737 Operations Manual
Performance Inflight -
Engine Inoperative
737-500/CFM56-3_20K
Copyright © The Boeing Company. See title page for details.
PI.33.6 D6-27370-400E-TBCE
ENGINE INOP
MAX CONTINUOUS THRUST
Driftdown/LRC Cruise Range Capability
Ground to Air Miles Conversion
Driftdown/Cruise Fuel and Time
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
141 131 121 113 106 100 94 90 85 81 77
290 266 246 228 213 200 188 178 169 160 153
436 399 369 343 320 300 282 267 253 240 229
580 532 491 457 426 400 377 356 337 321 305
722 663 613 570 533 500 471 445 422 401 382
863 793 734 683 639 600 566 535 507 482 460
1002 923 855 796 745 700 660 625 593 564 538
1141 1052 975 909 851 800 755 715 678 646 616
1280 1180 1095 1021 957 900 850 805 764 727 694
1417 1308 1215 1134 1063 1000 944 895 850 809 773
1555 1436 1334 1246 1168 1100 1039 985 936 891 851
1693 1564 1454 1358 1274 1200 1134 1075 1022 973 929
1831 1693 1574 1471 1380 1300 1229 1165 1107 1055 1008
1970 1822 1694 1583 1486 1400 1323 1255 1193 1137 1086
2110 1951 1815 1696 1592 1500 1418 1345 1278 1218 1164
2250 2081 1936 1809 1698 1600 1513 1434 1364 1300 1241
AIR
DIST
(NM)
FUEL REQUIRED (1000 KG)
TIME
(HRS:MIN)
WEIGHT AT START OF DRIFTDOWN (1000 KG)
35 40 45 50 55 60 65
100 0.4 0.4 0.4 0.4 0.5 0.5 0.5 0:18
200 0.8 0.9 0.9 1.0 1.1 1.2 1.3 0:37
300 1.2 1.4 1.5 1.7 1.8 2.0 2.2 0:56
400 1.7 1.8 2.1 2.3 2.5 2.8 3.0 1:14
500 2.1 2.3 2.6 2.9 3.2 3.5 3.8 1:32
600 2.5 2.8 3.1 3.5 3.9 4.2 4.6 1:50
700 2.9 3.3 3.7 4.1 4.5 4.9 5.3 2:07
800 3.3 3.7 4.2 4.7 5.1 5.6 6.1 2:24
900 3.7 4.2 4.7 5.2 5.8 6.3 6.9 2:40
1000 4.1 4.6 5.2 5.8 6.4 6.9 7.6 2:57
1100 4.5 5.1 5.7 6.4 7.0 7.6 8.3 3:13
1200 4.9 5.5 6.2 7.0 7.7 8.3 9.1 3:30
1300 5.3 6.0 6.7 7.5 8.3 9.0 9.8 3:46
1400 5.7 6.4 7.2 8.1 8.9 9.6 10.5 4:03
1500 6.1 6.8 7.7 8.6 9.5 10.3 11.2 4:20
1600 6.5 7.3 8.2 9.2 10.1 10.9 12.0 4:37
Includes APU fuel burn.
Driftdown at optimum speed and cruise at Long Range Cruise speed.
June 08, 2001
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