Piper Dakota Manuel utilisateur

DAKOTA

MAINTENANCE MANUAL

CARD 1 OF 3

PA-28-236 DAKOTA

PIPER AIRCRAFT CORPORATION

(PART NUMBER, 761 681 )

1A1

INTRODUCTION

This Piper Aircraft maintenance manual is prepared in accordance with the General Aviation

Manufacturers Association format.

Introduction

Page - 1

Reissued: August 1, 1986

1A2

PIPER AIRCRAFT

PA-28-236

MAINTENANCE MANUAL

VENDOR PUBLICATIONS

—WARNING—

When servicing or inspecting vendor equipment installed in Piper

aircraft, it is the user’s responsibility to refer to the applicable

vendor publication.

ENGINE:

Overhaul Manual = AVCO LYCOMING - OVERHAUL MANUAL

DIRECT DRIVE ENGINE - P/N 60294-7

Avco Lycoming Division

Williamsport, Pa. 17701

Parts Catalog = AVCO LYCOMING - P/N PC-415

Avco Lycoming Division

Williamsport, Pa. 17701

Operators Handbook = AVCO LYCOMING O-540, IO-540 and

HIO-540 SERIES AIRCRAFT ENGINES

P/N 60297-l0

Avco Lycoming Division

Williamsport, Pa. 1770l

PROPELLER:

Overhaul Instructions = HARTZELL COMPACT CONSTANT SPEED

and FEATHERING PROPELLER - P/N 117-D

Hartzell Propeller Inc.

Piqua, Ohio 45356

MAGNETOS:

Installation, Operation

and Maintenance

Instructions = BENDIX ELECTRICAL COMPONENTS

DIVISION

Sidney, New York l3838

S-200 Series

Magnetos = L-526-3 Installation and Maintenance Instructions

L-527-4 Overhaul Instructions

L-528-7 Service Parts List

S-20 Series

Magnetos = L-205-l0 Overhaul Instructions

L-223-15 Service Parts List

AUTOFLIGHT:

Operational Service

Manual = CENTURY 21, EDO-AIRE MITCHELL

Box 610, Mineral Wells, Texas 76067

Introduction

Page - 2

Reissued: August 1, 1986

1A3

PIPER AIRCRAFT

PA-28-236

MAINTENANCE MANUAL

PIPER PUBLICATIONS

COMMUNICATIONS:

Removal, Installation

and Maintenance

Instructions = 76l 502 AutoControl III B Service Manual

76l 48l AutoFlite II Service Manual

753 771 Pitch Trim Service Manual

Radio Service and

Maintenance Manual = 761 685 Avionics Wiring Diagram Service Manual

(1978)

76l 713 Avionics Wiring Diagram Service Manual

Vol. I and Vol. II (l979)

REPAIRS:

A.B.S. Thermoplastic

Landing Gear Wheel

and Strut Fairing

Repair Instructions = 76l 708V A.B.S. Thermoplastic Landing Gear

Wheel and Strut Fairing Repair Instruction Manual

PARTS CATALOG = 761 680

PA-28-236

PERIODIC INSPECTION

REPORT FORM = 230 8l1

PA-28-236

PROGRAMMED

INSPECTION MANUAL = 76l 734

PA-28-236/ 201T

Introduction

Page - 3

Reissued: August 1, 1986

1A4

PIPER AIRCRAFT

PA-28-236

MAINTENANCE MANUAL

AEROFICHE EXPLANATION AND REVISION STATUS

The maintenance manual information incorporated in this set of Aerofiche cards has been arranged in

accordance with general specifications for Aerofiche adopted by the General Aviation Manufacturer’s

Association. The information in this Aerofiche maintenance manual is kept current by revisions distributed

periodically. These revisions supersede all previous revisions and are complete Aerofiche card replacements

and supersede Aerofiche cards of the same number in the set.

Identification of revised material:

Revised text and illustrations are indicated by a black vertical line along the left-hand margin opposite

revised or added material. Revision lines indicate only current revisions with changes and additions to existing

text and illustrations. Changes in capitalization, spelling, punctuation, indexing, the physical location of the

material or complete page additions are not identified by revision lines.

A reference and record of the material revised is included in each chapter’s Table of Contents/ Effectivity.

The codes used in the effectivity columns of each chapter are defined as follows:

TABLE OF CONTENTS/EFFECTIVITY CODES

Original Issue: None

First Revision: Revision Identification, (1R Month-Year)

Second Revision: Revision Identification, (2R Month-Year)

All subsequent revisions will follow with consecutive revision numbers

such as 3R, 4R, etc., along with the appropriate month-year.

