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Piper PA-28-161 Maintenance Manual

Piper PA-28-161
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PIPER AIRCRAFT, INC.
PA-28-161, WARRIOR III
MAINTENANCE MANUAL
PAGE 2
Nov 30/06
1E2
5-50-00
2. Engine
Ov
ertemp, Loss of Oil, or Sudden Stoppage
Item Inspection Inspection Interval
Engine. See latest revisions of appropriate Each occurrence,
Textron-Lycoming Service Bulletins before further flight.
and Overhaul Manual.
Propeller. Refer to latest Sensenich Repair Manual. Each occurrence,
(Sudden Stoppage only.) Remove and recondition before before further flight.
return to service, if required.
Engine Mount and Inspect for distortion and Each occurrence,
Attachments. damage. Replace or repair before further flight.
as required.
3. Severe Turbulence, Hard or Overweight Landing
CAUTION: MINOR OR APPARENTLY SUPERFICIAL DAMAGE MAY INDICATE A MORE SEVERE
CONDITION SOMEWHERE ELSE IN THE STRUCTURE.
A. Place aircraft in a normal level attitude.
B. Make a preliminary inspection of checking alignment and out-of-track condition of engine, wings,
tail, landing gear and doors.
C. Follow Piper and Textron-Lycoming Maintenance Manual procedures. If there are any questions
regarding repairs or procedures, contact your Piper Dealer’s Service Advisor (DSA).
D. Inspect the following items closely to determine the extent of damage:
Item Inspection Inspection Interval
Landing Gear Struts. Cracks, signs of overstress Each occurrence,
(Not required for deformation, loose or damaged before further flight.
severe turbulence.) strut housings. Axles for cracks,
bending or flat spots. Damaged oleos
and seals, hydraulic leaks and landing
gear alignment.
Wheels, Tires, Brakes. Cracks, chips, loose or cracked Each occurrence,
(Not required for mounting bolts, alignment of slippage before further flight.
severe turbulence.) marks, sidewall distress, hydraulic or
air leaks. Inspect the wheels (dye
penetrant method) and wheel bolts
(magnetic particle method).
Landing Gear attach Buckling, cracks, overstress, and Each occurrence,
points. (Not required for wing skin buckling damage before further flight.
severe turbulence.) and condition. Inspect landing
gear attachment bolts
(magnetic particle method).

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Piper PA-28-161 Specifications

General IconGeneral
ManufacturerPiper Aircraft
ModelPA-28-161 Warrior II
EngineLycoming O-320-D3G
Horsepower160 hp
Seating Capacity4
Wingspan35 ft (10.7 m)
Length24 ft 0 in
Maximum Speed127 knots
Cruise Speed122 knots
Maximum Takeoff Weight2, 325 lb (1, 055 kg)
Fuel Capacity48 US gallons (182 L)

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