Piper WARRIOR III PA-28-161, Руководство по эксплуатации для пилотов

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RIGHT WING
Begin the walk-around at the trailing edge of the right wing by checking
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 and 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.
Drain the fuel tank through the quick drain located at the lower
inboard rear corner of the tank, making sure that enough fuel has been
drained to insure that all water and sediment is removed. The fuel system
should be drained daily prior to the first flight and after each refueling and
checked for proper fuel.
CAUTION
When draining any amount of fuel, care should
be taken to insure that no fire hazard exists
before starting engine.
Remove the tie down and chock.
Next, a check of the landing gear. Check the gear strut for proper
inflation; there should be 4.50± .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.
Check that the fresh air inlet is clear of foreign matter.
NOSE SECTION
Check the general condition of the nose section, look for oil or fluid
leakage and that the cowling is secure. Check the windshield and clean if
necessary. The propeller and spinner should be checked for detrimental nicks,
cracks, or other defects. The air inlets should be clear of obstructions and
check the alternator belt for proper tension. The landing light should be clean
and intact.
RIGHT WING
Begin the walk-around at the trailing edge of the right wing by checking
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 and 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.
Drain the fuel tank through the quick drain located at the lower
inboard rear corner of the tank, making sure that enough fuel has been
drained to insure that all water and sediment is removed. The fuel system
should be drained daily prior to the first flight and after each refueling and
checked for proper fuel.
CAUTION
When draining any amount of fuel, care should
be taken to insure that no fire hazard exists
before starting engine.
Remove the tie down and chock.
Next, a check of the landing gear. Check the gear strut for proper
inflation; there should be 4.50± .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.
Check that the fresh air inlet is clear of foreign matter.
NOSE SECTION
Check the general condition of the nose section, look for oil or fluid
leakage and that the cowling is secure. Check the windshield and clean if
necessary. The propeller and spinner should be checked for detrimental nicks,
cracks, or other defects. The air inlets should be clear of obstructions and
check the alternator belt for proper tension. The landing light should be clean
and intact.
PIPER AIRCRAFT CORPORATION SECTION 4
PA-28-161, WARRIOR III NORMAL PROCEDURES
PIPER AIRCRAFT CORPORATION SECTION 4
PA-28-161, WARRIOR III NORMAL PROCEDURES
ISSUED: JULY 1, 1994 REPORT: VB-1565
4-13
ISSUED: JULY 1, 1994 REPORT: VB-1565
4-13