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61.8
228
2700
60.9
224
2620
59.9
220
2540
59.0
216
2460
58.1
212
2370
57.2
208
2290
56.2
204
2210
55.2
199
2130
54.2
195
2050
53.1
190
1970
51.9
186
1890
50.8
182
1850
49.6
179
1770
1500
60.6
235
2910
59.8
231
2830
58.9
228
2750
58.1
224
2670
57.3
220
2590
56.4
216
2510
55.5
212
2420
54.6
208
2340
53.7
203
2260
52.7
199
2190
51.6
194
2110
50.6
190
2030
49.5
185
1950
48.3
182
1910
47.2
179
1840
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 70 737
Rev. 11/15/02 #41 Continental Flight Manual
C Holding
Based On:
Flaps Up
VMIN Drag
( Vref40 + 70 Knots Lower Limit)
PRESSURE GROSS WEIGHT 1,000 LBS
ALTITUDE
FEET
180 175 170 165 160 155 150 145 140 135 130 125 120 115 110 105 100
41000
93.4
217
2600
90.9
217
2430
89.4
212
2290
88.1
208
2170
86.8
203
2070
85.5
198
1960
84.2
192
1860
35000
93.5
250
3400
91.5
250
3220
90.1
248
3080
89.1
244
2950
88.2
240
2830
87.2
236
2720
86.3
232
2610
85.3
227
2500
84.4
223
2400
83.4
218
2300
82.5
214
2210
81.5
209
2110
80.4
204
2020
79.3
199
1950
78.2
195
1860
77.0
190
1770
30000
87.3
257
3230
86.6
253
3130
85.8
249
3030
85.1
245
2930
84.3
241
2830
83.5
237
2730
82.7
233
2640
81.8
229
2540
81.0
224
2450
80.1
220
2360
79.1
216
2270
78.1
212
2170
77.1
207
2080
76.0
203
1990
74.9
198
1930
73.7
193
1840
72.4
188
1760
25000
83.1
254
3150
82.4
250
3050
81.7
246
2960
80.9
243
2860
80.1
239
2770
79.3
235
2680
78.5
231
2580
77.6
227
2490
76.7
223
2400
75.7
219
2310
74.7
214
2220
73.7
210
2140
72.7
205
2060
71.7
201
1990
70.6
196
1910
69.5
192
1870
68.2
187
1790
20000
78.8
252
3130
78.1
248
3040
77.3
245
2950
76.5
241
2860
75.7
237
2780
74.9
233
2690
74.0
229
2610
73.2
225
2530
72.3
221
2450
71.5
217
2370
70.5
213
2290
69.5
208
2200
68.4
204
2120
67.3
200
2040
66.2
195
1950
65.1
191
1900
64.0
186
1820
15000
74.6
250
3180
73.9
246
3090
73.1
243
3010
72.4
239
2920
71.6
235
2830
70.8
231
2750
69.9
228
2660
69.0
224
2570
68.0
220
2490
67.1
216
2400
66.2
212
2320
65.3
207
2240
64.4
203
2160
63.4
199
2080
62.4
195
1990
61.2
190
1910
59.8
186
1860
10000
70.5
249
3200
69.7
245
3110
69.0
242
3020
68.2
238
2940
67.5
234
2860
66.7
230
2770
66.0
227
2690
65.2
223
2610
64.4
219
2520
63.5
215
2440
　
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本文鏈接地址：737 FLIGHT MANUAL 737飛行手冊2(132)