Added Subject: Revision Identification, (A Month-Year)

Deleted Subject: Revision Identification, (D Month-Year)

Introduction

Page - 4

Reissued: August 1, 1986

1A5

PIPER AIRCRAFT

PA-28-236

MAINTENANCE MANUAL

The information in this Aerofiche maintenance manual was reissued August l, l986. This edition

supersedes all preceding revisions and is a complete Aerofiche card replacement. Revisions to this

maintenance manual 761 681 are as follows:

PN/Effectivity Publication Date Aerofiche Card Effectivity

761 68l (PR860801) March 16, 1987* All

761 681 (IR870223) March 16, 1987 1

761 681 (IR950215)* February 15, 1995 1 and 2

*INTERIM REVISION

Chapters 5, 6, and 27 of Card 1, and Chapter 51 of Card 2 have

been revised. There are no other changes included in this interim

change revision. Please discard your current cards 1 and 2, and

replace them with the revised ones. DO NOT DISCARD CARD 3.

The date on Aerofiche cards must not be earlier than the date noted for the respective card effectivity.

Consult the latest Aerofiche card in this series for current Aerofiche card effectivity.

SERIAL NUMBER INFORMATION

PA-28-236, DAKOTA- l979

Serial Numbers 28-7911001 to 28-7911395 inclusive.

PA-28-236, DAKOTA- l980

Serial Numbers 28-8011001 to 28-8011161 inclusive.

PA-28-236, DAKOTA- 1981

Serial Numbers 28-8111001 to 28-8111105 inclusive.

PA-28-236, DAKOTA- l982

Serial Numbers 28-82l1001 to 28-8211060 inclusive.

PA-28-236, DAKOTA- 1983

Serial Numbers 28-8311001 to 28-8311025 inclusive.

PA-28-236, DAKOTA- l984

Serial Numbers 28-84l1001 to 28-8411031 inclusive.

PA-28-236, DAKOTA- 1985

Serial Numbers 28-8511001 to 28-8511020 inclusive.

PA-28-236, DAKOTA- 1986

Serial Numbers 28-8611001 to 28-8611008 inclusive.

Serial Numbers 2811001 and up*.

*New method of assigning serial numbers used.

Introduction

Page - 5

Interim Revision: February 15, 1995

1A6

PIPER AIRCRAFT

PA-28-236

MAINTENANCE MANUAL

GAMA SYSTEM/CHAPTER INDEX GUIDE

SYST SUB-SYST AEROFICHE

CHAP SECTION TITLE GRID NO.

4AIRWORTHINESS LIMITATIONS 1A17

5 TIME LIMITS/MAINT CHECKS 1A21

6 DIMENSIONS AND AREAS 1B12

7 LIFTING AND SHORING 1B20

8 LEVELING AND WEIGHING 1C1

9 TOWING AND TAXIING 1C6

10 PARKING AND MOORING 1C10

11 REQUIRED PLACARDS 1C14

12 SERVICING 1C19

20 STANDARD PRACT - AIRFRAME 1EI

21 ENVIRONMENTAL SYSTEMS 1F12

22 AUTOFLIGHT 1H8

23 COMMUNICATIONS 1H12

24 ELECTRICAL POWER 1H21

25 EQUIPMENT/FURNISHINGS 1J17

27 FLIGHT CONTROLS 1J21

28 FUEL 2A17

32 LANDING GEAR 2B10

33 LIGHTS 2C20

34 NAVIGATION & PITOT/STATIC 2D7

37 VACUUM 2E1

39 ELECTRIC/ELECTRONIC PANELS AND

MULTIPURPOSE PARTS 2E16

Introduction

Page - 6

Reissued: August 1, 1986

1A7

PIPER AIRCRAFT

PA-28-236

MAINTENANCE MANUAL

GAMA SYSTEM/CHAPTER INDEX GUIDE (cont)

SYST SUB-SYST AEROFICHE

CHAP SECTION TITLE GRID NO.

51 STRUCTURES 2E19

52 DOORS 2F13

55 STABILIZERS 2F21

56 WINDOWS 2G7

57 WINGS 2G12

61 PROPELLER 2H2

70 STANDARD PRACTICES - ENGINE 2H10

71 POWERPLANT 2H14

73 ENGINE FUEL SYSTEM 2I10

74 IGNITION 2I18

77 ENGINE INDICATING 2K2

78 EXHAUST 2K10

79 OIL 2K14

80 STARTING 2K19

91 CHARTS/WIRING DIAGRAMS 3A17

95 SPECIAL PURPOSE EQUIPMENT 3D1

Introduction

Page - 7

Interim Revision: February 15, 1995

1A8

PIPER AIRCRAFT

PA-28-236

MAINTENANCE MANUAL

LIST OF ILLUSTRATIONS

FIGURE NO. SUBJECT GRID NO.

