Hawker Beechcraft Hawker 800XP, Руководство по эксплуатации для пилотов

Страница: 674 / 923

Page 6-11
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 -57 -57 -56 -56 -56 -55 -55 -55
TIME min 24 26 30 33 36 39 41 43
DISTANCE nm 117 129 148 168 184 198 210 221
FUEL USED lb 385 435 505 595 665 735 800 860
FINAL ALTITUDE ft 31,380 31,030 30,180 29,290 28,380 27,480 26,570 25,650
31,000
CONSTANT KIAS 189 194 198 202 206 210 214
IOAT AT START
°
C -53 -53 -53 -52 -52 -52 -51
TIME min 10 20 27 31 34 37 39
DISTANCE nm 47 101 134 157 174 189 202
FUEL USED lb 165 355 485 580 660 735 805
FINAL ALTITUDE ft 30,820 30,070 29,210 28,320 27,430 26,520 25,610
29,000
CONSTANT KIAS 198 202 206 210 214
IOAT AT START
°
C -49 -49 -49 -48 -48
TIME min 7 21 27 31 35
DISTANCE nm 34 102 135 158 176
FUEL USED lb 130 390 530 630 720
FINAL ALTITUDE ft 28,910 28,170 27,330 26,450 25,550
27,000
CONSTANT KIAS 206 210 214
IOAT AT START
°
C -45 -45 -45
TIME min 4 20 27
DISTANCE nm 20 98 134
FUEL USED lb 80 405 565
FINAL ALTITUDE ft 26,960 26,270 25,440
25,000
CONSTANT KIAS
IOAT AT START
°
C
TIME min
DISTANCE nm
FUEL USED lb
FINAL ALTITUDE ft
8XC177-2
ISA -15° 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.