Page 2-154
Pilot’s Operating Manual
Revision A1: Nov, 2002
Sub-section 2
PREFLIGHT
Hawker 800XP Pro Line 21
Section IV - FLIGHT PLANNING DATA
INTERMEDIATE PROCEDURE
ALTITUDE
29,000 ft
31,000 ft
33,000 ft
35,000 ft
SECTOR
SECTOR
SECTOR
SECTOR
AIR DIST
nm
TIME
min
FUEL
lb
TIME
min
FUEL
lb
TIME
min
FUEL
lb
TIME
min
FUEL
lb
100
200
36
1023
36
1019
36
1013
36
1010
300
49
1438
49
1431
49
1405
50
1384
400
63
1852
62
1842
63
1796
63
1754
500
77
2266
76
2253
76
2187
77
2125
600
90
2680
89
2664
90
2578
90
2496
700
104
3095
102
3075
103
2969
104
2866
800
117
3517
115
3491
116
3362
118
3237
900
131
3942
129
3909
130
3759
131
3612
1000
145
4366
142
4327
143
4157
145
3989
1100
158
4791
156
4746
157
4555
159
4367
1200
172
5215
169
5164
170
4953
173
4744
1300
186
5641
182
5582
184
5351
186
5121
1400
199
6076
196
6006
198
5750
200
5499
1500
213
6512
209
6430
211
6153
214
5880
1600
227
6947
223
6855
225
6556
228
6265
1700
240
7382
236
7279
239
6960
242
6649
1800
254
7817
250
7703
253
7363
256
7034
1900
268
8252
264
8127
266
7766
270
7419
2000
281
8688
277
8552
280
8169
285
7804
2100
295
9123
291
8976
294
8573
299
8189
2200
308
9558
304
9400
308
8976
313
8573
2300
322
9993
318
9824
321
9379
327
8958
2400
335
9782
341
9343
2500
349
10,186
355
9728
2600
369
10,112
2700
ISA + 20
C
High Altitude
Arrival Weight 20,000 lb
NOTE:
Shaded areas are to be used for interpolation purposes.
8XC078-1
Содержание Hawker 800XP
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