Malibu Boats PA-46-310P, Pilot Operating Handbook

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SECTION 4 PIPER AIRCRAFT CORPORATION
NORMAL PROCEDURES PA-46-310P, MALIBU
REPORT: VB-1300 ISSUED: JULY 1, 1986
4-16
primary airspeed system static ports on the left and right side of the aft fuse-
lage and the alternate static port on the underside of the aft fuselage are
clear of obstructions. The elevator and rudder should be operational and
free from damage or interference of any type. Elevator and rudder static
wicks should be firmly attached and in good condition. Check the condition
of the tab and ensure that all hinges and push rods are sound and opera-
tional. If the tail has been tied down, remove the tie down rope.
RIGHT WING
Check that the wing surface and control surfaces are clear of ice, frost,
snow or other extraneous substances. Check the flap, aileron and hinges for
damage and operational interference. Static wicks should be firmly attached
and in good condition. Check the wing tip and lights for damage.
Open the fuel cap and visually check the fuel color. The quantity should
match the indication that was on the fuel quantity gauge. Replace cap
securely. The fuel tank vent should be clear of obstructions.
Remove the tie down and chock.
Next, complete a check of the landing gear. Check the gear strut for
proper inflation. There should be 2.5 +/- .25 inches of strut exposure under a
normal static load. Check the tire for cuts, wear, and proper inflation. Make
a visual check of the brake block and disc.
Drain the fuel tank sump through the quick drain located on the lower
surface of the wing just inboard of the gear well, making sure that enough
fuel has been drained to ensure that all water and sediment is removed. The
fuel system should be drained daily prior to the first flight and after each
refueling.
CAUTION
When draining any amount of fuel, care should
be taken to ensure that no fire hazard exists
before starting engine.
NOSE SECTION
Check the general condition of the nose section; look for oil or fluid
leakage and that the cowling is secure. Drain the fuel filter sump located on
the lower fuselage aft of the cowling. Check the windshield and clean if
SECTION 4 PIPER AIRCRAFT CORPORATION
NORMAL PROCEDURES PA-46-310P, MALIBU
REPORT: VB-1300 ISSUED: JULY 1, 1986
4-16
primary airspeed system static ports on the left and right side of the aft fuse-
lage and the alternate static port on the underside of the aft fuselage are
clear of obstructions. The elevator and rudder should be operational and
free from damage or interference of any type. Elevator and rudder static
wicks should be firmly attached and in good condition. Check the condition
of the tab and ensure that all hinges and push rods are sound and opera-
tional. If the tail has been tied down, remove the tie down rope.
RIGHT WING
Check that the wing surface and control surfaces are clear of ice, frost,
snow or other extraneous substances. Check the flap, aileron and hinges for
damage and operational interference. Static wicks should be firmly attached
and in good condition. Check the wing tip and lights for damage.
Open the fuel cap and visually check the fuel color. The quantity should
match the indication that was on the fuel quantity gauge. Replace cap
securely. The fuel tank vent should be clear of obstructions.
Remove the tie down and chock.
Next, complete a check of the landing gear. Check the gear strut for
proper inflation. There should be 2.5 +/- .25 inches of strut exposure under a
normal static load. Check the tire for cuts, wear, and proper inflation. Make
a visual check of the brake block and disc.
Drain the fuel tank sump through the quick drain located on the lower
surface of the wing just inboard of the gear well, making sure that enough
fuel has been drained to ensure that all water and sediment is removed. The
fuel system should be drained daily prior to the first flight and after each
refueling.
CAUTION
When draining any amount of fuel, care should
be taken to ensure that no fire hazard exists
before starting engine.
NOSE SECTION
Check the general condition of the nose section; look for oil or fluid
leakage and that the cowling is secure. Drain the fuel filter sump located on
the lower fuselage aft of the cowling. Check the windshield and clean if
FOR REFERENCE ONLY
NOT FOR FLIGHT