Hawker Beechcraft Hawker 800XP, Руководство по эксплуатации для пилотов

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Page 2-3
Pilot’s Operating Manual
Revision A1: Nov, 2002
Sub-section 2
ABNORMAL HANDLING
Hawker 800XP Pro Line 21
Section V - FLIGHT HANDLING
SLIPPERY RUNWAYS
The following information is provided for operation on runways which are either:
(a) Covered by compacted snow.
or
(b) Expected to have very low braking action due to the presence of wet ice.
Compacted snow is snow which has been compressed into a solid mass which resists further
compression and will hold together or break into lumps if picked up.
LANDING
For unfactored landing distances on compacted snow and wet ice, refer to the Airplane Flight Manual.
Obtain the landing distance required for the intended landing weight and compare it with the runway
length available. Then decide whether the safety margin is adequate taking into account the weather
and the possible consequence of an overrun or undershoot.
Landing downhill or with a tailwind on a slippery runway should be avoided. The limiting combinations
of wind and runway gradient are shown in the Airplane Flight Manual. Combinations of wind and
gradient lying in the shaded area are not permitted.
Reverse thrust should be used if available, but forward idle thrust should be selected if directional
control becomes difficult. If reverse thrust is not being used, deceleration will be assisted by shutting
down either engine after normal selection of lift dump.
NOTE: In a crosswind the downwind engine should be shut down.
OPERATION IN HIGH SURFACE TAILWIND
When the reported wind speed at a height of 33 ft (10 m) exceeds 20 knots and has a tail component,
70% N
1
should not be exceeded except during takeoff.
For takeoff, the brakes should be released before 70% N
1
is reached and the thrust levers advanced
smoothly so that the full thrust is achieved at an airspeed of approximately 15 knots.
REJECTED TAKEOFF BEFORE V
1
Apply maximum braking using anti-skid, close both thrust levers, select airbrakes OPEN and select
reverse idle.
It is recommended that both thrust reversers are deployed even if takeoff has been abandoned for
actual or suspected engine failure, but that power is not increased above reverse idle on a
malfunctioning engine.