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3660
69.1
189
3500
67.8
186
3350
1500
74.1
218
4660
73.1
214
4500
72.0
209
4340
70.9
205
4180
69.8
201
4030
68.7
196
3880
67.6
192
3720
66.4
189
3570
65.1
186
3410
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 90 737
Rev. 11/15/02 #41 Continental Flight Manual
D Holding - One Engine Inop
Based On:
VMIN Drag
(Vref40 + 70 Knots Lower Limit)
A/C Auto (High)
Flaps Up
PRESSURE GROSS WEIGHT 1000 LBS
ALTITUDE FEET 180 175 170 165 160 155 150 145
30000
25000
20000
97.3
237
5820
95.6
233
5530
94.0
229
5270
92.5
225
5040
15000
94.4
250
6450
93.3
246
6220
92.2
243
6000
91.3
239
5780
90.3
235
5580
89.4
231
5370
88.3
228
5170
87.3
224
4970
10000
89.4
249
6300
88.6
245
6100
87.7
242
5900
86.8
238
5700
85.9
234
5510
84.9
230
5310
83.9
227
5120
83.0
223
4930
5000
85.1
247
6260
84.3
244
6060
83.5
241
5870
82.6
237
5680
81.6
233
5490
80.6
229
5310
79.6
226
5120
78.6
222
4940
1500
82.2
247
6250
81.3
243
6060
80.4
240
5880
79.6
236
5690
78.7
232
5510
77.8
229
5330
76.9
225
5150
76.0
222
4980
D
PRESSURE GROSS WEIGHT 1000 LBS
ALTITUDE FT. 140 135 130 125 120 115 110 105 100
30000
95.2
193
3720
92.6
188
3440
25000
96.3
214
4660
94.1
210
4370
92.0
205
4110
90.2
201
3890
88.5
196
3680
87.1
192
3480
85.7
187
3290
20000
91.1
221
4820
89.8
217
4610
88.7
213
4410
87.5
208
4210
86.3
204
4020
85.0
200
3830
83.7
195
3640
82.3
191
3450
81.0
187
3280
15000
86.2
220
4780
85.2
216
4580
84.1
212
4390
82.9
207
4200
81.7
203
4020
80.5
199
3830
79.2
194
3660
77.9
190
3480
76.6
187
3330
10000
81.9
219
4750
80.9
215
4560
79.7
211
4380
78.5
206
4200
77.4
202
4030
76.2
198
3850
75.0
194
3680
73.8
190
3520
72.6
187
3360
5000
77.7
218
4770
76.7
214
4590
75.6
210
4410
74.6
206
4240
73.4
202
4060
72.1
197
3880
70.8
193
3720
69.6
190
3560
68.3
187
3410
1500
75.0
218
4800
73.9
214
4620
72.7
209
4440
71.5
205
4270
70.3
201
4100
69.1
197
3930
68.0
193
3770
66.8
190
3620
65.7
187
3480
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
737 Sec. 5 Page 91
Flight Manual Continental Rev. 11/15/02 #41
LANDING
NORMAL LANDING LIMITS – ACCULOAD
For dispatch purposes, FARs require that the flight must be planned to arrive at
the destination at a weight, which does not exceed the aircraft Structural
Landing Limit weight, the Approach Climb Limit weight, the Landing Climb
Limit weight or the Landing Field Length Limit weight, for the forecast
conditions at the planned destination airport and runway.
Normally, the Landing Limit is computed by ACCULOAD, which presents the
　
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