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Piper PA-28-161 User Manual

Piper PA-28-161
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2.25 PLACARDS
In full view of the pilot:
THIS AIRPLANE MUST BE OPERATED AS A
NORMAL OR UTILITY CATEGORY AIRPLANE
IN COMPLIANCE WITH THE OPERATING
LIMITATIONS STATED IN THE FORM OF
PLACARDS, MARKINGS AND MANUALS.
ALL MARKINGS AND PLACARDS ON THIS
AIRPLANE APPLY TO ITS OPERATION AS A
UTILITY CATEGORY AIRPLANE. FOR NORMAL
AND UTILITY CATEGORY OPERATION, REFER
TO THE PILOT’S OPERATING HANDBOOK.
NO ACROBATIC MANEUVERS ARE APPROVED
FOR NORMAL CATEGORY OPERATIONS. SPINS
ARE PROHIBITED FOR NORMAL AND UTILITY
CATEGORY.
In full view of the pilot:
TAKEOFF CHECKLIST
Fuel on proper tank Seat backs erect
Electric fuel pump on Fasten belts/harness
Engine gauges checked Trim tab - set
Flaps - set Controls - free
Carb. heat off Door - latched
Mixture set Air conditioner off
Primer locked
LANDING CHECKLIST
Fuel on proper tank Flaps - set (White Arc)
Mixture rich Fasten belts/harness
Electric fuel pump on Air conditioner off
Seat backs erect
The AIR COND OFF item in the above takeoff and landing checklists is
mandatory for air conditioned aircraft only.
PIPER AIRCRAFT CORPORATION SECTION 2
PA-28-161, WARRIOR II LIMITATIONS
ISSUED: AUGUST 13, 1982 REPORT: VB-1180
2-7

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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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