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500 600 700  4.1 4.9 5.6  4.3 5.1 5.8  4.4 5.2 6.0  4.6 5.4 6.2  4.7 5.6 6.4  4.9 5.8 6.6  5.0 6.0 6.8  5.2 6.2 7.1  5.4 6.3 7.3 
800 900 1000  6.4 7.2 7.9  6.6 7.4 8.1  6.8 7.6 8.4  7.0 7.9 8.7  7.3 8.1 8.9  7.5 8.4 9.2  7.7 8.6 9.5  8.0 8.9 9.8  8.2 9.2 10.1 
1100 1200 1300  8.7 9.4 10.2  8.9 9.6 10.4  9.2 10.0 10.7  9.5 10.3 11.1  9.8 10.6 11.4  10.1 10.9 11.8  10.4 11.3 12.1  10.7 11.6 12.5  11.1 12.0 12.9 
1400 1500 1600  10.9 11.7 12.5  11.1 11.9 12.7  11.5 12.3 13.0  11.9 12.7 13.4  12.2 13.1 13.9  12.6 13.5 14.3  13.0 13.9 14.7  13.4 14.3 15.2  13.8 14.7 15.7 
1700 1800  13.2 14.0  13.4 14.2  13.8 14.5  14.2 15.0  14.7 15.5  15.1 16.0  15.6 16.4  16.1 16.9  16.6 17.5 

Based on:  Emergency descent to 10000 ft.  Level cruise at 10000 ft.  250 KIAS descent to 1500 ft.  15 minutes
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 exist, increase fuel by 15% to account for engine and wing anti-ice on (7%) and ice
accumulation on unheated surfaces (8%).
Allowance for performance deterioration not included.
Compare the fuel required from this chart with critical fuel reserves for one engine inoperative.
Use the higher of the two.

Copyright . The Boeing Company. See title page for details.
737-800/CFM56-7B27

Performance Dispatch
FAA
Enroute
Category C Brakes
737 Flight Crew Operations Manual

MAX CONTINUOUS THRUST
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 
292 595 898  267 542 817  246 498 749  229 460 692  213 428 643  200 400 600  188 375 563  178 354 530  168 334 500  160 317 474  152 301 451 
1201 1504 1808  1092 1366 1641  1000 1252 1503  923 1155 1386  857 1072 1286  800 1000 1200  750 937 1124  706 882 1058  666 833 999  631 789 946  600 749 898 
2111 2414 2717  1916 2191 2466  1754 2006 2257  1618 1849 2081  1501 1716 1930  1400 1600 1800  1312 1499 1686  1234 1410 1586  1165 1331 1497  1103 1260 1417  1047 1197 1346 

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  1.7 2.3 3.0  1.7 2.4 3.1  1.8 2.5 3.3  1.9 2.7 3.4  2.0 2.8 3.6  2.1 2.9 3.7  2.1 3.0 3.8  2.2 3.1 4.0  2.3 3.2 4.1 
500 600 700  3.7 4.3 5.0  3.8 4.5 5.2  4.0 4.7 5.5  4.2 4.9 5.7  4.4 5.1 5.9  4.5 5.4 6.2  4.7 5.6 6.4  4.9 5.8 6.6  5.1 6.0 6.9 
800 900 1000  5.7 6.4 7.0  5.9 6.6 7.3  6.2 6.9 7.6  6.4 7.2 7.9  6.7 7.5 8.2  7.0 7.8 8.6  7.2 8.1 8.9  7.5 8.4 9.2  7.8 8.7 9.6 
1100 1200 1300  7.7 8.4 9.0  7.9 8.6 9.3  8.3 9.0 9.7  8.6 9.4 10.1  9.0 9.8 10.5  9.4 10.2 10.9  9.7 10.5 11.4  10.1 10.9 11.8  10.4 11.3 12.2 
1400 1500 1600  9.7 10.4 11.1  10.0 10.6 11.3  10.4 11.1 11.7  10.8 11.5 12.2  11.3 12.0 12.7  11.7 12.5 13.2  12.2 12.9 13.7  12.6 13.4 14.3  13.0 13.9 14.8 
1700 1800  11.7 12.4  12.0 12.6  12.4 13.1  12.9 13.6  13.5 14.2  14.0 14.8  14.5 15.3  15.1 15.9  15.6 16.5 

Based on:  Emergency descent to 10000 ft.  Level cruise at 10000 ft.  250 KIAS descent to 1500 ft.  15 minutes
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 exist, increase fuel by 15% to account for engine and wing anti-ice on (6%) and ice
accumulation on unheated surfaces (9%).
Allowance for performance deterioration not included.
Compare the fuel required from this chart with critical fuel reserves for all engines operative.
Use the higher of the two.

Copyright . The Boeing Company. See title page for details.
Performance Dispatch

737-800/CFM56-7B27 Enroute
FAA Category C Brakes
　
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