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Piper Cherokee Six User Manual

Piper Cherokee Six
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PIPER
CHEROKEE
SIX
Service
Manual
PA-32-260
PA-32-300
PA-32R-300
CARD
1
OF
3
PIPER
AIRCRAFT
CORPORATION
753
690
1Al

Table of Contents

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Piper Cherokee Six Specifications

General IconGeneral
ManufacturerPiper Aircraft
ModelCherokee Six
Seating Capacity6-7
EngineLycoming O-540
TypeLight aircraft
First flight1965
Crew1
Capacity5-6 passengers
Max takeoff weight3, 400 lb (1, 542 kg)
Rate of climb1, 050 ft/min (5.3 m/s)
Engine TypePiston engine
Range720 nautical miles (1, 333 km)
VariantsPA-32-260, PA-32-300
Wingspan32 ft 10 in (10.01 m)
Powerplant1 × Lycoming O-540-E4B5 6-cylinder horizontally opposed piston engine, 260 hp (194 kW)

Summary

Aerofiche Explanation and Revision Status

Conversion of Aerofiche Alpha Numeric Code Numbers

Explains the alpha-numeric code system for aerofiche cards, including card number and grid location.

Identification of Revised Material

Describes how revised text and illustrations are indicated by a black vertical line along the left margin.

SECTION I

INTRODUCTION

Provides general information about the service manual and the aircraft, covering scope and major components.

SECTION II

HANDLING AND SERVICING

Covers routine handling, servicing procedures, ground handling, and lubrication.

SECTION III

INSPECTION

Provides instructions for conducting inspections and programmed maintenance schedules.

SECTION IV

STRUCTURE

Explains removal, installation, rigging, and adjustment procedures for structural surfaces.

SECTION V

SURFACE CONTROLS

Details removal, installation, rigging, and adjustment procedures for control surfaces.

SECTION VA

HYDRAULIC SYSTEM (PA-32R-300)

Covers overhaul, inspection, adjustment, and troubleshooting of hydraulic system components.

SECTION VI

LANDING GEAR AND BRAKE SYSTEM (PA-32-260 and 300)

Provides instructions for removal, disassembly, inspection, overhaul, and installation of landing gear and brake system components.

SECTION VIA

LANDING GEAR AND BRAKE SYSTEM (PA-32R-300)

Covers overhaul, inspection, and adjustment of PA-32R-300 landing gear and brake system components.

SECTION VII

POWER PLANT (PA-32-260)

Details removal, installation, and adjustment procedures for the PA-32-260 engine and propeller systems.

SECTION VIIA

POWER PLANT (PA-32-300 & PA-32R-300)

Covers overhaul, inspection, and adjustment of the PA-32-300 and PA-32R-300 engine and propeller systems.

SECTION VIII

FUEL SYSTEM

Provides instructions for inspection, repair, removal, installation, and troubleshooting of the fuel system.

SECTION IX

INSTRUMENTS

Details maintenance, troubleshooting, removal, and installation of aircraft instruments.

SECTION X

ELECTRICAL SYSTEM

Covers description, troubleshooting, testing, and maintenance of the aircraft's electrical system components.

SECTION XI

ELECTRONICS

Provides instructions for removal, installation, and operational checks of electronic equipment like ELTs and autopilots.

SECTION XII

CABIN HEATER AND VENTILATOR SYSTEM

Details description, maintenance, and malfunction diagnosis for the cabin heating and ventilation system.

SECTION XIII

ACCESSORIES AND UTILITIES

Covers installation, servicing, and troubleshooting of air conditioning system components.

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