Hawker Beechcraft Hawker 800XP, Руководство по эксплуатации для пилотов, Страница: 668 / 923

Page 6-5
Pilot’s Operating Manual
P/N 140-590032-0007
Revision A4: Sep, 2010 Section IV Sub-section 6
SINGLE ENGINE
SINGLE ENGINE
NOTE: These altitudes are determined with the operative engine running at
Maximum Continuous Thrust.
SINGLE ENGINE MINIMUM CRUISE SPEED and
MAXIMUM CRUISE ALTITUDE
TEMPERATURE RELATIVE TO ISA
°
C
-15 -10 -5 0 +5 +10 +15 +20
MINIMUM
CRUISE
WEIGHT lb
SPEED
KIAS
MAXIMUM CRUISE ALTITUDE ft
26,000 210 25,800 25,200 23,900 22,500 21,400 20,300 18,800 16,700
25,000 206 26,800 26,200 25,100 23,700 22,500 21,600 20,100 18,300
24,000 202 27,800 27,400 26,300 25,000 23,800 22,800 21,400 19,900
23,000 198 28,700 28,500 27,500 26,300 25,000 23,900 22,600 21,300
22,000 194 29,700 29,500 28,700 27,600 26,200 25,100 23,800 22,600
21,000 189 30,700 30,500 29,800 29,000 27,500 26,300 25,000 23,800
20,000 185 31,600 31,500 30,900 30,200 28,800 27,500 26,200 25,000
19,000 180 32,500 32,400 32,000 31,500 30,300 28,900 27,500 26,300
18,000 175 33,400 33,300 33,000 32,600 31,700 30,500 28,800 27,700
8XC172