Piper PA-34-220T Airplane Maintenance Manual

3433089 thru 3433136 1988 3433137 thru 3433168 1989 3433171 thru 3433172 3433169 and 3433170 1990 Seneca III 28 V 3448001 thru 3448004 1989 3448005 thru 3448007 1990 3448009 3448011 thru 3448014 3448008 and 3448010 1992 3448015 thru 3448022 3448023 thru 3448028 1993 3448030 thru 3448033 (036 & 037 renumbered 3448029 1994 as Seneca IV’s 051 & 060) 3448034 and 3448035 Seneca IV 3448038 thru 3448061 1994 3448062 thru 3448079 1995 Introduction Page 2 April 17, 2007 1A8 PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL Introduction Page 3 April 17, 2007 1A9 4. SERIAL NUMBER EXPLANATION This manual encompasses airplanes manufactured under two different serial numbering systems. A. The earlier system is comprised of four sets of numbers, as shown in the following example: B. The later system is comprised of three sets of numbers, as shown in the following example: 5. ASSIGNMENT OF SUBJECT MATERIAL This publication is divided into industry standard, three element, numeric subject groupings as follows: A. System/Chapter - The various groups are broken down into major systems such as Environmental Systems, Electrical Power, Landing Gear, etc. They are assigned a number, which becomes the first element of the standardized numbering system. Thus, the element “28” of the number 28-40-00 refers to the chapter “Fuel”. Everything concerning the fuel system will be covered in this chapter. B. Sub-System/Section - The major systems/chapters of an airplane are broken down into subsystems. These sub-systems are identified by the second element of the standard numbering system. The element “40” of the number 28-40-00 concerns itself with the indicating section of the fuel system. C. Unit/Subject - The individual units within a sub-system/section may be identified by the third element of the standard numbering system. The element “00” of the number 28-40-00 is a subject designator. This element is assigned at the option of the manufacturer and is normally zeroed out by PIPER. Refer to the Chapter/Section Index Guide, below, for a complete breakdown and list. The material is arranged in ascending numerical sequence. 6. PAGINATION The Chapter - Section (i.e. - 28-40-00) numbering system explained above forms the primary page numbering system for this manual. Within each Section, pages are numbered consecutively beginning with Page 1 (i.e. - 28-40-00, Page 1). PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 34 48 001 TYPE CERTIFICATE DESIGNATION SEQUENCE NUMBER MODEL CODE (33 = PA-34-220T 14v) (48 = PA-34-220T 28v, Piper Aircraft Corp.) 34 81 33 001 TYPE CERTIFICATE DESIGNATION MODEL CODE (33 = PA-34-220T 14v) SEQUENCE NUMBER MODEL YEAR Introduction Page 4 April 17, 2007 1A10 PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 7. AEROFICHE EFFECTIVITY A. The General Aviation Manufacturers Association (GAMA) have developed specifications for microfiche reproduction of aircraft publications. The information compiled in this Aerofiche Maintenance Manual will be kept current by revisions distributed periodically. These revisions will supersede all previous revisions and will be complete Aerofiche card replacements and shall supersede Aerofiche cards of the same number in the set. The “Aerofiche Effectivity” page at the front of this manual lists the current revision for each card in this set. B. Conversion of Aerofiche alpha/numeric grid code numbers: First number is the Aerofiche card number. Letter is the horizontal row reference per card Second number is the vertical column reference per card. Example: 2J16 = Aerofiche card number two, row J, column 16. C. To aid in locating information, the following is provided: (1) At the beginning of the first aerofiche card: (a) A complete Chapter/Section Index Guide for all fiche in the set. (b) A complete List of Illustrations for all fiche in the set. (c) A complete List of Charts for all fiche in the set. (2) At the beginning of the the second and subsequent aerofiche cards: (a) A complete Chapter/Section Index Guide for all fiche in the set. (b) A complete List of Illustrations for the individual aerofiche card. (c) A complete List of Charts for the individual aerofiche card. 8. IDENTIFYING REVISED MATERIAL Revised text and illustrations are indicated by a vertical line along the left-hand margin of the page, opposite revised, added or deleted material. Revision lines indicate only current revisions with changes, additions to, or deletions of, existing text and illustrations. Changes in capitalization, spelling, punctuation, indexing, or the physical location of the material are not identified by revision lines, but are identified as revised by the revision date on each page. Example. 