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35000
35800
36300
32200
33600
34600
135
130
125
120
37200
38000
38800
39700
38300
39000
39700
40400
37100
37800
38500
39200
35600
36200
37000
37700
D Maneuver Capability
LRC AND .79 MACH
MAXIMUM PRESSURE ALTITUDE (FT)
WEIGHT MANEUVER CAPABILITY 'G' (BANK ANGLE)
1000 LB 1.2 (33°) 1.3 (39°) 1.4 (44°) 1.5 (48°) 1.6 (51°) 1.7 (54°)
180
175
170
36000
36600
37200
34200
34800
35400
32600
33200
33800
31200
31800
32500
29900
30600
31200
28700
29300
29900
165
160
155
37800
38500
39100
36000
36700
37300
34500
35100
35800
33100
33800
34400
31800
32500
33200
30600
31200
31900
150
145
140
39800
40500
41000
38000
38700
39400
36500
37200
37900
35100
35800
36600
33900
34600
35300
32600
33400
34100
135
130
125
120
40200
41000
38600
39400
40300
41000
37300
38100
38900
39800
36100
36900
37700
38500
34900
35700
36500
37300
Sec. 5 Page 56 737
Rev. 11/15/02 #41 Continental Flight Manual
(Continued)
>> Two Engine Long Range Cruise
LONG RANGE CRUISE
ALL ENGINES l A/C AUTO
MAX CRUISE THRUST
LIMITS
ISA Average % N1 Required
Max TAT for Thrust Rating
IAS Knots
Mach Number
ISA Fuel Flow LB/HR/ENG
ISA TAS Kts.
PRESSURE ALTITUDE 37000 FT TO 25000 FT
Press
Alt
1000
GROSS WEIGHT (1,000 POUNDS)
Feet
(Std
TAT)
140 135 130 125 120 115 110 105 100 95 90 85 80 75
37
(-32)
91.1
-21
239
.743
2751
426
89.3
-14
240
.745
2602
427
87.8
-7
240
.745
2473
427
86.4
0
240
.745
2360
427
85.2
240
.745
2260
427
84.2
240
.745
2174
427
83.2
240
.745
2097
427
82.3
240
.745
2026
427
81.4
239
.743
1956
426
80.3
237
.736
1871
422
79.2
233
.725
1783
416
35
(-30)
90.5
-16
251
.744
2938
429
89.0
-9
251
.745
2798
429
87.7
-3
252
.745
2674
430
86.5
2
251
.745
2563
429
85.4
251
.745
2465
429
84.5
251
.745
2379
429
83.6
251
.745
2301
429
82.8
251
.745
2229
429
81.9
251
.744
2160
429
81.0
249
.739
2078
426
80.0
246
.731
1991
421
78.9
242
.719
1901
414
77.7
237
.705
1804
406
33
(-26)
89.0
-6
263
.745
3009
433
87.8
0
263
.745
2891
433
86.8
4
263
.745
2783
433
85.8
263
.745
2688
433
85.0
263
.745
2603
433
84.2
263
.745
2525
433
83.4
263
.745
2452
433
82.6
263
.744
2381
433
81.8
261
.741
2302
431
80.9
259
.734
2214
427
80.0
255
.724
2124
421
78.9
250
.712
2029
414
77.7
245
.698
1929
406
76.5
239
.682
1827
397
31
(-21)
86.9
7
275
.745
3009
437
86.1
11
275
.745
2918
437
85.4
275
.745
2834
437
84.6
275
.745
2757
437
83.9
275
.745
2683
437
83.2
275
.744
2612
437
82.5
273
.741
2531
435
81.6
271
.735
2443
　
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