PIPER
AIRCRAFT
CORPORATION
SECTION 8
PA-28-161,
WARRIOR
II
HANDLING,
SERV & MAINT
(5) Secure tie-down ropes to the wing tie-down rings and to the
tail skid
at
approximately 45-degree angles to the ground.
When using rope
of
non-synthetic material, leave sufficient
slack to avoid damage to the airptane should the ropes
contract.
CAUTION
Use
bowline knots, square knots or locked slip
knots.
Do
not use plain slip knots.
NOTE
Additional preparations for high winds include
using tie-down ropes from the landing gear
forks and securing the rudder.
(6)
lns~all
a pi tot head cover if available.
Be
sure to remove the
pitot head cover before flight.
(7) Cabin and baggage doors should be locked when the
airplane
is
unattended.
8.11
ENGINE
AIR
FILTER
The wet-type polyurethane foam air filter must
be
inspected
at
least once
every fifty hours. Under extremely adverse operating conditions, it may
be
necessary to inspect the filter more frequently. The filter
is
disposable and
inexpensive and a spare should
be
kept on hand for a rapid replacement.
(a) Removal
Of
Engine Air Filter
The filter
is
located in the lower right front
of
the engine
compartment
and
may
be
removed by the following procedure:
(I)
Open the right side
o~
the engine cowling.
(2}
Loosen each
of
the four quarter-turn fasteners securing the
air filter cover.
(3)
Separate the cover
and
remove the filter.
(
4)
Inspect the filter. If it
is
excessively dirty
or
shows any
damage, replace it immediately.
ISSUED:
AUGUST
13, 1982
REPORT:
VB-1180
8-7
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