Hawker Beechcraft Hawker 800XP, Руководство по эксплуатации для пилотов

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Page 6-19
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 -21 -20 -20 -20 -19 -19 -18 -18
TIME min 49 53 56 59 62 67 72 77
DISTANCE nm 239 258 275 292 310 331 357 381
FUEL USED lb 790 880 960 1050 1145 1255 1395 1540
FINAL ALTITUDE ft 26,500 24,520 23,370 22,200 20,980 19,710 18,320 16,820
31,000
CONSTANT KIAS 185 189 194 198 202 206 210 214
IOAT AT START
°
C -18 -17 -17 -16 -16 -16 -15 -15
TIME min 44 49 53 56 60 64 69 74
DISTANCE nm 214 238 256 275 294 316 342 367
FUEL USED lb 720 830 915 1005 1105 1220 1360 1510
FINAL ALTITUDE ft 26,440 24,480 23,330 22,160 20,940 19,670 18,280 16,790
29,000
CONSTANT KIAS 185 189 194 198 202 206 210 214
IOAT AT START
°
C -14 -14 -13 -13 -13 -12 -12 -12
TIME min 37 44 49 52 56 61 66 72
DISTANCE nm 179 213 235 255 276 299 326 352
FUEL USED lb 620 760 855 955 1055 1175 1320 1470
FINAL ALTITUDE ft 26,340 24,430 23,280 22,110 20,900 19,630 18,240 16,750
27,000
CONSTANT KIAS 185 189 194 198 202 206 210 214
IOAT AT START
°
C -11 -10 -10 -10 -9 -9 -9 -8
TIME min 24 37 43 48 52 57 63 69
DISTANCE nm 116 178 206 230 254 279 308 335
FUEL USED lb 410 650 770 880 990 1120 1270 1425
FINAL ALTITUDE ft 26,150 24,340 23,210 22,050 20,840 19,580 18,190 16,690
25,000
CONSTANT KIAS 189 194 198 202 206 210 214
IOAT AT START
°
C -7 -7 -6 -6 -6 -5 -5
TIME min 24 34 41 47 53 59 65
DISTANCE nm 113 163 197 226 256 286 315
FUEL USED lb 425 625 770 900 1050 1205 1365
FINAL ALTITUDE ft 24,200 23,080 21,950 20,760 19,500 18,120 16,630
8XC181-2
ISA +20° 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.