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 185 189 194 198 202 206 210 214
IOAT AT START
°
C -55 -54 -54 -53 -53 -52 -52 -51
TIME min 41 42 43 47 49 51 53 55
DISTANCE nm 208 217 226 244 258 271 282 293
FUEL USED lb 615 660 705 790 860 930 995 1060
FINAL ALTITUDE ft 31,430 31,080 30,210 29,250 28,240 27,210 26,180 25,140
39,000
CONSTANT KIAS 185 189 194 198 202 206 210 214
IOAT AT START
°
C -56 -56 -55 -55 -54 -54 -53 -53
TIME min 38 40 41 45 47 49 51 53
DISTANCE nm 193 202 211 231 246 259 271 283
FUEL USED lb 590 630 675 765 835 905 975 1045
FINAL ALTITUDE ft 31,410 31,060 30,190 29,230 28,220 27,190 26,160 25,120
37,000
CONSTANT KIAS 185 189 194 198 202 206 210 214
IOAT AT START
°
C -57 -56 -56 -56 -55 -55 -54 -54
TIME min 35 37 38 42 45 47 49 51
DISTANCE nm 176 185 196 217 232 247 259 271
FUEL USED lb 550 590 640 730 805 880 950 1020
FINAL ALTITUDE ft 31,380 31,030 30,160 29,210 28,190 27,170 26,140 25,110
35,000
CONSTANT KIAS 185 189 194 198 202 206 210 214
IOAT AT START
°
C -55 -55 -55 -54 -54 -53 -53 -53
TIME min 31 33 35 39 42 45 47 49
DISTANCE nm 154 165 177 200 217 232 245 258
FUEL USED lb 495 540 595 690 770 845 915 990
FINAL ALTITUDE ft 31,350 31,000 30,130 29,180 28,160 27,140 26,110 25,080
8XC178-1
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.