Malibu Boats PA-46-310P, Руководство по эксплуатации для пилотов

Страница: 104 / 355

SECTION 4 PIPER AIRCRAFT CORPORATION
NORMAL PROCEDURES PA-46-310P, MALIBU
REPORT: VB-1300 ISSUED: JULY 1, 1986
4-24 REVISED: OCTOBER 31, 1997
Ensure that the battery and alternator switches are ON. Check that the
cabin pressurization controls are properly set. Check and set all of the flight
instruments as required. Check the fuel selector to make sure it is on the
proper tank (fullest). Ensure auxiliary fuel pump is OFF. Check all engine
gauges. The induction air should be in the PRIMARY position. Turn pitot,
stall warning, windshield, and propeller heat ON if necessary.
All seat backs should be erect. Seats should be adjusted and locked in
position.
The mixture and propeller control levers should be set, and the seat belts
and shoulder harnesses should be fastened. Fasten the seat belts snugly
around the empty seats.
Exercise and set the flaps and trim. Ensure proper flight control move-
ment and response. The door should be properly latched and the door ajar
annunciator light out. On air conditioned models, the air conditioner must
be OFF to ensure normal takeoff climb performance. Release the parking
brake.
4.23 TAKEOFF
NORMAL TECHNIQUE (See Chart, Section 5)
When the available runway length is well in excess of that required and
obstacle clearance is no factor, the normal takeoff technique may be used.
The flaps should be set in the retracted position and the pitch trim set slightly
aft of neutral. Align the airplane with the runway, apply full power, and
accelerate to 77 KIAS.
NOTE
Takeoffs are normally made with full throttle.
However, under some off standard conditions
manifold pressure and/or fuel flow indications
can exceed their indicated limits at full throttle.
Limit manifold pressure to 38 in. Hg maximum.
(See Section 7)
Apply back pressure to the control wheel to lift off, then control pitch
attitude as required to attain the desired climb speed. Retract the landing
gear when a straight-ahead landing on the runway is no longer possible.
NOTE
During landing gear operation it is normal for
t h e H Y D P U M P a n n u n c i a t o r l i g h t t o
illuminate until full system pressure is restored.
SECTION 4 PIPER AIRCRAFT CORPORATION
NORMAL PROCEDURES PA-46-310P, MALIBU
REPORT: VB-1300 ISSUED: JULY 1, 1986
4-24 REVISED: OCTOBER 31, 1997
Ensure that the battery and alternator switches are ON. Check that the
cabin pressurization controls are properly set. Check and set all of the flight
instruments as required. Check the fuel selector to make sure it is on the
proper tank (fullest). Ensure auxiliary fuel pump is OFF. Check all engine
gauges. The induction air should be in the PRIMARY position. Turn pitot,
stall warning, windshield, and propeller heat ON if necessary.
All seat backs should be erect. Seats should be adjusted and locked in
position.
The mixture and propeller control levers should be set, and the seat belts
and shoulder harnesses should be fastened. Fasten the seat belts snugly
around the empty seats.
Exercise and set the flaps and trim. Ensure proper flight control move-
ment and response. The door should be properly latched and the door ajar
annunciator light out. On air conditioned models, the air conditioner must
be OFF to ensure normal takeoff climb performance. Release the parking
brake.
4.23 TAKEOFF
NORMAL TECHNIQUE (See Chart, Section 5)
When the available runway length is well in excess of that required and
obstacle clearance is no factor, the normal takeoff technique may be used.
The flaps should be set in the retracted position and the pitch trim set slightly
aft of neutral. Align the airplane with the runway, apply full power, and
accelerate to 77 KIAS.
NOTE
Takeoffs are normally made with full throttle.
However, under some off standard conditions
manifold pressure and/or fuel flow indications
can exceed their indicated limits at full throttle.
Limit manifold pressure to 38 in. Hg maximum.
(See Section 7)
Apply back pressure to the control wheel to lift off, then control pitch
attitude as required to attain the desired climb speed. Retract the landing
gear when a straight-ahead landing on the runway is no longer possible.
NOTE
During landing gear operation it is normal for
t h e H Y D P U M P a n n u n c i a t o r l i g h t t o
illuminate until full system pressure is restored.
FOR REFERENCE ONLY
NOT FOR FLIGHT