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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 9500 7200 4900
60 12300 10200 7900
56 15200 13200 11000
52 18000 16200 14100
48 20900 19200 17400
44 24000 22300 20600
40 27000 25600 24000
36 30000 28800 27500
32 33200 32200 31000
With engine anti-ice on, decrease altitude capability by 1400ft.
With engine and wing anti-ice on, decrease altitude capability by 5300ft.
June 7, 2002
737 Flight Crew Operations Manual
Performance Inflight -
Engine Inoperative
737-300/CFM56-3_22K
Copyright © The Boeing Company. See title page for details.
PI.23.8
ENGINE INOP
MAX CONTINUOUS THRUST
Long Range Cruise Control
WEIGHT
(1000 KG)
PRESSURE ALTITUDE (1000 FT)
10 12 14 16 18 20 22 24 26 28
64
%N1 90.9 92.4
MACH .561 .577
KIAS 311 309
FF/ENG 2974 2952
60
%N1 89.2 90.7 92.2
MACH .547 .564 .580
KIAS 303 302 299
FF/ENG 2796 2780 2755
56
%N1 87.5 88.9 90.4 91.9
MACH .531 .549 .566 .582
KIAS 294 293 292 289
FF/ENG 2613 2603 2584 2553
52
%N1 85.7 87.0 88.5 90.0 91.6 93.2
MACH .513 .532 .550 .567 .584 .600
KIAS 284 284 283 281 278 275
FF/ENG 2428 2419 2409 2383 2353 2333
48
%N1 83.6 85.1 86.5 88.0 89.5 91.1 92.8
MACH .495 .513 .532 .550 .568 .584 .600
KIAS 274 274 273 272 271 268 265
FF/ENG 2243 2233 2225 2210 2185 2161 2153
44
%N1 81.5 82.9 84.4 85.8 87.3 88.8 90.4 92.1
MACH .475 .493 .511 .530 .549 .567 .584 .600
KIAS 263 263 263 262 261 260 257 254
FF/ENG 2059 2049 2040 2030 2014 1994 1981 1970
40
%N1 79.0 80.5 82.0 83.5 84.9 86.4 88.0 89.6 91.3 93.3
MACH .454 .471 .489 .508 .527 .546 .565 .582 .599 .616
KIAS 251 251 251 251 250 250 248 246 243 239
FF/ENG 1878 1866 1857 1849 1838 1825 1816 1799 1781 1777
36
%N1 76.4 77.8 79.4 80.9 82.4 83.8 85.3 86.9 88.5 90.2
MACH .434 .449 .465 .484 .502 .522 .541 .561 .578 .595
KIAS 240 239 239 239 238 238 238 236 234 231
FF/ENG 1707 1689 1677 1668 1660 1650 1646 1635 1613 1594
December 1, 2000
737 Flight Crew Operations Manual
Performance Inflight -
Engine Inoperative
737-300/CFM56-3_22K
Copyright © The Boeing Company. See title page for details.
 PI.23.9
ENGINE INOP
MAX CONTINUOUS THRUST
Long Range Cruise Diversion Fuel and Time
Ground to Air Miles Conversion
Reference Fuel and Time Required at Check Point
Fuel Required Adjustment (1000 KG)
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
299 272 249 230 214 200 190 181 173 166 159
608 552 504 464 430 400 380 362 345 330 316
920 834 759 697 646 600 570 542 517 494 473
1235 1118 1015 932 862 800 760 722 688 658 630
1553 1403 1273 1167 1078 1000 949 903 860 821 787
1873 1691 1532 1403 1295 1200 1139 1082 1031 984 943
2196 1980 1792 1640 1512 1400 1328 1262 1202 1147 1099
2524 2273 2055 1877 1730 1600 1517 1441 1372 1310 1255
AIR
DIST
(NM)
PRESSURE ALTITUDE (1000 FT)
10 14 18 22 26
FUEL
(1000 KG)
TIME
(HR:MIN)
FUEL
(1000 KG)
TIME
(HR:MIN)
FUEL
(1000 KG)
TIME
(HR:MIN)
FUEL
(1000 KG)
TIME
(HR:MIN)
FUEL
(1000 KG)
TIME
(HR:MIN)
200 1.4 0:42 1.2 0:40 1.1 0:39 1.0 0:38 0.9 0:37
400 2.8 1:22 2.6 1:18 2.3 1:14 2.1 1:11 2.0 1:09
600 4.2 2:03 3.9 1:56 3.5 1:50 3.3 1:46 3.1 1:42
800 5.6 2:44 5.2 2:35 4.7 2:26 4.4 2:20 4.1 2:15
1000 7.0 3:26 6.4 3:14 5.9 3:03 5.5 2:55 5.2 2:48
1200 8.3 4:08 7.7 3:54 7.1 3:40 6.6 3:30 6.2 3:22
1400 9.6 4:51 8.9 4:34 8.2 4:18 7.7 4:05 7.2 3:56
1600 11.0 5:35 10.1 5:15 9.4 4:57 8.7 4:41 8.2 4:30
REFERENCE FUEL REQUIRED
(1000 KG)
WEIGHT AT CHECK POINT (1000 KG)
35 40 45 50 55 60
2 -0.2 -0.1 0.0 0.1 0.3 0.5
4 -0.3 -0.2 0.0 0.3 0.7 1.0
6 -0.5 -0.3 0.0 0.5 1.0 1.5
8 -0.7 -0.4 0.0 0.6 1.3 2.0
10 -0.9 -0.4 0.0 0.7 1.6 2.5
12 -1.0 -0.5 0.0 0.9 1.8 2.9
14 -1.2 -0.6 0.0 1.0 2.1 3.3
December 1, 2000
737 Flight Crew Operations Manual
Performance Inflight -
Engine Inoperative
737-300/CFM56-3_22K
Copyright © The Boeing Company. See title page for details.
PI.23.10
ENGINE INOP
MAX CONTINUOUS THRUST
Holding
Flaps Up
WEIGHT
(1000 KG)
　
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