Hawker Beechcraft Hawker 800XP, Руководство по эксплуатации для пилотов

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Page 1-7
Pilot’s Operating Manual
Original Issue: Feb, 2002
Sub-section 1
GENERAL
Hawker 800XP Pro Line 21
Section IV - FLIGHT PLANNING DATA
CEILING DATA
NOTE: These weights and altitudes are determined by either the maximum altitude of 41,000 ft,
or by a 200 ft/min rate of climb limit at M = 0.7.
NOTE: These weights and altitudes are determined by either the maximum altitude of 41,000 ft,
or by a 200 ft/min rate of climb limit at M = 0.7.
MAXIMUM CRUISE ALTITUDE
TEMPERATURE RELATIVE TO ISA
°
C
-15 -10 -5 0 +5 +10 +15 +20
WEIGHT lb MAXIMUM CRUISE ALTITUDE ft
27,000 40,600 40,400 39,800 39,100 38,300 37,400 36,400 34,300
26,000 41,000 41,000 40,600 39,900 39,000 38,100 37,100 35,400
25,000 41,000 41,000 41,000 40,700 39,800 38,700 37,700 36,400
24,000 41,000 41,000 41,000 41,000 40,600 39,500 38,400 37,100
23,000 41,000 41,000 41,000 41,000 41,000 40,400 39,200 38,000
22,000 41,000 41,000 41,000 41,000 41,000 41,000 40,000 38,800
21,000 41,000 41,000 41,000 41,000 41,000 41,000 40,800 39,600
20,000 41,000 41,000 41,000 41,000 41,000 41,000 41,000 40,500
MAXIMUM CRUISE WEIGHT
TEMPERATURE RELATIVE TO ISA
°
C
-15 -10 -5 0 +5 +10 +15 +20
CRUISE
ALTITUDE ft
MAXIMUM CRUISE WEIGHT lb
35,000 26,400
36,000 25,500
37,000 26,100 24,100
38,000 26,100 24,600 22,900
39,000 25,900 24,600 23,200 21,700
40,000 26,700 25,900 24,800 23,500 22,000 20,600
41,000 26,400 26,300 25,400 24,700 23,600 22,300 20,700 19,300
Table 1
Table 2