
Page 6-1
Pilot’s Operating Manual
P/N 140-590032-0007
Revision A4: Sep, 2010
Section IV
FLIGHT PLANNING DATA
Sub-section 6
SINGLE ENGINE
Table of Contents
Page
INTRODUCTION ......................................................................................... 6-3
SINGLE ENGINE CEILING ...................................................................... 6-3
SINGLE ENGINE DRIFT DOWN .............................................................. 6-3
SINGLE ENGINE CRUISE ....................................................................... 6-4
SINGLE ENGINE MAXIMUM CONTINUOUS THRUST
FOR DESCENT AND CRUISE................................................................. 6-4
SINGLE ENGINE......................................................................................... 6-5
SINGLE ENGINE MINIMUM CRUISE SPEED and
MAXIMUM CRUISE ALTITUDE ............................................................... 6-5
SINGLE ENGINE MAXIMUM CRUISE WEIGHT ..................................... 6-6
SINGLE ENGINE LONG RANGE CRUISE SPEED ................................. 6-6
SUMMARY of SINGLE ENGINE CEILINGS............................................... 6-7
OBSTACLE CLEARANCE ......................................................................... 6-8
RANGE AFTER ENGINE FAILURE ........................................................... 6-9
SINGLE ENGINE DRIFT DOWN............................................................... 6-10
ISA -15° C............................................................................................... 6-10
ISA -10° C............................................................................................... 6-12
ISA .......................................................................................................... 6-14
ISA +10° C .............................................................................................. 6-16
ISA +20° C .............................................................................................. 6-18
SINGLE ENGINE LONG RANGE CRUISE............................................... 6-20
11,000 ft.................................................................................................. 6-20
13,000 ft.................................................................................................. 6-21
15,000 ft.................................................................................................. 6-22
17,000 ft.................................................................................................. 6-23
19,000 ft.................................................................................................. 6-24
21,000 ft.................................................................................................. 6-25
23,000 ft.................................................................................................. 6-26
25,000 ft.................................................................................................. 6-27
27,000 ft.................................................................................................. 6-28
SINGLE ENGINE HOLDING - FUEL FLOW
ENGINE ANTICE OFF............................................................................... 6-29
Содержание Hawker 800XP
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