piper Arrow IV PA28RT-201 maintenance service manual

INTRODUCTION. This PIPER AIRCRAFT Maintenance Manual is prepared in accordance with the GAMA (General Aviation Manufacturers Association) format. This maintenance manual is divided into various Groups which enable a broad separation of contents (Chapters) within each group. The various Chapters are broken down into major systems such as Electrical Power, Flight Controls, Fuel, Landing Gear, etc. The System/Chapters are arranged more or less alphabetically rather than by precedence or importance. All System/Chapters are assigned a number, which becomes the first element of a standardized numbering system. Thus the element “32” of the number series 32-00-00 refers to the System/Chapter on “Landing Gear.” All information pertaining to the landing gear will be covered in this System/Chapter. The major System/Chapters are then broken down into Sub-System/Sections. These sections are identified by the second element of the standardized numbering system. The number “40” of the basic number series 32- 40-00 is for the “Wheels and Brakes” portion of the landing gear. The individual units within a Sub-System/Section may be identified by a third element of the standardized numbering system, such as 32-40-0l. This number could be assigned by the manufacturer to fit the coverage requirements of the publication. Example: This manual does not contain hardware callouts for installation. Hardware callouts are only indicated where a special application is required. To confirm the correct hardware used, refer to the PA-28RT-201/201T Parts Catalog P/N 761 693, and FAR 43 for proper utilization. Introduction Page - 1 December 1, 1978 1A2 PIPER AIRCRAFT PA-28RT-201 / 201T MAINTENANCE MANUAL CHAPTER/SYSTEM LANDING GEAR SUB-SYSTEMS WHEELS AND BRAKES INDIVIDUAL UNITS NOSE WHEEL REMOVAL 32-40-01

VENDOR PUBLICATIONS. ENGINE (LYCOMING): 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-102 Avco Lycoming Division Williamsport, Pa. 17701 Operators Handbook = AVCO LYCOMING O-360, HO-360, IO-360, AIO-360, HIO-360, LIO-360 and TIO-360 SERIES AIRCRAFT ENGINES - P/N 60297-12 Avco Lycoming Division Williamsport, Pa. 17701 ENGINE (CONTINENTAL): Overhaul Manual = CONTINENTAL - OVERHAUL MANUAL Form No. X-30030A Teledyne Continental Motors Aircraft Products Division Mobile, Alabama 36601 Parts Catalog = CONTINENTAL - Form No. X-30031A Teledyne Continental Motors Aircraft Products Division Mobile, Alabama 36601 Operators Handbook = CONTINENTAL - Form No. X-30512 Teledyne Continental Motors Aircraft Products Division Mobile, Alabama 36601 PROPELLER: Overhaul Instructions = HARTZELL COMPACT CONSTANT SPEED and FEATHERING PROPELLER - P/N 113A Hartzell Propeller Inc. Piqua, Ohio 45356 Service Manual = McCAULEY C200 SERIES CONSTANT SPEED PROPELLERS - P/N 780630 McCauley Accessory Division 3535 McCauley Drive Vandalia, Ohio 45377 MAGNETOS: Installation, Operation and Maintenance Instructions = D-2000 and D-2200 SERIES MAGNETO IGNITION SYSTEM - P/N L-928 Bendix Electrical Components Division Sidney, New York 13838 AUTOPILOT: CENTURY 41 AUTOPILOT, Edo-Aire Mitchell Box 610, Mineral Wells, Texas 76067 Introduction Page - 2 Revised: August 17, 1982 1A3 PIPER AIRCRAFT PA-28RT-201 / 201T MAINTENANCE MANUAL

PIPER PUBLICATIONS. ELECTRONICS: AutoFlight II Service Manual = Piper P/N 761 481 Pitch Trim Service Manual = Piper P/N 753 771 AutoControl III B and Altimatic III B Service Manual = Piper P/N 753 502 Altimatic III C Service Manual = Piper P/N 761 602 79 Vero Beach Avionics Wiring Diagrams Manual = Piper P/N 761 713 AEROFICHE: PA-28RT-201/201T Parts Catalog = Piper P/N 761 693 INSPECTION: PA-28RT-201/201T Program Inspection Manual = Piper P/N 761 736 Inspection Forms = Piper P/N 230 818 Introduction Page - 3 Added: August 17, 1982 1A4 PIPER AIRCRAFT PA-28RT-201 / 201T MAINTENANCE MANUAL

