Page 4-8
Pilot’s Operating Manual
Original Issue: Feb, 2002
Sub-section 4
CRUISE - ENROUTE
Hawker 800XP Pro Line 21
Section IV - FLIGHT PLANNING DATA
HIGH SPEED CRUISE
TEMPERATURE RELATIVE TO ISA C
CRUISE
WEIGHT
lb
-15
-10
-5
0
+5
+10
+15
+20
AMBIENT TEMP C
-22
-17
-12
-7
-2
3
8
13
IOAT C
-9
-4
2
7
12
17
23
28
18,000
KTAS
373
377
381
384
388
391
395
398
TOTAL FUEL FLOW
lb/hr
2329
2360
2393
2425
2456
2487
2517
2547
KIAS
335
335
335
335
335
335
335
335
KTAS
373
377
381
384
388
391
395
398
20,000
TOTAL FUEL FLOW
lb/hr
2342
2373
2407
2439
2470
2500
2531
2561
KIAS
335
335
335
335
335
335
335
335
KTAS
373
377
381
384
388
391
395
398
22,000
TOTAL FUEL FLOW
lb/hr
2358
2389
2423
2455
2487
2516
2547
2578
KIAS
335
335
335
335
335
335
335
335
KTAS
373
377
381
384
388
391
395
398
24,000
TOTAL FUEL FLOW
lb/hr
2374
2406
2440
2472
2504
2534
2565
2596
KIAS
335
335
335
335
335
335
335
335
KTAS
313
316
319
322
325
328
331
334
26,000
TOTAL FUEL FLOW
lb/hr
1832
1855
1880
1905
1929
1953
1977
2002
KIAS
280
280
280
280
280
280
280
280
KTAS
313
316
319
322
325
328
331
334
27,000
TOTAL FUEL FLOW
lb/hr
1847
1871
1896
1921
1946
1970
1995
2019
KIAS
280
280
280
280
280
280
280
280
NOTE:
V
MO
is limited to the ventral tank full speed at higher weights.
8XC115
11,000 ft
Содержание Hawker 800XP
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