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Flight Manual Continental Rev. 11/15/02 #41
>>@ Holding - One Engine Inop
Based On:
VMIN Drag
(210 Knots Lower Limit)
A/C Auto (High)
Flaps Up
PRESSURE
ALTITUDE
GROSS WEIGHT 1,000 LBS
FEET 135 130 125 120 115 110 105 100 95 90 85 80
30000
90.1
210
3410
25000
90.3
211
4040
88.7
210
3830
87.3
210
3660
86.1
210
3500
84.9
210
3360
20000
89.3
226
4630
88.0
220
4400
86.6
215
4180
85.2
210
3980
84.1
210
3810
82.9
210
3650
81.9
210
3510
80.9
210
3380
15000
89.4
243
5470
88.3
239
5240
87.2
234
5020
86.0
229
4800
84.9
224
4590
83.7
219
4390
82.5
214
4180
81.2
210
3990
80.1
210
3830
79.1
210
3680
78.1
210
3540
77.0
210
3420
10000
85.3
242
5450
84.3
237
5240
83.2
233
5030
82.1
229
4830
81.0
224
4620
79.9
219
4420
78.6
214
4220
77.3
210
4030
76.2
210
3880
75.1
210
3730
74.1
210
3600
73.1
210
3480
5000
81.5
242
5480
80.5
237
5280
79.4
233
5070
78.2
228
4870
77.0
223
4670
75.8
217
4470
74.5
212
4270
73.4
210
4100
72.2
210
3950
71.2
210
3810
70.1
210
3680
69.1
210
3570
1500
78.7
241
5520
77.6
236
5320
76.5
231
5120
75.4
226
4920
74.3
221
4720
73.0
216
4530
71.7
210
4330
70.6
210
4170
69.5
210
4030
68.4
210
3890
67.4
210
3760
66.4
210
3640
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 88 737
Rev. 11/15/02 #41 Continental Flight Manual
B Holding - One Engine Inop
Based On:
VMIN Drag
(Vref 40 + 70 Knots Lower Limit)
A/C Auto (High)
Flaps Up
PRESSURE GROSS WEIGHT 1000 LBS
ALTITUDE FEET 160 155 150 145 140 135 130 125
30000
25000
98.2
225
5010
96.4
220
4730
94.5
216
4450
92.5
212
4200
20000
95.1
239
5480
93.6
235
5250
92.3
231
5040
91.0
227
4830
89.9
223
4630
88.8
219
4450
87.7
215
4260
86.6
210
4080
15000
89.0
237
5330
88.1
234
5140
87.1
230
4960
86.2
226
4780
85.2
222
4600
84.1
217
4420
83.1
213
4240
82.0
209
4070
10000
84.6
236
5260
83.7
232
5090
82.8
229
4910
81.8
225
4740
80.8
221
4570
79.8
217
4400
78.8
213
4230
77.6
209
4070
5000
80.2
236
5250
79.4
232
5080
78.5
228
4920
77.6
224
4750
76.6
220
4590
75.7
216
4420
74.7
212
4260
73.6
208
4090
1500
77.5
235
5270
76.6
231
5110
75.7
228
4940
74.8
224
4780
73.8
220
4610
72.7
216
4450
71.6
212
4290
70.5
208
4130
B
PRESSURE GROSS WEIGHT 1000 LBS
ALTITUDE FT. 120 115 110 105 100 95 90
30000
98.9
204
4190
96.3
200
3890
94.0
195
3610
91.4
190
3360
89.1
185
3150
87.0
180
2940
25000
90.8
207
3980
89.2
203
3770
87.7
198
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本文链接地址：
737 FLIGHT MANUAL 737飞行手册2(139)
