Hawker Beechcraft Hawker 800XP, Руководство по эксплуатации для пилотов

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Section IV Sub-section 6
SINGLE ENGINE
P/N 140-590032-0007
Revision A4: Sep, 2010
Pilot’s Operating Manual
SINGLE ENGINE DRIFT DOWN
ALTITUDE ft
AT ENGINE
FAILURE
WEIGHT lb
AT ENGINE
FAILURE
20,000 21,000 22,000 23,000 24,000 25,000 26,000 27,000
41,000
CONSTANT KIAS 185 189 194 198
IOAT AT START
°
C -34 -33 -33 -32
TIME min 54 56 58 60
DISTANCE nm 277 286 297 309
FUEL USED lb 855 905 960 1030
FINAL ALTITUDE ft 28,440 27,210 26,010 24,850
39,000
CONSTANT KIAS 185 189 194 198 202 206
IOAT AT START
°
C -35 -34 -34 -33 -33 -32
TIME min 52 54 56 58 60 63
DISTANCE nm 263 274 284 297 312 326
FUEL USED lb 825 880 940 1005 1085 1165
FINAL ALTITUDE ft 28,420 27,190 25,990 24,840 23,670 22,560
37,000
CONSTANT KIAS 185 189 194 198 202 206 210 214
IOAT AT START
°
C -36 -35 -35 -35 -34 -34 -33 -33
TIME min 49 51 53 56 58 61 64 66
DISTANCE nm 246 258 270 283 298 313 328 342
FUEL USED lb 790 850 910 980 1060 1140 1225 1310
FINAL ALTITUDE ft 28,390 27,160 25,970 24,810 23,650 22,540 21,410 20,250
35,000
CONSTANT KIAS 185 189 194 198 202 206 210 214
IOAT AT START
°
C -35 -34 -34 -33 -33 -32 -32 -31
TIME min 45 48 50 53 56 59 61 64
DISTANCE nm 226 240 253 268 284 299 314 329
FUEL USED lb 740 805 870 945 1030 1110 1195 1285
FINAL ALTITUDE ft 28,350 27,130 25,940 24,780 23,630 22,520 21,380 20,230
8XC180-1
ISA +10° C
These ceilings are based on average performance at Maximum Continuous Thrust and a constant
drift down KIAS (minimum cruise speed at start of drift down weight).
To check obstacle clearance use the EN ROUTE NET GRADIENT in the Airplane Flight Manual which
will give a lower ceiling than the final drift down altitudes below.