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 or Complete Reissue: None Revisions: nRmmyy (i.e. - 2R0698) Added Subject: Ammyy (i.e. - A0698) Deleted Subject: Dmmyy (i.e. - D0698) Where “nR” = revision number (since issue or reissue), “A” = added, “D” = deleted; and “mmyy” = month and year. Introduction Page 5 April 17, 2007 1A11 9. WARNINGS, CAUTIONS, AND NOTES The Warnings, Cautions, and Notes used throughout this manual emphasize important information. WARNING: OPERATING PROCEDURES, PRACTICES, ETC., WHICH MAY RESULT IN PERSONAL INJURY OR LOSS OF LIFE IF NOT CAREFULLY FOLLOWED. CAUTION: OPERATING PROCEDURES, PRACTICES, ETC., WHICH IF NOT STRICTLY OBSERVED MAY RESULT IN DAMAGE TO EQUIPMENT. NOTE: An operating procedure, condition, etc., which is essential to emphasize. 10. ACCIDENT/INCIDENT REPORTING To improve our Service and Reliability system and aid in Piper’s compliance with FAR 21.3, knowledge of all incidents and/or accidents must be reported to Piper immediately. To expedite and assist in reporting all incidents and accidents, Piper Form 420-01 has been created. See Service Letter 1041 for latest revision. This procedure is to be used by all Dealers, Service Centers and Repair Facilities. 11. SUPPLEMENTARY PUBLICATIONS A. PIPER PUBLICATIONS P/N (1) PA-34-220T Seneca III / IV Parts Catalog 761-750 (2) PA-34-220T Seneca III / IV Progressive Inspection Manual (50 HR) 761-753 (3) PA-34-220T Seneca III / IV Inspection Report 230-1061 (4) AutoFlight II Service Manual 761-481 (5) Pitch Trim Service Manual 753-771 (6) AutoControl IIIB and Altimatic IIIB Service Manual 753-502 (7) Altimatic IIIC Service Manual 761-602 (8) Customer Service Information Aerofiche 1753-755 (9) Service Bulletin / Service Letter Index 762-332 B. VENDOR PUBLICATIONS WARNING: FAILURE TO CONSULT APPLICABLE VENDOR PUBLICATION(S), WHEN SERVICING OR INSPECTING VENDOR EQUIPMENT INSTALLED IN PIPER AIRCRAFT, MAY RENDER THE AIRCRAFT UNAIRWORTHY. (1) AIR CONDITIONING COMPRESSOR: Vendor: Sanden International (USA), Inc. PH - 972-442-8400 601 South Sanden Blvd. Wylie, TX 75098-4999 http://www.sanden.com PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL Introduction Page 6 April 17, 2007 1A12 PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL (2) AUTOFLIGHT: Vendor(s): Honeywell One Technology Center 23500 W. 105th St., M/D #45 Olathe, Kansas 66061-1950 http://www.bendixking.com/ System Flight Line KFC 150 Installation Manual: P/N 006-0287-00 System Flight Line KFC 200 Maintenance Manual: P/N 006-5134-01 (3) BRAKES: Vendor: Parker Hannifin Corp. PH - 800-272-5464 Aircraft Wheel and Brake Division 1160 Center Road Avon, Ohio 44011 http://www.parker.com/ (4) ENGINE: Vendor: Teledyne Continental Motors PH - 800-718-3411 Attn: Aircraft Products Division FAX - 251-432-7352 Mobile, Alabama 36601 Overhaul Manual: Form No. X-30596A Parts Catalog: Form No. X-30597A Operators Handbook: Form No. X-30583 (5) FIRE EXTINGUISHER (PORTABLE): Vendor: H3R Inc. PH - 800-249-4289 43 Magnolia Ave # 4 San Francisco, California 94123-2911 http://www.h3r.com/index.htm (6) FUEL CELLS: Vendor: Engineered Fabrics Corporation PH - 770-684-7855 669 Goodyear Street FAX - 770-684-7438 Rockmart, Georgia 30153-0548 http://www.kfefc.com/index.htm (7) GEAR LOCKING ACTUATORS, HYDRAULIC PUMP, AND ALL HYDRAULIC COMPONENTS: Vendor: Parker Hannifin Corporation PH - 800-C-PARKER 6035 Parkland Boulevard 800-272-7537 Cleveland, OH 44124-4141 USA FAX - 440-266-7400 email: c-parker@parker.com Introduction Page 7 April 17, 2007 1A13 PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL (8) KEVLAR: Vendor: KEVLAR Special Products E.I. DuPont De Nemours & Co. Inc. Textile Fibers Department Centre Road Building Wilmington, Delaware 19898 A Guide to Cutting and Machining Kevlar Aramid (9) MAGNETOS: Vendor: TCM Aircraft Products PH - 800-718-3411 P. O. Box 90 FAX - 251-432-7352 Mobile, AL 36601 http://www.tcmlink.com/ Installation, Operation Teledyne Continental Motors (TCM) and Maintenance Service Support Manual, P/N X42002 Instructions: S-20 / S-200 Series High Tension Magnetos or, Vendor: Slick