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PIPER AIRCRAFT CORPORATION
PA-28R-20I, ARROW
SECTION 4
NORMAL PROCEDURES
4.7
AMPLIFIED NORMAL PROCEDURES (GENERAL)
The following paragraphs are provided to supply detailed information
and explanations of the normal procedures necessary for the safe operation
of the airplane.
4.9 PREFLIGHT CHECK (4.5a)
The airplane should be given a thorough preflight and walk-around
check. the preflight should include a check of the airplane's operational
status, computation of weight and e.G. limits, takeoff and landing
distances, and in-flight performance. A weather briefing should be obtained
for the intended flight path. and any other factors relating to a safe flight
should be cJ:iecked before takeoff.
4.9a Cockpit (4.5a)
CAUTION
The flap position should be noted before
boarding the airplane. The flaps must be placed
in the UP position before they will lock and
support weight on the step.
Upon entering the cockpit. release the seat belts securing the control
wheel. Check that the landing gear selector handle is in the DOWN position
and set the parking brake. Ensure that all avionics and electrical switches are
OFF. Check that the mixture is in the idle cut-off and the magneto switch is
OFF. Turn ON the battery master (BATT MASTR) switch; check the fuel
quantity gauges for adequate supply and check that the annunciator panel
illuminates. Turn OFF the battery master (BATT MASTR) switch. Check
the primary flight controls and flaps for proper operation and set the trim to
neutral. Open the pitot and static drains to remove any moisture that has
accumulated in the lines. Check the windows for cleanliness and that the
required papers and POH are on board. Properly stow the tow bar and
baggage and secure. Close and secure the baggage door.
4.9b Right Wing (4.5a)
Begin the wal k-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.
ISSUED: SEPTEMBER 15, 1988
REPORT: VB-1365
4-15
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