Page 6-8
Section IV Sub-section 6
SINGLE ENGINE
P/N 140-590032-0007
Revision A4: Sep, 2010
Pilot’s Operating Manual
OBSTACLE CLEARANCE
Cruise Ceiling for Zero En Route Net Gradient
TEMPERATURE RELATIVE TO ISA
°
C
-15
-10
-5
0
+5
+10
+15
+20
CRUISE WEIGHT lb
MAXIMUM CRUISE ALTITUDE ft
29,000
17,300 16,300 15,100 13,800 12,500 10,900
9100
7100
11,000
9600
8200
7000
5500
3200
200
---
28,000
18,600 17,500 16,200 14,900 13,600 12,600 10,400
8500
12,300 11,100
9700
8400
7100
5200
2500
---
27,000
19,800 18,700 17,500 16,200 14,700 13,300 11,700
9800
13,800 12,600 11,200
9800
8400
6800
4500
1200
26,000
21,200 20,000 18,800 17,500 16,100 14,600 13,000 11,200
15,100 14,000 12,700 11,400 10,000
8300
6300
3700
25,000
22,000 21,000 19,800 18,500 17,200 15,600 14,000 12,100
16,300 15,200 14,100 12,700 11,500
9800
8100
5800
24,000
23,000 22,000 21,000 19,700 18,300 16,800 15,200 13,400
17,500 16,300 15,100 13,800 12,500 11,000
9300
7300
23,000
24,200 23,200 22,100 21,000 19,700 18,200 16,700 14,800
18,800 17,700 16,500 15,200 13,900 12,500 10,800
8900
22,000
25,200 24,100 23,200 22,200 21,000 19,600 18,000 16,200
20,000 18,800 17,700 16,400 15,100 13,600 12,100 10,100
21,000
26,300 25,500 24,500 23,500 22,300 21,000 19,500 17,700
21,300 20,200 19,000 17,700 16,500 15,100 13,600 11,800
20,000
27,500 26,600 25,700 24,700 23,700 22,500 21,000 19,400
23,000 21,900 20,700 19,500 18,200 16,700 15,200 13,400
19,000
28,600 27,800 27,000 26,000 24,800 23,600 22,300 20,700
24,400 23,400 22,300 21,100 19,800 18,300 16,700 14,800
18,000
29,800 29,100 28,300 27,500 26,400 25,200 24,000 22,600
26,100 25,000 23,800 22,700 21,400 20,000 18,500 16,700
NOTES:
1.
With ENGINE ANTICE ON use shaded values.
2.
These altitudes are based upon Airplane Flight Manual Fig. 5.40.1.
8XC176
Содержание Hawker 800XP
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