Page 6-16
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
IOAT AT START
°
C
-34
-33
-33
-32
TIME min
54
56
58
60
DISTANCE nm
277
286
297
309
FUEL USED lb
855
905
960
1030
FINAL ALTITUDE ft
28,440
27,210 26,010
24,850
39,000
CONSTANT KIAS
185
189
194
198
202
206
IOAT AT START
°
C
-35
-34
-34
-33
-33
-32
TIME min
52
54
56
58
60
63
DISTANCE nm
263
274
284
297
312
326
FUEL USED lb
825
880
940
1005
1085
1165
FINAL ALTITUDE ft
28,420
27,190
25,990
24,840
23,670
22,560
37,000
CONSTANT KIAS
185
189
194
198
202
206
210
214
IOAT AT START
°
C
-36
-35
-35
-35
-34
-34
-33
-33
TIME min
49
51
53
56
58
61
64
66
DISTANCE nm
246
258
270
283
298
313
328
342
FUEL USED lb
790
850
910
980
1060
1140
1225
1310
FINAL ALTITUDE ft
28,390
27,160 25,970
24,810 23,650
22,540 21,410
20,250
35,000
CONSTANT KIAS
185
189
194
198
202
206
210
214
IOAT AT START
°
C
-35
-34
-34
-33
-33
-32
-32
-31
TIME min
45
48
50
53
56
59
61
64
DISTANCE nm
226
240
253
268
284
299
314
329
FUEL USED lb
740
805
870
945
1030
1110
1195
1285
FINAL ALTITUDE ft
28,350
27,130 25,940
24,780 23,630
22,520 21,380
20,230
8XC180-1
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.
Содержание Hawker 800XP
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