AEROFICHE GRID NUMBERING AND REVISION IDENTIFICATION 1. Aer of ic he Gr id Number ing Piper has ceased production of all Aerofiche (i.e., microfiche) products. The Aerofiche grid numbers will be removed in the next complete revision. In the interim, as partial revisions occur, the Aerofiche grid numbering system may be modified, as explained below, to simplify production. Deviations from the legacy Aerofiche grid numbering system will occur when it becomes necessary to add pages to the manual and will typically take two forms: A. Inserting pages between two existing grids in the same row. When inserting two pages between the existing grids 1A8 and 1A9, the two new pages will be numbered 1A8A and 1A8B. B. Inserting pages at the end of an Aerofiche grid row. The legacy Aerofiche grid numbering system limited page numbers in a row to a maximum of 24 (i.e., row 1A would be numbered 1A1–1A24). That limit no longer applies. Accordingly, if two pages need to be added between any existing grid row end and grid row start (i.e., 1A24 and 1B1), the new pages will simply be numbered 1A25 and 1A26. 2. Identifying Re vised Ma ter ial A. Dec 1978 through 1995: Revised text and illustrations are indicated by a black vertical line along the left-hand margin of the frame, opposite revised, added or deleted material. Revision lines indicate only current revisions with changes and additions to or deletions of 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. B. 2009 and later: A revision to a page is defined as a change to the text or illustrations that existed previously. Revisions, additions and deletions are identified by a vertical line (aka change bar) along the left- hand margin of the page opposite only the text or illustration that was changed. Reformatted, but otherwise unchanged, text is not identified by a change bar. Change bars in the section Tables of Contents do not indicate a change to that page, but rather that the information in the actual paragraph has changed. A change bar in the left-hand margin opposite the footer (i.e. - chapter/section/subject, page number and date), indicates that the text was unchanged but the material was relocated to a different page. Example. NO TE : Change bars are not used in the title pages. Likewise, when a publication is completely revised (i.e. - reissued), change bars will only appear in the Tables of Contents. 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) Introduction Page - 4 Revised: January 31, 2009 1A5 PIPER AIRCRAFT PA-28RT-201 / 201T MAINTENANCE MANUAL

REVISION STATUS Revisions to Maintenance Manual (761-694) originally published December 1, 1978 are as follows: Re visions Da te Aer of ic he Car d Ef f ecti vity ORG 781201 December 1, 1978 1, 2 and 3 PR790223 February 23, 1979 1, 2 and 3 PR791106 November 6, 1979 1, 2 and 3 PR800818 August 18, 1980 1, 2 and 3 PR810724 July 24, 1981 1, 2 and 3 PR811221 December 21, 1981 1, 2 and 3 PR820817 August 17, 1982 1, 2 and 3 PR830713 July 13, 1983 1, 2 and 3 PR840808 August 8, 1984 1, 2 and 3 IR860730 July 30, 1986 (Interim) 1 IR860921 September 21, 1986 (Interim) 1 IR950227 February 27, 1995 (Interim) 1, 2 and 3 PR090131 January 31, 2009 N/A* * Piper has ceased production of all Aerofiche (i.e., microfiche) products. Maintenance Manual subscriptions are available exclusively from Avantext, Inc. (www.Avantext.com) on CD-Rom or DVD. The CDs/DVDs include applicable Service Bulletins and Service Letters. Consult the “Customer Service Information File" (available in the Avantext CD/DVD cited above) to verify that you have the latest revision. SERIAL NUMBER INFORMATION This encompasses the following model years: NO TE : The following is provided as a general reference only. Model Sub-Model Ser ial Number s Model Y ear PA-28RT-201 Arrow IV 28R-7918002 thru 28R-7918267 1979 28R-8018001 thru 28R-8018106 1980 28R-8118001 thru 28R-8118082 1981 28R-8218001 thru 28R-8218026 1982 PA-28RT-201T Turbo Arrow IV 28R-7931002 thru 28R-7931310 1979 28R-8031001 thru 28R-8031178 1980 28R-8131001 thru 28R-8131208 1981 28R-8231001 thru 28R-8231080 1982 28R-8331001 thru 28R-8331051 1983 28R-8431001 thru 28R-8431032 1984 28R-8531001 thru 28R-8531015 1985 28R-8631001 and 28R-8631005 1986 28R-8631002 thru 28R-8631004 1987 2831001 thru 2831033 1987 2831034 thru 2831038 1988 Introduction Page - 5 Revised: January 31, 2009 1A6 PIPER AIRCRAFT PA-28RT-201 / 201T MAINTENANCE MANUAL

