Hawker Beechcraft Hawker 800XP, Руководство по эксплуатации для пилотов, Страница: 365 / 923

Page 1-8
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.
MAXIMUM TAKE-OFF WEIGHT for CRUISE ALTITUDE
TEMPERATURE RELATIVE TO ISA
°
C
-15 -10 -5 0 +5 +10 +15 +20
CRUISE
ALTITUDE ft
MAXIMUM TAKE-OFF WEIGHT lb
35,000 28,000
36,000 27,100
37,000 27,500 25,600
38,000 27,400 25,900 24,300
39,000 27,100 25,800 24,500 23,000
40,000 27,800 27,100 26,000 24,700 23,200 21,900
41,000 27,500 27,400 26,500 25,800 24,700 23,400 21,900 20,500
Table 3