Aircraft Products PH: - (904) 739-4000 Unison Industries FAX: - (904) 739-4006 Attn: Subscription Service 7575 Baymeadows Way Jacksonville, FL 32256 http://www.unisonindustries.com/ Installation, Operation F1100 MASTER SERVICE MANUAL, and Maintenance 4300/6300 SERIES MAGNETO MAINTENANCE AND Instructions: OVERHAUL MANUAL - L-1363 (10) OXYGEN SYSTEM: Vendor: AVOX Systems PH - 716-686-1798 2225 Erie Street FAX - 716-686-1597 Lancaster, New York 14086 http://www.avoxsys.com/ Introduction Page 8 April 17, 2007 1A14 PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL (11) PROPELLER: Vendor: Hartzell Propeller Inc. PH - 937-778-4379 One Propeller Place FAX - 937-778-4321 Piqua, OH 45356-2634 http://www.hartzellprop.com/index2.htm Overhaul Instructions: Manual No. 117 or, Vendor: McCauley Propeller Systems 7751 East Pawnee P.O. Box 7704 Wichita, KS 67277-7704 Service Manual: McCauley C500 Series Service Manual - P/N 810915 (12) VOLTAGE CONTROL: Vendor: Lamar Technologies Corp. PH - 360-651-6666 14900 - 40th Ave. N.E. FAX - 360-651-6677 Marysville, WA 98271 http://www.lamartech.com/ (13) WHEELS: (see Brakes, above) Introduction Page 9 April 17, 2007 1A15 PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 12. CHAPTER/SECTION INDEX GUIDE NOTE: The following GAMA Specification No. 2 standard chapters are not included in this Maintenance Manual: 31, 36, 38, 49, 53, 54, 60, 72, 78, and 83. These chapters are omitted because the subject system is either: not installed in these airplanes; adequately covered in vendor or other manuals; or, for ease of use, has been combined with another chapter. CHAPTER SECTION TITLE GRID NO. 4 AIRWORTHINESS LIMITATIONS 1B7 00 Airworthiness Limitations 5 TIME LIMITS/MAINTENANCE CHECKS 5I1 00 General 10 Time Limits 20 Scheduled Maintenance 30 Special Inspections 50 Unscheduled Maintenance Checks 6 DIMENSIONS AND AREAS 1C3 10 Dimensions and Areas 20 Station References 30 Access and Inspection Provisions 7 LIFTING AND SHORING 1C16 00 General 8 LEVELING AND WEIGHING 1C22 10 Leveling 20 Weighing 9 TOWING AND TAXIING 1D5 10 Towing 20 Taxiing 10 PARKING AND MOORING 1D12 10 Parking 20 Mooring 11 REQUIRED PLACARDS 1D18 20 Exterior Placards/Markings 30 Interior Placards/Markings Introduction Page 10 April 17, 2007 1A16 PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL CHAPTER SECTION TITLE GRID NO. 12 SERVICING 1E3 00 General 10 Replenishing 20 Scheduled Servicing 20 STANDARD PRACTICES - AIRFRAME 1F6 00 General 10 Standard Practices - Airframe 21 ENVIRONMENTAL SYSTEMS 1F22 00 General 20 Distribution 40 Heating 50 Cooling 22 AUTO FLIGHT 1J6 00 General 10 Autopilot 23 COMMUNICATIONS 1J13 00 General 10 Emergency Locator Transmitter 24 ELECTRICAL POWER 1J23 00 General 30 DC Generation 40 External Power 50 Electrical Load Distribution 25 EQUIPMENT/FURNISHINGS 2B5 10 Flight Compartment / Passenger Compartment 26 FIRE PROTECTION 2B14 00 General 20 Extinguishing 27 FLIGHT CONTROLS 2B19 00 General 10 Aileron and Tab 20 Rudder and Tab 30 Stabilator Controls 50 Flaps CHAPTER SECTION TITLE GRID NO. Introduction Page 11 April 17, 2007 1A17 PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 28 FUEL 2E11 00 General 10 Storage 20 Distribution 40 Indicating 29 HYDRAULIC POWER 2F24 00 General 10 Main 30 ICE AND RAIN PROTECTION 2H12 00 General 10 Airfoil 30 Pitot and Static 40 Windows, Windshields and Doors 60 Propellers/Rotors 80 Detection 32 LANDING GEAR 3A19 00 General 10 Main Gear and Doors 20 Nose Gear and Doors 30 Extension and Retraction 40 Wheels and Brakes 60 Position and Warning 33 LIGHTS 3D17 00 General 10 Flight Compartment 20 Passenger Compartment 40 Exterior 34 NAVIGATION AND PITOT /STATIC 3E24 00 General 10 Flight Environment Data And Pitot/Static 20 Attitude & Direction 35 OXYGEN 3F21 00 General 10 Crew/Passenger CHAPTER SECTION TITLE GRID NO. Introduction Page 12 April 17, 2007 1A18 PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 37 VACUUM 3H8 00 General 10 Distribution 39 ELECTRICAL/ELECTRONIC PANELS & 3H24 MULTIPURPOSE PARTS 00 General 10 Instrument and Control Panels 51 STRUCTURES 3I14 00 General 10 Structural Repairs 52 DOORS 3J11 00 General 10 Passenger/Crew 30 Cargo 55 STABILIZERS 3J24 00 General 20 Stabilator 30 Vertical Stabilizer 40 Rudder 56 WINDOWS 3K15 10 Flight Compartment 20 Cabin 57 WINGS 3K24 00 General 20 Auxiliary Structure 40 Attach Fittings 50 Flight Surfaces 61 PROPELLERS 4B5 00 General 10 Propeller