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8 0 12 30 45 C C C W W W
0 0 0 10 23 37 53 C C C W
150 4 0 0 18 32 48 C C C W W
8 0 8 28 43 C C C W W W
0 0 0 8 20 35 50 C C C C
145 4 0 0 17 30 47 C C C W W
8 0 0 27 40 57 C C C W W
0 0 0 7 18 33 47 C C C C
140 4 0 0 15 28 45 60 C C W W
8 0 0 23 35 53 C C C W W
0 0 0 0 15 32 43 C C C C
135 4 0 0 15 25 38 53 C C W W
8 0 0 22 33 50 C C C W W
0 0 0 0 13 28 40 C C C C
130 4 0 0 12 22 37 50 C C C C
8 0 0 20 32 47 C C C W W
0 0 0 0 10 22 33 47 60 C C
120 4 0 0 0 17 27 47 C C C C
8 0 0 13 27 42 58 C C W W
· Add 3 minutes for each approximate taxi mile.
· For low speed RTOs (<80Kts.) at airport elevations below 1000’ and OAT below
15°C no cooling time is required. Otherwise, use cooling limits for 80 knots.
· Interpolation may be used for airport elevations above 8000’.
0-60 mins Cool as scheduled prior to takeoff.
C Caution Wheel Fuse Plugs may melt. Delay takeoff and inspect after 60
minutes.
· Alert fire equipment. · Clear runway immediately.
W · Unless required, do not set
parking brake.
· Do not approach gear or
attempt taxi for 90 min.
· Tire, wheel, and brake replacement may be required.
Sec. 5 Page 50 737
Rev. 11/15/02 #41 Continental Flight Manual
INTENTIONALLY LEFT BLANK
737 Sec. 5 Page 51
Flight Manual Continental Rev. 11/15/02 #41
ENROUTE
NORMAL
>> Altitude Capability
LRC AND .74 MACH
OPTIMUM CRUISE THRUST LIMIT PRESS ALT (FT)
WEIGHT
1000 LB.
ALTITUDE
FEET
ISA + 10°C
& BELOW
ISA + 15°C ISA + 20°C
140
135
130
31000
31800
32600
34500
35400
36300
33600
34600
35600
32600
33700
34700
125
120
115
33500
34400
35300
37000
37000
37000
36500
37000
37000
35800
36700
37000
110
105
36200
37000
37000
37000
37000
37000
37000
37000
>> Maneuver Capability
LRC AND .74 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°)
140
135
130
34200
35000
35800
32600
33300
34200
31000
31800
32600
29500
30300
31100
28000
28800
29700
26700
27500
28300
125
120
115
36600 35000
35800
36600
33400
34300
35200
31900
32800
33700
30500
31400
32300
29200
30100
31000
110
105
100
36000
37000
34600
35600
36600
33300
34300
35300
32000
33000
34000
95
90
36300 35100
36200
Sec. 5 Page 52 737
Rev. 11/15/02 #41 Continental Flight Manual
@ Altitude Capability
LRC AND .74 MACH
OPTIMUM CRUISE THRUST LIMIT PRESS ALT (FT)
WEIGHT
1000 LB.
ALTITUDE
FEET
ISA + 10°C
& BELOW
ISA + 15°C ISA + 20°C
140
135
130
125
120
31000
31800
32600
33500
34400
34300
35200
36100
36900
37000
33400
34400
35400
36300
37000
32400
33500
34500
35600
36500
115
110
105
100
35300
36200
37000
37000
37000
37000
37000
37000
37000
37000
37000
37000
37000
37000
37000
37000
@ Maneuver Capability
LRC AND .74 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°)
140
135
130
125
120
34200
35100
35900
36700
32600
33400
34100
35000
35900
31000
31800
32600
33500
34300
29500
30300
31200
32000
32800
28000
28900
29700
30500
31400
26700
27500
28400
29200
30100
115
110
105
100
95
90
36800 35200
36100
33700
34700
35700
36700
32400
33400
34300
35300
36400
31000
　
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