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32000
33000
34000
35200
36300
737 Sec. 5 Page 53
Flight Manual Continental Rev. 11/15/02 #41
B Altitude Capability
LRC AND .78 MACH
OPTIMUM CRUISE THRUST LIMIT PRESS ALT (FT)
WEIGHT
1000 LB.
ALTITUDE
FEET
ISA + 10°C
& BELOW
ISA + 15°C ISA + 20°C
155
150
145
33800
34500
35200
37200
37800
38500
36300
37000
37600
35000
35800
36500
140
135
130
35900
36700
37500
39100
39800
40500
38300
38900
39600
37200
37800
38500
125
120
115
38300
39100
40000
41000
41000
41000
40400
41000
41000
39200
40000
40700
B Maneuver Capability
LRC AND .78 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°)
155
150
145
39500
40200
40900
37800
38500
39200
36200
36800
37500
34800
35500
36200
33500
34200
34900
32200
32900
33600
140
135
130
41000 39900
40700
41000
38300
39000
39800
36900
37700
38500
35600
36400
37200
34300
35100
35900
125
120
115
40600
41000
39300
40100
41000
38000
38800
39700
36700
37600
38500
Sec. 5 Page 54 737
Rev. 11/15/02 #41 Continental Flight Manual
C Altitude Capability
LRC AND .78 MACH
OPTIMUM CRUISE THRUST LIMIT PRESS ALT (FT)
WEIGHT
1000 LB.
ALTITUDE
FEET
ISA + 10°C
& BELOW
ISA + 15°C ISA + 20°C
180
175
170
31100
31700
32400
33800
34600
35300
32100
33100
34000
29100
30300
31500
165
160
155
33000
33700
34300
36000
36600
37200
34900
35600
36200
32800
33800
34700
150
145
140
35000
35700
36500
37800
38500
39100
36900
37500
38200
35500
36200
37000
135
130
125
120
37200
38000
38800
39700
39800
40500
41000
41000
38800
39500
40200
40900
37600
38300
39000
39700
C Maneuver Capability
LRC AND .78 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
36400
37000
37600
34600
35200
35800
32900
33500
34200
31600
32200
32800
30300
30900
31500
29000
29600
30200
165
160
155
38300
38900
39600
36400
37100
37700
34800
35400
36100
33400
34100
34700
32200
32800
33500
30900
31600
32200
150
145
140
40200
40900
41000
38400
39100
39800
36800
37500
38200
35400
36100
36900
34200
34900
35600
32900
33700
34400
135
130
125
120
40600
41000
39000
39800
40600
41000
37600
38400
39200
40100
36400
37200
38000
38900
35200
36000
36800
37600
737 Sec. 5 Page 55
Flight Manual Continental Rev. 11/15/02 #41
D Altitude Capability
LRC AND .79 MACH
OPTIMUM CRUISE THRUST LIMIT PRESS ALT (FT)
WEIGHT
1000 LB.
ALTITUDE
FEET
ISA + 10°C
& BELOW
ISA + 15°C ISA + 20°C
180
175
170
31100
31800
32400
31200
32200
33200
27900
29100
30500
24400
25600
26900
165
160
155
33000
33700
34400
34100
35000
35700
31800
33000
34000
28100
29300
30600
150
145
140
35000
35800
36500
36300
37000
37600
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本文链接地址：
737 FLIGHT MANUAL 737飞行手册2(120)
