Hawker Beechcraft Hawker 800XP, Руководство по эксплуатации для пилотов, Страница: 678 / 923

Page 6-15
Pilot’s Operating Manual
P/N 140-590032-0007
Revision A4: Sep, 2010 Section IV Sub-section 6
SINGLE ENGINE
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
33,000
CONSTANT KIAS 185 189 194 198 202 206 210 214
IOAT AT START
°
C -42 -41 -41 -40 -40 -40 -39 -39
TIME min 35 35 40 44 47 50 53 55
DISTANCE nm 172 178 204 225 242 258 270 282
FUEL USED lb 575 605 710 805 885 965 1040 1110
FINAL ALTITUDE ft 29,880 29,690 28,520 27,270 26,000 24,730 23,510 22,370
31,000
CONSTANT KIAS 185 189 194 198 202 206 210 214
IOAT AT START
°
C -38 -38 -38 -37 -37 -36 -36 -36
TIME min 25 27 34 39 43 47 50 52
DISTANCE nm 123 135 172 198 218 237 252 265
FUEL USED lb 425 470 610 725 820 910 985 1065
FINAL ALTITUDE ft 29,750 29,560 28,420 27,190 25,940 24,680 23,470 22,330
29,000
CONSTANT KIAS 194 198 202 206 210 214
IOAT AT START
°
C -34 -34 -33 -33 -33 -32
TIME min 22 31 37 42 45 48
DISTANCE nm 109 156 187 211 229 245
FUEL USED lb 400 585 715 825 915 1005
FINAL ALTITUDE ft 28,190 27,050 25,840 24,600 23,410 22,280
27,000
CONSTANT KIAS 198 202 206 210 214
IOAT AT START
°
C -30 -30 -30 -29 -29
TIME min 15 27 35 40 44
DISTANCE nm 72 136 174 199 220
FUEL USED lb 280 535 700 815 920
FINAL ALTITUDE ft 26,680 25,660 24,480 23,330 22,210
25,000
CONSTANT KIAS
IOAT AT START
°
C
TIME min
DISTANCE nm
FUEL USED lb
FINAL ALTITUDE ft
8XC179-2
ISA
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.