Page 2-176
Pilot’s Operating Manual
Revision A1: Nov, 2002
Sub-section 2
PREFLIGHT
Hawker 800XP Pro Line 21
Section IV - FLIGHT PLANNING DATA
LONG RANGE 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
39
1006
38
1004
37
1008
37
1013
300
56
1377
54
1362
53
1353
52
1354
400
73
1748
71
1719
69
1699
68
1696
500
90
2119
87
2077
85
2044
83
2038
600
107
2499
104
2440
101
2395
98
2383
700
124
2879
120
2806
117
2751
114
2734
800
141
3259
137
3172
133
3107
129
3086
900
158
3641
153
3537
149
3463
145
3437
1000
175
4032
170
3912
165
3826
160
3794
1100
192
4422
186
4289
181
4194
175
4159
1200
209
4813
203
4665
197
4562
191
4523
1300
226
5203
220
5004
212
4930
206
4887
1400
243
5593
238
5337
228
5298
221
5251
1500
260
5984
256
5690
244
5666
237
5616
1600
277
6374
275
6074
260
6034
252
5980
1700
294
6764
292
6463
276
6402
268
6344
1800
311
7155
309
6845
292
6770
283
6708
1900
328
7545
326
7215
308
7139
298
7072
2000
345
7936
342
7580
324
7507
314
7437
2100
358
7948
340
7875
329
7801
2200
356
8243
344
8165
2300
2400
ISA
High Altitude
Arrival Weight 23,000 lb
NOTE:
Shaded areas are to be used for interpolation purposes.
8XC088-1
Содержание Hawker 800XP
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