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.11.6 September 29, 2005
737-700/CFM56-7B20
Performance Dispatch
FAA
Enroute
Category A Brakes
737 Flight Crew Operations Manual
MAX CONTINUOUS THRUST
Net Level Off Weight
PRESSURE ALTITUDE (1000 FT) LEVEL OFF WEIGHT (1000 KG)
ISA + 10° & BELOW ISA + 15°C ISA + 20°C
30 28 26 43.5 47.3 51.4 42.3 45.9 49.8 44.4 48.3
24 22 20 54.8 57.3 59.8 53.1 55.4 57.4 51.4 53.4 54.6
18 16 14 61.3 61.9 64.1 58.3 58.7 61.1 55.0 55.8 58.2
12 10 8 6 66.7 69.4 72.3 75.3 63.5 66.0 68.9 71.8 60.3 62.8 65.6 68.3
Anti-Ice Adjustments
ANTI-ICE CONFIGURATION LEVEL OFF WEIGHT ADJUSTMENT (1000 KG)
PRESSURE ALTITUDE (1000 FT)
6 8 10 12 14 16 18 20 22 24 26 28 30
ENGINE ONLY -2.2 -2.1 -2.2 -2.0 -1.8 -1.9 -1.9 -1.9 -1.5 -1.3 -1.2 -1.1 -1.0
ENGINE & WING -8.0 -7.9 -7.8 -7.5 -7.0 -7.0 -7.0 -6.7 -5.9 -5.0 -4.5 -4.3
Copyright . The Boeing Company. See title page for details.
March 29, 2004 PD.11.7
Performance Dispatch
737-700/CFM56-7B20 Enroute
FAA Category A 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
290 593 897 266 541 816 246 497 749 228 460 692 213428643 200 400 600 188 376 563 178 354 530 169 335 501 160 317 474 153302451
1201 1505 1809 1091 1367 1642 1000 1252 1504 923 1155 1387 8571072 1287 80010001200 750 937 1124 706 882 1058 667 832 998 631 788 945 600749898
2113 2417 2721 1917 2193 2468 1755 2007 2259 1618 1850 2082 1501 1716 1931 140016001800 1312 1499 1686 1234 1409 1585 1164 1330 1496 1102 1260 1417 104711961345
Critical Fuel (1000 KG)
AIR DIST (NM) WEIGHT AT CRITICAL POINT (1000 KG)
40 45 50 55 60 65 70 75 80
200300400 1.8 2.5 3.2 1.8 2.6 3.3 1.92.73.4 2.0 2.8 3.6 2.1 2.9 3.7 2.1 3.0 3.8 2.23.14.0 2.3 3.2 4.1 2.4 3.3 4.2
500600700 3.9 4.6 5.3 4.1 4.8 5.5 4.25.05.7 4.4 5.2 5.9 4.5 5.3 6.1 4.7 5.5 6.3 4.85.76.6 5.0 5.9 6.8 5.2 6.1 7.0
8009001000 6.0 6.7 7.4 6.2 7.0 7.7 6.57.27.9 6.7 7.5 8.2 6.9 7.7 8.5 7.2 8.0 8.8 7.48.29.1 7.6 8.5 9.4 7.9 8.8 9.7
110012001300 8.2 8.9 9.6 8.4 9.1 9.8 8.79.410.1 9.0 9.8 10.5 9.3 10.1 10.9 9.6 10.411.2 9.9 10.8 11.6 10.3 11.1 12.0 10.6 11.5 12.3
1400 15001600 10.3 11.0 11.7 10.511.211.9 10.9 11.612.3 11.3 12.0 12.7 11.7 12.4 13.2 12.012.813.6 12.4 13.2 14.0 12.8 13.7 14.5 13.2 14.1 15.0
1700 1800 12.413.1 12.6 13.3 13.0 13.7 13.5 14.2 13.9 14.7 14.415.2 14.9 15.7 15.3 16.2 15.8 16.7
Based on: Emergency descent to 10000 ft. Level cruise at 10000 ft. 250 KIAS descent to 1500 ft. 15 minute
hold at 1500 ft. One missed approach; approach and land. 5% allowance for wind errors.
Increase fuel required 0.5% for each 10°C hotter than ISA conditions.
If icing conditions exists, increase fuel by 16% to account for engine and wing anti-ice on (6%) and ice
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