Hawker Beechcraft Hawker 800XP, Руководство по эксплуатации для пилотов

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Page 2-6
Pilot’s Operating Manual
Revision A1: Nov, 2002
Sub-section 2
ABNORMAL HANDLING
Hawker 800XP Pro Line 21
Section V - FLIGHT HANDLING
CRUISE WITH ONE ENGINE INOPERATIVE
Performance data for Single Engine Operation can be found in Section IV - FLIGHT PLANNING DATA
Sub-section 6.
If an engine fails, thrust may be increased up to maximum continuous on the operating engine, to
minimize the loss of speed and altitude.
The recommended Long Range cruising speed, provided in Section IV - FLIGHT PLANNING DATA
Sub-section 4 gives best range at a fixed altitude. However, it will be an advantage to frequently reduce
the speed to the minimum cruising KIAS in order to reduce the loss of altitude.
This minimum speed is the same as that given for all engine operation and should be used only until
the airplane can accelerate to the Long Range speed.
If obstacle clearance is most important, the en-route climb speed will give the minimum gradient of
descent and the best ceiling, but it is too slow for Long Range operation. Therefore, the general
procedure is to increase power to maximum continuous and maintain altitude while speed falls to the
minimum cruising speed. The airplane will then drift down to the single engine cruise ceiling.
When a satisfactory cruise altitude is established, allow the speed to rise to the Long Range KIAS or
higher if range is not critical.
MAXIMUM PERMISSIBLE SPEED
NOTE: The following procedures apply when the airplane is used solely for the purpose of pilot
training or routine test flights with no passengers on board.
FLIGHTS IN EXCESS OF M
MO
/V
MO
It is permissible, for the purpose of pilot training or routine test flights, to exceed V
MO
or M
MO
(as stated
in the AFM, Section 2) provided the following conditions are observed:
• Passengers are not carried.
• There is no significant turbulence.
• The maximum airspeed is an indicated Mach number of 0.82, at an altitude of at least 30,000 feet
with wings level and no applied "G".
• The maximum airspeed does not exceed V
MO
by more than 20 KIAS, at an altitude of no more than
20,000 feet.
Commence the maneuver in level flight by selecting maximum continuous power and gently lower the
nose if necessary. Recovery action is to reduce power to idle, extend the airbrakes and execute a gentle
pull up.
If a Mach number greater than 0.82 indicated or an airspeed of greater than 20 KIAS above V
MO
is
inadvertently achieved, or if any airframe or aileron buffet is encountered, take recovery action
immediately.