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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 1
Nov 30/06
5C5
74 - CONTENTS
CHAPTER 74 - IGNITION
T
ABLE OF CONTENTS
SUBJECT SECTION P
AGE GRID NO.
ELECTRICAL PO
WER SUPPLY
74-10-00 1 5C7
Ignition System 1 5C7
Description 1 5C7
Troubleshooting 1 5C7
Replacement Magnetos 1 5C7
Overhaul 1 5C7
Magnetos 3 5C9
100 Hour Inspection 3 5C9
Removal 5 5C11
500 Hour Inspection and Cleaning 5 5C11
Disassembly 11 5C17
Assembly 12 5C18
Testing 17 5C23
Installation 17 5C23
DISTRIBUTION 74-20-00 1 5D3
Ignition Harness 1 5D3
Inspection 1 5D3
Removal 1 5D3
Disassembly 1 5D3
Assembly 4 5D6
Installation 6 5D8
Spark Plugs 6 5D8
Removal 6 5D8
Inspection and Cleaning 7 5D9
Installation 7 5D9
SWITCHING
74-30-00 1 5D13
Ignition Switch 1 5D13

Table of Contents

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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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