Hawker Beechcraft Hawker 800XP, Руководство по эксплуатации для пилотов, Страница: 676 / 923

Page 6-13
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 -52 -52 -51 -51 -51 -50 -50 -49
TIME min 25 27 30 35 39 42 44 47
DISTANCE nm 121 134 151 178 197 214 229 243
FUEL USED lb 400 450 520 630 720 795 875 950
FINAL ALTITUDE ft 31,280 30,940 30,080 29,130 28,120 27,100 26,080 25,050
31,000
CONSTANT KIAS 185 189 194 198 202 206 210 214
IOAT AT START
°
C -49 -48 -48 -48 -47 -47 -47 -46
TIME min 4 11 21 29 34 37 41 43
DISTANCE nm 20 56 106 145 170 190 208 224
FUEL USED lb 70 195 380 525 635 725 815 895
FINAL ALTITUDE ft 30,960 30,750 29,980 29,040 28,050 27,050 26,030 25,010
29,000
CONSTANT KIAS 198 202 206 210 214
IOAT AT START
°
C -44 -44 -44 -43 -43
TIME min 12 24 30 35 39
DISTANCE nm 60 120 153 179 198
FUEL USED lb 225 460 600 715 810
FINAL ALTITUDE ft 28,750 27,900 26,940 25,950 24,940
27,000
CONSTANT KIAS 206 210 214
IOAT AT START
°
C -40 -40 -39
TIME min 14 25 31
DISTANCE nm 72 127 160
FUEL USED lb 295 525 670
FINAL ALTITUDE ft 26,660 25,790 24,830
25,000
CONSTANT KIAS 214
IOAT AT START
°
C -36
TIME min 16
DISTANCE nm 83
FUEL USED lb 360
FINAL ALTITUDE ft 24,560
8XC178-2
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.