6-1. Three View 1B17

6-2. Station References 1B18

6-3. Access Plates and Panels 1B19

7-1. Jacking Arrangement 1B23

8-1. Weighing Airplane 1C4

8-2. Leveling Longitudinally 1C5

8-3. Leveling Laterally 1C5

11-1. Placards and Decals 1C17

12-1. Fuel Filter Bowl and Screen 1C22

12-2. Servicing Points 1D2

12-3. Main Gear Oleo Struts (Cut-away View) 1D6

12-4. Lubrication Chart (Landing Gear, Main) 1D14

12-5. Lubrication Chart (Landing Gear, Nose) 1D15

12-6. Lubrication Chart (Control System) 1D16 thru

1D19

12-7. Lubrication Chart (Cabin Door, Baggage Door and Seat) 1D20

12-8. Lubrication Chart (Power Plant, Propeller and Control

Pivot Points) 1D21

12-9. Lubrication Chart (Air Conditioning Condenser) 1D22

20-1. Torque Wrench Extension 1E5

20-2. Correct Method of Installing Rod End Bearings 1E5

20-3. Cherrylock Rivet Removal 1E6

20-4. Hose/Line Markings 1E8

20-5. Flareless Tube fittings 1E9

21-1. Cabin Heater, Defroster and Fresh Air System 1F16

21-2. Air Conditioning System Installation (Typical) 1F24

21-3. Service Valves 1G5

21-4. Test Gauge and Manifold Set 1G6

21-5. Manifold Set Operation 1G7

21-6. Leak Test Hookup 1G8

21-7. Evacuation Hookup 1G10

21-8. Charging Stand 1G12

21-9. Charging Hookup 1G14

21-10. Compressor and Fabricated Oil Dipstick 1G17

21-11. Compressor and Alternator Belt Installation 1G18

21-12. Magnetic Clutch 1G21

21-13. Condenser Air Scoop Installation 1G24

21-14. Expansion Valve 1H1

Introduction

Page - 8

Reissued: August 1, 1986

1A9

PIPER AIRCRAFT

PA-28-236

MAINTENANCE MANUAL

LIST OF ILLUSTRATIONS

FIGURE NO. SUBJECT GRID NO.

21-15. Components Installation 1H3

21-16. Overhead Vent System (Not Available with

Air Conditioning) 1H5

23-1. Avionics Master and Emergency Switch Circuit 1H14

23-2. Communications Components ELT Schematic 1H16

23-3. Emergency Locator Transmitter Schematic (Narco) 1H16

23-4. ELT Portable Folding Antenna (Narco) 1H18

23-5. ELT Using Fixed Aircraft Antenna (Narco) 1H18

24-1. Lamp-Bank Load 1I10

24-2. Exploded View of Alternator (Chrysler) 1I12

24-3. Checking Field Coil Current Draw 1I12

24-4. Testing Field Circuit 1I12

24-5. Testing Positive Rectifiers 1I14

24-6. Testing Negative Rectifiers 1I14

24-7. Rectifier End Shield and Stator Assembly 1I14

24-8. Testing Positive Rectifiers With Test Lamp 1I16

24-9. Testing Negative Rectifiers With Test Lamp 1I16

24-10. Rectifier and Heatsink Assembly Removal 1I17

24 11. Rectifier End Shield Assembly 1I17

24-12. Testing Stator 1I18

24-13. Removal of Pulley 1I18

24-14. Removal of Bearing 1I19

24-15. Removal of Rectifier End Shield Bearing 1I19

24-16. Testing Rotor for Ground 1I20

24-17. Testing Rotor for Opens or Shorts 1I20

24-18. Installation of Grease Retainer 1I21

24-19. Installation of Rectifier End Shield Bearing 1I21

24-20. Installation of Drive End Shield Bearing 1I21

24-21 . Installation of Pulley 1I21

24-22. Installation of Insulators 1I23

24-23. Installation of Positive Rectifier Assembly 1I23

24-24. Installation of Capacitor 1I23

24-25. Installation of Battery Output Insulator 1I23

24-26. Installation of Negative Rectifier Assembly 1J1

24-27. Installation of Stator 1J1

24-28. Exploded View of Alternator (Prestolite) 1J3

24-29. Removal of Slip Ring End Bearing 1J4

24-30. Removal of Rectifier 1J4

24-31. Removal of Drive End Head 1J4

24-32. Removal of End Head Bearing 1J4

24-33. Testing Rotor for Ground 1J5

Introduction

Page - 9

Reissued: August 1, 1986

1A10

PIPER AIRCRAFT

PA-28-236

MAINTENANCE MANUAL

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