Page 6-17
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
-31
-31
-30
-30
-30
-29
-29
-28
TIME min
41
44
47
50
53
56
59
62
DISTANCE nm
201
219
234
251
268
284
300
316
FUEL USED lb
675
750
825
905
990
1075
1160
1250
FINAL ALTITUDE ft
28,300
27,080 25,900
24,750 23,600
22,490 21,360
20,200
31,000
CONSTANT KIAS
185
189
194
198
202
206
210
214
IOAT AT START
°
C
-28
-28
-27
-27
-26
-26
-26
-25
TIME min
34
39
43
46
50
53
56
59
DISTANCE nm
168
192
211
231
250
267
284
300
FUEL USED lb
575
675
760
850
940
1030
1120
1215
FINAL ALTITUDE ft
28,220
27,020 25,840
24,700 23,560
22,450 21,320
20,170
29,000
CONSTANT KIAS
185
189
194
198
202
206
210
214
IOAT AT START
°
C
-25
-24
-24
-23
-23
-23
-22
-22
TIME min
23
32
37
42
46
50
53
57
DISTANCE nm
112
154
183
207
228
248
265
284
FUEL USED lb
400
555
670
775
875
975
1065
1165
FINAL ALTITUDE ft
28,070
26,920 25,770
24,640 23,510
22,400 21,280
20,130
27,000
CONSTANT KIAS
189
194
198
202
206
210
214
IOAT AT START
°
C
-21
-20
-20
-20
-19
-19
-19
TIME min
15
28
35
41
45
49
53
DISTANCE nm
74
135
172
199
223
243
263
FUEL USED lb
275
510
660
785
895
995
1105
FINAL ALTITUDE ft
26,660 25,630
24,540 23,430
22,340 21,220
20,080
25,000
CONSTANT KIAS
198
202
206
210
214
IOAT AT START
°
C
-17
-16
-16
-16
-15
TIME min
22
32
38
44
48
DISTANCE nm
105
154
188
214
238
FUEL USED lb
415
620
770
895
1015
FINAL ALTITUDE ft
24,320 23,300
22,240 21,140
20,010
8XC180-2
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.
Содержание Hawker 800XP
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