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ISA +
15°C
ISA +
20°C
180 173 265 18800 17700 16700
170 163 258 20300 19300 18200
160 154 251 21700 20800 19800
150 144 243 23100 22300 21400
140 135 235 24700 23900 23000
130 125 226 26500 25600 24800
120 115 218 28400 27600 26700
110 106 209 30300 29600 28700
100 ft/min residual rate of climb
D Driftdown Speed / Level Off - One Engine Inop
WEIGHT
1000 LBS LEVEL OFF ALTITUDE – FT
START
DRIFT
DOWN
LEVEL
OFF
OPTIMUM
DRIFT DOWN
SPEED
ISA + 10°C
&
BELOW
ISA +
20°C
ISA +
30°C
180 173 267 18300 17100 15900
170 163 261 19800 18700 17500
160 154 252 21200 20200 19100
150 145 243 22600 21700 20700
140 135 234 24100 23200 22300
130 125 225 25900 24900 24000
120 116 216 27900 27000 26000
110 106 206 29900 29100 28100
100 ft/min residual rate of climb
737 Sec. 5 Page 81
Flight Manual Continental Rev. 11/15/02 #41
>> Altitude Capability - LRC - One Engine Inop
Max Continuous Thrust
WEIGHT PRESSURE ALTITUDE - FT
1000 LB ISA + 10°C
BELOW
ISA + 15°C ISA + 20°C
140
130
120
110
100
90
80
70
10,600
13,800
17,000
18,700
21,100
24,800
28,800
32,300
4,400
10,500
15,000
17,800
19,600
23,100
27,200
31,500
4,400
8,800
12,800
16,300
18,600
21,300
25,600
30,100
Based on A/C Auto (HIGH)
@ Altitude Capability - LRC - One Engine Inop
Max Continuous Thrust
WEIGHT PRESSURE ALTITUDE
1000 LB ISA + 10°C
& Below
ISA + 15°C ISA + 20°C
140
130
120
110
100
90
80
11,100
14,300
17,200
19,000
21,500
25,200
29,000
5,700
12,100
15,500
18,000
19,800
23,600
27,600
5,000
9,700
13,300
16,900
18,900
21,800
26,000
Based on A/C AUTO (HIGH)
B Altitude Capability - LRC - One Engine Inop
Max Continuous Thrust
WEIGHT PRESSURE ALTITUDE
1000 LB ISA + 10°C
& Below
ISA + 15°C ISA + 20°C
155
150
145
140
135
130
125
120
115
18000
19300
20500
21600
22800
24000
25200
26400
27600
15500
16800
18000
19300
20900
22300
23600
24900
26300
12900
14400
15800
17100
18500
19900
21300
22700
24100
Based on A/C AUTO
Sec. 5 Page 82 737
Rev. 11/15/02 #41 Continental Flight Manual
C Altitude Capability - LRC - One Engine Inop
Max Continuous Thrust
WEIGHT PRESSURE ALTITUDE
1000 LB ISA + 10°C
& Below
ISA + 15°C ISA + 20°C
180
175
170
165
160
155
150
145
140
135
130
125
120
15300
16300
17200
18200
19100
20100
20800
21500
22200
23000
23800
24600
25600
12800
13900
15300
16300
17300
18400
19400
20300
21100
21800
22600
23400
24300
10500
11700
12900
14100
15200
16200
17200
18200
19300
20200
21100
22000
22900
Based on A/C AUTO
D Altitude Capability - LRC - One Engine Inop
Max Continuous Thrust
WEIGHT PRESSURE ALTITUDE
1000 LB ISA + 10°C
& Below
ISA + 15°C ISA + 20°C
180
175
170
165
160
155
150
145
140
135
130
125
120
15500
16500
17400
18300
19300
20100
20800
21600
22300
23100
23900
24700
25800
13500
14700
15700
16600
17600
18600
19600
20400
21200
22000
22800
23600
24500
10800
12000
13300
14600
15600
16600
17600
18700
19800
20600
21500
22400
23200
Based on A/C AUTO
737 Sec. 5 Page 83
Flight Manual Continental Rev. 11/15/02 #41
>>@ LRC Mach Schedule - One Engine Inop
WEIGHT PRESSURE ALTITUDE - 1000 FT
1000 LB 12 14 16 18 20 22 24 26 28 30
140 .58 .59
　
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