GAMA SYSTEM/CHAPTER INDEX GUIDE SYST SUB-SYST AEROFICHE CHAP SECTION TITLE GRID NO. 4 AIRWORTHINESS LIMITATIONS 1A18 5 TIME LIMITS/MAINT CHECKS 1A22 6 DIMENSIONS AND AREAS 1B16 7 LIFTING AND SHORING 1C5 8 LEVELING AND WEIGHING 1C9 9 TOWING AND TAXIING 1C14 10 PARKING AND MOORING 1C18 11 REQUIRED PLACARDS 1C22 12 SERVICING 1D5 20 STANDARD PRACT - AIRFRAME 1E14 21 ENVIRONMENTAL SYSTEM 1E21 22 AUTOFLIGHT 1H1 23 COMMUNICATIONS 1H8 24 ELECTRICAL POWER 1H17 27 FLIGHT CONTROLS 1J17 28 FUEL 2A18 29 HYDRAULIC POWER 2B17 32 LANDING GEAR 2D4 33 LIGHTS 2F19 34 NAVIGATION & PITOT/STATIC 2G7 35 OXYGEN SYSTEM 2G21 37 VACUUM SYSTEM 2H17 Introduction Page - 6 Revised: July 13, 1983 1A7 PIPER AIRCRAFT PA-28RT-201 / 201T MAINTENANCE MANUAL

GAMA SYSTEM/CHAPTER INDEX GUIDE (cont) SYST SUB-SYST AEROFICHE CHAP SECTION TITLE GRID NO. 39 ELECTRICAL/ELECTRONIC PANELS AND MULTI-PURPOSE PARTS 2I2 51 STRUCTURES 2I6 52 DOORS 2J1 55 STABILIZERS 2J10 56 WINDOWS 2J19 57 WINGS 2J24 61 PROPELLER 3A18 70 STANDARD PRACTICES - ENGINE 3B9 71 POWER PLANT 3B12 73 ENGINE FUEL AND CONTROL 3C12 74 IGNITION 3D7 77 ENGINE INDICATING 3F16 78 EXHAUST 3G1 79 OIL SYSTEM 3G6 80 STARTING 3G10 81 TURBINES 3H1 91 CHARTS AND WIRING DIAGRAMS 3H7 95 SPECIAL PURPOSE EQUIPMENT 3K1 Introduction Page - 7 Interim Revision: February 27, 1995 1A8 PIPER AIRCRAFT PA-28RT-201 / 201T MAINTENANCE MANUAL

