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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 4
Nov 30/06
1C22
5-20-00
4. Annual / 100 Hour Inspection
Procedure
A. Scheduled Maintenance (i.e. - paragraph 5.)
(1) The required periodic inspection procedure is listed in paragraph 5. This inspection procedure
is broken down into major groups which include Propeller, Engine, Cabin and Cockpit,
Fuselage and Empennage, Wing, Landing Gear, Special Inspection, Operational Inspection
and General. The first column in each group lists the inspection or procedure to be performed.
The second column is divided into two sub-columns indicating the required inspection interval
of 50 hours or 100 hours. Each inspection or operation is required at each of the inspection
intervals indicated by a circle (O). When vendor publications specify times other than those
designated in the the various columns, it will be indicated as:
or
in the inspection interval columns, or listed as a special inspection in 5-30-00, or both.
(2) Refer to the applicable chapter of this manual for instructions on how to gain access to remove
any item that must be removed and is not completely accessible.
(3) Inspection Report Forms.
To help in the performance of periodic inspections, Inspection Report forms are available
through Piper Dealers:
P/N 230-1802 for the Warrior III (S/N’s 2842001 & up).
NOTE: Service centers conducting Part 91 Annual / 100 Hour Inspections can use the
Inspection Report Form (P/N 230-1802), as a working check-off list, provided they
verify its currency against an up-to-date copy of the ICA (i.e. - this Maintenance
Manual, see 4-00-00 and 5-20-00).
(4) In addition to inspection intervals required in scheduled maintenance (i.e. - paragraph 5),
preflight inspection must also be performed.
(5) References to maintenance manual applicable areas are per the “chapter - system/sub-system”
assignment of subject material numbering system.
B. Special Inspections (see 5-30-00.)
C. Unscheduled Maintenance (see 5-50-00.)
As required by
“applicable vendor
publication”
See Note “X”

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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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