Page 2-75
Pilot’s Operating Manual
Revision A1: Nov, 2002
Sub-section 2
PREFLIGHT
Hawker 800XP Pro Line 21
Section IV - FLIGHT PLANNING DATA
HIGH SPEED PROCEDURE
ALTITUDE
8000 ft
10,000 ft
15,000 ft
19,000 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
20
739
20
706
20
653
21
625
200
36
1424
36
1366
35
1247
35
1168
300
52
2108
51
2026
50
1842
49
1711
400
68
2792
67
2686
64
2436
63
2254
500
84
3482
83
3350
79
3032
77
2797
600
101
4172
98
4016
94
3632
91
3345
700
117
4861
114
4681
109
4232
105
3896
800
133
5554
130
5346
123
4832
119
4446
900
149
6255
145
6017
138
5432
133
4996
1000
165
6956
161
6689
153
6037
147
5547
1100
181
7657
176
7361
167
6643
162
6103
1200
197
8358
192
8034
182
7249
176
6659
1300
212
9063
206
8718
197
7855
190
7216
1400
225
9783
221
9409
211
8460
204
7772
1500
235
10,103
226
9066
218
8326
1600
240
9672
232
8878
1700
246
9429
1800
260
9981
ISA + 10
C
Low Altitude
Arrival Weight 20,000 lb
NOTE:
Shaded areas are to be used for interpolation purposes.
8XC030A-1
Содержание Hawker 800XP
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