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SECTION 4
NORMAL PROCEDURES
PIPER AlRCRAFf CORPORATION
PA-28R-201, ARROW
4.9
PREFLIGHT CHECK (4.5a) (continued)
4.9b
Right Wing (4.5a) (continued)
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.
CAUTION
When draining any amount of fuel, care should
be taken to ensure that no fire hazard exists
before starting engine.
Drain a fuel sample from the fuel
tank
into a container, through the quick
drain located at the lower inboard rear comer of the
tank.
Make sure that
enough fuel has been drained to ensure that all water and sediment is removed;
check for proper fuel. The fuel system should be dmined daily prior to the first
flight and after each refueling.
Remove the tie down and chock.
Next, a complete check of the landing gear. Check the gear strut for proper
inflation, there should be 2.0
+/-
0.25 inches of strut exposure under a nonnal
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.
4.9c
Nose Section (4.Sa)
Check the general condition of the nose section and check for oil or fluid
leakage and that the cowling is secure. Check the oil level; make sure that the
dipstick has been properly seated and the oil cap properly secured. Check the
engine baffle seals. 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.
Remove the chock and check the nose gear strut for proper inflation; there
should be 2.75
+/-
0.25 inches of strut exposure under a normal static load.
Check the tire for cuts, wear, and proper inflation.
I
REPORT: VB-1365
4-16
ISSUED: SEPTEMBER 15, 1988
REVISED; APRIL 9, 1990
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