Assembly 20 Controlling 70 STANDARD PRACTICES — ENGINES 4C9 00 General CHAPTER SECTION TITLE GRID NO. Introduction Page 13 April 17, 2007 1A19 PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 71 POWER PLANT 4C13 00 General 10 Cowling 20 Mounts 60 Air Intakes 73 ENGINE FUEL AND CONTROL 4D11 00 General 10 Distribution 30 Indicating 74 IGNITION 4D19 00 General 10 Electrical Power Supply 20 Distribution 76 ENGINE CONTROLS 4E15 00 General 10 Power Control 77 ENGINE INDICATING 4F6 00 General 10 Power 20 Temperature 79 OIL 4F18 00 General 20 Distribution 30 Indicating 80 STARTING 4G3 00 General 10 Cranking 81 TURBINES 4G13 00 General 20 Turbocharger 91 CHARTS AND WIRING DIAGRAMS 5B3 95 SPECIAL EQUIPMENT 5G9 Introduction Page 14 April 17, 2007 1A20 PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK List of Illustrations Page 1 April 17, 2007 1A21 LIST OF ILLUSTRATIONS FIGURE NO. SUBJECT GRID NO. PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 6-l. Seneca III and IV Three View . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1C8 6-2. Station Reference Lines . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1C10 6-3. Access Plates and Panels . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1C11 7-1. Jacking Arrangement . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1C18 8-l. Leveling Airplane . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1C24 8-2. Weighing Airplane . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1D1 9-1. Aircraft Turning Distance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1D8 11-1. Exterior Placards and Decals . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1D20 11-2. Interior Placards and Decals . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1D21 12-1. Service Points . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1E11 12-2. Fuel Filter Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1E12 12-3. Lubrication Chart (Main Landing Gear) . . . . . . . . . . . . . . . . . . . . . . . 1E23 12-4. Lubrication Chart (Nose Landing Gear) . . . . . . . . . . . . . . . . . . . . . . . 1E24 12-5. Lubrication Chart (Control System) . . . . . . . . . . . . . . . . . . . . . . . . . . . 1F1 12-6. Lubrication Chart (Power Plant and Propeller) . . . . . . . . . . . . . . . . . . 1F3 12-7. Lubrication Chart (Cabin Door, Baggage Door and Seats) . . . . . . . . . 1F4 20-1. Cherrylock Rivet Removal . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1F11 20-2. Hose/Line Markings . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1F12 20-3. Flareless Tube Fittings . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1F14 20-4. Self Lubricating Bearing/Bushing . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1F16 20-5. Torque Wrench Formula . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1F18 21-1. Cabin Heat. Vent and Defrost Systems . . . . . . . . . . . . . . . . . . . . . . . . 1G8 21-2. Heater and Combustion Air Blower Assembly . . . . . . . . . . . . . . . . . . 1G12 21-3. Diagrammatic Cutaway of Heater to Show Whirling Flame Action . . 1G12 21-4. Fuel Regulator and Shutoff Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1G13 21-5. Top View - Duct Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1G13 21-6. Seneca III (14 Volt System) Heater and Defroster Wiring Diagram . . 1G17 21-7. Seneca III (28 Volt System) and Seneca IV Heater and Defroster Wiring Diagram . . . . . . . . . 1G18 21-8. Spark Plug Fixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1G20 21-9. Wiring Test Setup . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1G20 21-10. Spark Plug Gap Adjustment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1G20 21-11. Ignition Unit Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1H1 21-12. Test Setup for Fuel Regulator and Shutoff Valve . . . . . . . . . . . . . . . . . 1H4 21-13. Heater Fuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1H5 21-14. Suggested Design for Seal Plates, Plugs and Caps for Combustion Tube Leakage Test . . . . . . . . . . . . . . . . . . . . . . . . 1H10 21-15. Test Setup for Combustion Air Pressure Switch . . . . . . . . . . . . . . . . . 1H10 21-16. Exploded View of Heater Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . 1H15 21-17. Exploded - View Combustion Air Blower and Motor Assembly . . . . . 1H17 21-18. Suggested Setup of Heater Operation Test . . . . . . . . . . . . . . . . . . . . . . 