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240 .37 84.0 85.5 86.3 87.1 87.9 88.6 89.4 90.1 90.0 89.5 89.1 88.6
260 .40 83.8 85.4 86.2 87.0 87.7 88.5 89.2 90.0 90.1 89.7 89.2 88.7
BLEED
CONFIGURATION
PRESS ALT (1000 FT)
1 3 5 7 10 12
ENGINE ANTI-ICE ON -0.7 -0.7 -0.8 -0.8 -0.9 -0.9
ENGINE AND WING ANTI-ICE ON -2.6 -2.6 -2.8 -2.9 -3.1 -3.1
December 1, 2000
737 Flight Crew Operations Manual
Performance Inflight -
Engine Inoperative
737-300/CFM56-3_20K
Copyright © The Boeing Company. See title page for details.
 PI.13.5
ENGINE INOP
MAX CONTINUOUS THRUST
Driftdown Speed/Level Off Altitude
100 ft/min residual rate of climb
WEIGHT (1000 KG) OPTIMUM
DRIFTDOWN
SPEED
(KIAS)
LEVEL OFF ALTITUDE (FT)
START
DRIFTDOWN
LEVEL
OFF
ISA + 10°C
& BELOW ISA + 15°C ISA + 20°C
64 61 235 15300 14000 12600
60 57 228 17200 16200 14900
56 53 220 18600 17900 17100
52 49 212 20400 19500 18700
48 46 204 22900 21900 20700
44 42 196 25500 24600 23500
40 38 187 28300 27400 26400
Includes APU fuel burn.
December 7, 2001
737 Flight Crew Operations Manual
Performance Inflight -
Engine Inoperative
737-300/CFM56-3_20K
Copyright © The Boeing Company. See title page for details.
PI.13.6
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
142 131 121 113 106 100 94 89 85 81 77
290 266 246 228 213 200 188 178 169 160 153
436 400 369 343 320 300 282 267 253 240 229
580 532 491 457 426 400 377 356 337 320 305
722 663 613 570 533 500 471 445 422 401 382
863 794 734 683 639 600 565 535 507 482 460
1004 923 855 796 745 700 660 624 592 564 537
1143 1053 976 909 851 800 755 714 678 645 615
1281 1181 1096 1022 957 900 849 804 764 727 694
1419 1310 1215 1134 1063 1000 944 894 849 809 772
1557 1438 1335 1246 1169 1100 1039 984 935 891 850
1695 1566 1455 1359 1274 1200 1134 1074 1021 973 929
1834 1695 1575 1471 1380 1300 1228 1164 1107 1054 1007
1972 1823 1695 1584 1486 1400 1323 1254 1192 1136 1085
2112 1953 1816 1697 1592 1500 1418 1344 1278 1218 1163
2252 2082 1936 1810 1698 1600 1512 1434 1363 1299 1241
AIR
DIST
(NM)
FUEL REQUIRED (1000 KG)
TIME
WEIGHT AT START OF DRIFTDOWN (1000 KG) (HRS:MIN)
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 1.3 1.4 1.5 1.7 1.9 2.0 2.2 0:56
400 1.7 1.9 2.1 2.4 2.6 2.8 3.1 1:14
500 2.1 2.4 2.7 3.0 3.2 3.5 3.9 1:32
600 2.5 2.8 3.2 3.6 3.9 4.2 4.6 1:50
700 2.9 3.3 3.7 4.2 4.5 4.9 5.4 2:07
800 3.4 3.8 4.3 4.7 5.2 5.6 6.2 2:24
900 3.8 4.2 4.8 5.3 5.8 6.3 6.9 2:41
1000 4.2 4.7 5.3 5.9 6.5 7.0 7.7 2:57
1100 4.6 5.2 5.8 6.5 7.1 7.7 8.4 3:14
1200 5.0 5.6 6.3 7.1 7.7 8.4 9.2 3:30
1300 5.4 6.1 6.8 7.6 8.4 9.1 9.9 3:47
1400 5.8 6.5 7.3 8.2 9.0 9.7 10.6 4:04
1500 6.2 7.0 7.8 8.8 9.6 10.4 11.4 4:21
1600 6.6 7.4 8.3 9.3 10.2 11.1 12.1 4:38
Includes APU fuel burn.
Driftdown at optimum driftdown speed and cruise at Long Range Cruise speed.
December 1, 2000
737 Flight Crew Operations Manual
Performance Inflight -
Engine Inoperative
737-300/CFM56-3_20K
Copyright © The Boeing Company. See title page for details.
 PI.13.7
ENGINE INOP
MAX CONTINUOUS THRUST
Long Range Cruise Altitude Capability
100 ft/min residual rate of climb
WEIGHT
(1000 KG)
PRESSURE ALTITUDE (FT)
ISA + 10°C
& BELOW ISA + 15°C ISA + 20°C
64 4600 2400
62 6100 4100 2500
60 10900 5600 4900
58 12400 10100 6800
56 13900 11700 9200
54 15400 13300 11100
52 16900 14800 12700
50 17700 16400 14400
48 18500 17500 16000
46 19300 18400 17400
44 20400 19200 18200
42 22100 20300 19200
40 23800 22100 20200
38 25600 23900 22100
36 27400 25800 24100
34 29200 27700 26000
32 30900 29600 28100
With engine anti-ice on, decrease altitude capability by 4000ft.
With engine and wing anti-ice on, decrease altitude capability by 7600ft.
June 7, 2002
737 Flight Crew Operations Manual
Performance Inflight -
Engine Inoperative
737-300/CFM56-3_20K
Copyright © The Boeing Company. See title page for details.
PI.13.8
ENGINE INOP
MAX CONTINUOUS THRUST
Long Range Cruise Control
　
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