Piper PA-28-161 User Manual

PIPER AIRCRAFT CORPORATION
PA-28-161, WARRIOR II
RIGHT WING
SECTION 4
NORMAL PROCEDURES
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 svstem
should be drained daily prior to the first flight and after each refuelin-g 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 !luid
leakage and that the cowling is secure. Check the windshield and clean if
necessary.
The propeller and spinner should he checked for detrimental
nicks, cracb. or other defects. The air inkts should be clear of obstructions
and check the alternator belt for proper tension. The landing light should be
clean and intact.
ISSllED: AUGUST 13, 1982
REVISED: JUNE 28, 1984
REPORT: VB-1180
4-13

Piper PA-28-161 Specifications

General

Manufacturer	Piper Aircraft
Model	PA-28-161 Warrior II
Engine	Lycoming O-320-D3G
Horsepower	160 hp
Seating Capacity	4
Wingspan	35 ft (10.7 m)
Length	24 ft 0 in
Maximum Speed	127 knots
Cruise Speed	122 knots
Maximum Takeoff Weight	2, 325 lb (1, 055 kg)
Fuel Capacity	48 US gallons (182 L)