LIST OF ILLUSTRATIONS FIGURE NO. SUBJECT GRID NO. 6-1. Three View of PA-28RT-201T 1B22 6-2. Three View of PA-28RT-201 1B23 6-3. Station Reference Lines of PA-28RT-201/201T 1C1 6-4. Access Plates and Panels 1C3 7-1. Jacking Arrangements 1C7 8-1. Leveling Longitudinally 1C12 8-2. Leveling Laterally 1C12 8-3. Weighing Arrangement 1C12 11-1. Placards and Decals 1C24 12-1. Servicing Points (PA-28RT-201) 1D8 12-2. Servicing Points (PA-28RT-201T) 1D9 12-3. Fuel Strainer 1D10 12-4. Lubrication Chart (Landing Gear, Main) 1D24 12-5. Lubrication Chart (Landing Gear, Nose) 1E2 12-6. Lubrication Chart (Control System) 1E4 12-7. Lubrication Chart (Cabin Door, Baggage Door and Seat) 1E8 12-8. Lubrication Chart (Lycoming Power Plant, Propeller and Control Pivot Points) 1E9 12-9. Lubrication Chart (Continental Power Plant, Propeller and Control Pivot Points) 1E10 12-10. Lubrication Chart (Back-Up Extender) 1E11 12-11. Lubrication Chart (Air Conditioning Condenser) 1E12 20-1. Torque Wrench Extension 1E16 20-2. Method of Installing Rod End Bearings 1E17 21-1. Cabin Heater and Defroster (PA-28RT-201) 1F7 21-2. Cabin Heater and Defroster (PA-28RT-201T) 1F8 21-3. Overhead Vent System and Fresh Air System “Not Available with Air Conditioning” 1F9 21-4. Air Conditioning System Installation 1F11 21-5. Service Valves 1F16 21-6. Test Gauge and Manifold Set 1F16 21-7. Manifold Set Operation 1F18 21-8. Leak Test Hookup 1F19 21-9. Evacuation Hookup 1F21 21-10. Charging Stand 1F24 21-11. Charging Hookup 1F24 21-12. Top Dead Center Casting Mark (Sankyo Compressor) 1G6 21-13. Rotation of Clutch Front Plate (Sankyo Compressor Oil Check) 1G6 21-14. York Compressor and Fabricated Oil Dipstick (PA-28RT-201) 1G7 21-15. Compressor and Alternator Belt Installation (PA-28RT-201) 1G9 21-16. Magnetic Clutch (York Compressor) 1G10 Introduction Page - 8 Revised: July 13, 1983 1A9 PIPER AIRCRAFT PA-28RT-201 / 201T MAINTENANCE MANUAL

LIST OF ILLUSTRATIONS (cont) FIGURE NO. SUBJECT GRID NO. 21-17. Condenser Air Scoop Installation 1G14 21-18. Expansion Valve 1G15 21-19. Components Installation 1G17 21-20. Adjustment of Air Conditioning Throttle Switch (PA-28RT-201) 1G17 21-21. Air Conditioning Wiring Schematic 1G19 23-1. ELT Portable Folding Antenna (Narco) 1H12 23-2. ELT Using Fixed Aircraft Antenna (Narco) 1H12 23-3. ELT Schematics 1H16 24-1. Lamp-Bank Load 1I8 24-2. Exploded View of Alternator (Chrysler) 1I10 24-3. Checking Field Coil Current Draw 1I10 24-4. Testing Field Circuit 1I10 24-5. Testing Positive Rectifiers With C-3829 Tester 1I12 24-6. Testing Negative Rectifiers With C-3829 Tester 1I12 24-7. Rectifier End Shield and Stator Assembly 1I12 24-8. Testing Positive Rectifiers With Test Lamp 1I14 24-9. Testing Negative Rectifiers With Test Lamp 1I14 24-10. Rectifier and Heatsink Assembly Removal 1I14 24-11. Rectifier End Shield Assembly 1I14 24-12. Testing Stator 1I16 24-13. Removal of Pulley 1I16 24-14. Removal of Bearing 1I16 24-15. Removal of Rectifier End Shield Bearing 1I16 24-16. Testing Rotor for Ground 1I17 24-17. Testing Rotor for Opens or Shorts 1I17 24-18. Installation of Grease Retainer 1I18 24-19. Installation of Rectifier End Shield Bearing 1I18 24-20. Installation of Drive End Shield Bearing 1I18 24-21. Installation of Pulley 1I18 24-22. Installation of Insulators 1I20 24-23. Installation of Positive Rectifier Assembly 1I20 24-24. Installation of Capacitor 1I20 24-25. Installation of Battery Output Insulator 1I20 24-26. Installation of Negative Rectifier Assembly 1I21 24-27. Installation of Stator 1I21 24-28. Exploded View of Alternator (Prestolite) 1I23 24-29. Removal of Slip Ring End Bearing 1I24 24-30. Removal of Rectifier 1I24 24-31. Removal of Drive End Head 1J2 24-32. Removal of End Head Bearing 1J2 24-33. Testing Rotor for Ground 1J2 24-34. Testing Rotor for Shorts 1J2 Introduction Page - 9 Revised: July 13, 1983 1A10 PIPER AIRCRAFT PA-28RT-201 / 201T MAINTENANCE MANUAL

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piper Arrow IV PA28RT-201 maintenance service manual

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