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62.5
194
2000
61.3
190
1920
60.0
187
1880
10000
70.5
249
3200
69.7
245
3120
69.0
242
3030
68.3
238
2950
67.5
234
2860
66.8
230
2780
66.0
227
2700
65.3
223
2620
64.4
219
2530
63.6
215
2450
62.6
211
2370
61.5
206
2290
60.4
202
2210
59.3
198
2130
58.2
194
2050
57.1
190
1960
56.1
187
1890
5000
66.8
247
3230
66.1
244
3150
65.5
241
3060
64.7
237
2980
63.9
233
2900
63.0
229
2820
62.1
226
2740
61.2
222
2660
60.3
218
2580
59.4
214
2500
58.5
210
2420
57.5
206
2330
56.6
202
2250
55.7
197
2170
54.6
193
2090
53.6
190
2020
52.5
187
1940
1500
64.1
247
3280
63.3
243
3200
62.5
240
3120
61.7
236
3040
60.9
232
2960
60.1
229
2880
59.3
225
2790
58.5
222
2710
57.7
218
2630
56.9
214
2550
56.0
209
2470
55.1
205
2390
54.2
201
2310
53.2
197
2230
52.2
193
2160
51.2
190
2080
50.1
187
2010
Note: Fuel flow is based on a racetrack pattern.
For holding in straight and level flight, reduce fuel flow values by 5%.
%N1
KIAS
FF/ENG LB/HR
Sec. 5 Page 72 737
Rev. 11/15/02 #41 Continental Flight Manual
>>@ Alternate Planning
All Engine
Distance Time
Landing Weight – Lbs. Cruise
Altitude
To
Alternate
To
Alternate
80,000 to
90,000
90,000 to
100,000
100,000 to
114,000
To
Alternate
Fuel – Lbs.
50 & Less :13 1350 1400 1490 10,000
100 :21 2050 2150 2280 21,000
150 :29 2640 2780 2980 27,000
200 :35 3180 3350 3610 31,000
300 :49 4160 4410 4790 35,000
400 1:03 5170 5490 5980 35,000
500 1:17 6190 6570 7170 35,000
600 1:31 7210 7660 8380 35,000
Conditions: Climb at 280/.74
Cruise at Long Range Cruise
Descent at .74/280
B Alternate Planning
All Engine
Distance Time
Landing Weight – Lbs. Cruise
Altitude
To
Alternate
To
Alternate
100,000 to
110,000
110,000 to
120,000
120,000 to
128,000
To
Alternate
Fuel – Lbs.
50 & Less :13 1340 1410 1470 10,000
100 :22 2070 2180 2260 19,000
150 :29 2700 2830 2930 23,000
200 :36 3260 3420 3550 27,000
300 :49 4270 4500 4690 35,000
400 1:03 5300 5570 5800 35,000
500 1:16 6240 6600 6900 37,000
600 1:29 7190 7650 8070 39,000
Conditions: Climb at 280/.78
Cruise at Long Range Cruise
Descent at .78/280
737 Sec. 5 Page 73
Flight Manual Continental Rev. 11/15/02 #41
C Alternate Planning
All Engine
Distance Time
Landing Weight – Lbs. Cruise
Altitude
To
Alternate
To
Alternate
120,000 to
130,000
130,000 to
140,000
140,000 to
144,000
To
Alternate
Fuel – Lbs.
50 & Less :13 1500 1570 1600 10,000
100 :22 2320 2430 2470 19,000
150 :30 3020 3170 3220 23,000
200 :37 3680 3850 3920 27,000
300 :50 4870 5110 5220 35,000
400 1:03 6020 6320 6450 35,000
500 1:16 7180 7540 7700 35,000
600 1:30 8340 8770 8950 35,000
Conditions: Climb at 280/.78
Cruise at Long Range Cruise
Descent at .78/280
D Alternate Planning
All Engine
Distance Time
Landing Weight – Lbs. Cruise
Altitude
To
Alternate
To
Alternate
120,000 to
130,000
130,000 to
140,000
140,000 to
146,300
To
Alternate
Fuel – Lbs.
50 & Less :13 1510 1580 1630 10,000
100 :22 2340 2450 2520 19,000
150 :30 3060 3200 3290 23,000
200 :37 3720 3900 4010 27,000
300 :50 4930 5180 5340 35,000
400 1:03 6100 6410 6610 35,000
500 1:16 7280 7650 7900 35,000
600 1:30 8460 8900 9260 35,000
Conditions: Climb at 280/.78
　
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