjustments
ANTI-ICE CONFIGURATION LEVEL OFF WEIGHT ADJUSTMENT (1000 KG)
PRESSURE ALTITUDE (1000 FT)
10 12 14 16 18 20 22 24 26 28 30
ENGINE ONLY -2.9 -2.5 -1.7 -1.6 -1.5 -1.4 -1.3 -1.2 -1.1
ENGINE AND WING -5.3 -7.8 -6.4 -6.6 -6.3 -5.8 -5.5 -5.1 -4.7 -4.4
Copyright . The Boeing Company. See title page for details.
September 27, 2004 PD.51.7
Performance Dispatch
737-800/CFM56-7B27 Enroute
FAA Category C Brakes
737 Flight Crew Operations Manual
Long Range Cruise Critical Fuel Reserves Ground to Air Miles Conversion
AIR DISTANCE (NM) GROUND AIR DISTANCE (NM)
HEADWIND COMPONENT (KTS) DISTANCE TAILWIND COMPONENT (KTS)
100 80 60 40 20 (NM) 20 40 60 80 100
287 585 882 264 535 806 245 494 742 228 458 688 213 427 641 200 400 600 189 376 564 178 355 532 169 336 503 161 319 478 153 304 455
1180 1477 1774 1077 1348 1619 991 1240 1489 918 1148 1379 855 1069 1283 800 1000 1200 752 939 1127 709 886 1062 671 838 1005 636 795 953 605 756 907
2072 2369 2667 1890 2161 2432 1738 1987 2236 1609 1839 2069 1497 1711 1925 1400 1600 1800 1315 1502 1690 1239 1416 1593 1172 1339 1506 1112 1270 1429 1057 1208 1358
Critical Fuel (1000 KG)
AIR DIST (NM) WEIGHT AT CRITICAL POINT (1000 KG)
45 50 55 60 65 70 75 80 85
200 300 400 1.8 2.6 3.4 1.9 2.7 3.5 2.0 2.8 3.6 2.1 2.9 3.7 2.1 3.0 3.9 2.2 3.1 4.0 2.3 3.2 4.1 2.4 3.3 4.3 2.4 3.4 4.4
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