Hawker Beechcraft Hawker 800XP, Руководство по эксплуатации для пилотов

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Page 2-4
Pilot’s Operating Manual
Original Issue: Feb, 2002
Sub-section 2
ABNORMAL HANDLING
Hawker 800XP Pro Line 21
Section V - FLIGHT HANDLING
CONTINUED TAKEOFF (ENGINE FAILURE AFTER V
1
)
The APR system should automatically apply APR power which will be indicated by the APR green ON
legend being illuminated and, unless on the flat rating, a rise of N
1.
If the APR green ON legend remains
extinguished, immediately push the APR OVRD switch.
The use of aileron on the ground is effective in steering the airplane in the natural sense. In the event
of an engine failure before V
R
, aileron can be used instinctively to maintain wings level, and further
application will help minimize deviation. Rotate at V
R
.
In a continued takeoff after engine failure where field length or obstacle clearance is limiting, it is
important that airspeed rise during transition is kept to a minimum and that the initial climb is made at
an airspeed as close as possible to V
2
.
APR must be cancelled by pushing the APR ARM switch no more than five minutes after start of the
take-off roll.
ENGINE FAILURE AFTER LIFT-OFF
In the event of engine failure after lift-off, during the initial climb, airspeed should be held constant at
that obtained at the moment the failure is recognized. The thrust of the remaining engine should be
increased to maximum, if it is not already at that thrust, and both MAIN AIR VALVES selected to CLOSE.
APR must be cancelled and maximum continuous rating selected not more than five minutes after start
of the take-off roll.