1H20 21-19. Wiring Connections for Heater Operation Test . . . . . . . . . . . . . . . . . . 1H20 21-20. Air Conditioning System Installation . . . . . . . . . . . . . . . . . . . . . . . . . 1H24 21-21. Service ice Valves . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1I5 21-22. Test Gauge and Manifold Set . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1I6 List of Illustrations Page 2 April 17, 2007 1A22 PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL LIST OF ILLUSTRATIONS (cont.) FIGURE NO. SUBJECT GRID NO. 21-23. Manifold Set Operation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1I7 21-24. Leak Test Hookup . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1I8 21-25. Evacuation Hookup . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1I11 21-26. Charging Stand . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1I12 21-27. Charging Hookup . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1I13 21-28. Top Dead Center Casting Mark (Sankyo Compressor) . . . . . . . . . . . . 1I16 21-29. Rotation of Clutch Front Plate (Sankyo Compressor Oil Check) . . . . 1I16 21-30. Condenser Inlet Scoop Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . 1I20 21-31. Condenser Inlet Scoop Rigging . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1I21 21-32. Expansion Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1I24 21-33. Components Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1J2 23-1. Emergency Locator Transmitter Schematic (Narco) . . . . . . . . . . . . . . 1J17 23-2. ELT Portable Folding Antenna (Narco) . . . . . . . . . . . . . . . . . . . . . . . . 1J18 23-3. ELT Using Fixed Antenna (Narco) . . . . . . . . . . . . . . . . . . . . . . . . . . . 1J18 23-4 Emergency Locator Transmitter Schematic (Narco ELT 910) . . . . . . . 1J21 23-5 ELT 910 Battery Pack . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1J22 24-1. Base Electrical Installation (14 volt system) . . . . . . . . . . . . . . . . . . . . 1K11 24-2. Base Electrical Installation (28 volt system) . . . . . . . . . . . . . . . . . . . . 1K14 24-3. Testing Alternator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1K19 24-4. Internal Wiring Diagram . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1K19 24-5. Battery and Master Relays Installation (14 volt system) . . . . . . . . . . . 1L8 24-6. Battery and Master Relays Installation (28 volt system) . . . . . . . . . . . 1L9 24-7. Control Unit Diagram (14 volt system) . . . . . . . . . . . . . . . . . . . . . . . . 1L10 24-8. Bench Test of Alternator Control Unit - Lamar #B-00382-1 . . . . . . . . 1L10 24-9. Overvoltage Test of ACU (Procedure D) . . . . . . . . . . . . . . . . . . . . . . . 1L11 24-10. Testing Regulator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1L14 24-11. Adjusting Regulator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1L15 24-12. Application of Overvoltage Control . . . . . . . . . . . . . . . . . . . . . . . . . . . 1L16 24-13. Testing Overvoltage Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1L17 25-1. Seats and Console Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2B9 25-2. Seat Back Lock . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2B10 25-3. Lumbar Seat Bladder Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2B12 27-1. Rod End Installation Method . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2B23 27-2. Control Cable Inspection Technique . . . . . . . . . . . . . . . . . . . . . . . . . . 2B24 27-3 Cable Wear Patterns . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2C1 27-4 Internal Cable Wear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2C2 27-5 Pulley Wear Patterns . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2C4 27-6 Control Column Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2C8 27-7. Control Column Rigging . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2C10 27-8. Flex (Universal) Joint Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2C11 27-9 Aileron Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2C12 27-10. Aileron Rigging . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2C16 27-11. Aileron Bellcrank Rigging Tool Utilization . . . . . . . . . . . . . . . . . . . . . 2C16 27-12. Rudder Controls Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2C21 27-13. Rudder Pedals Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2C24 List of Illustrations Page 3 April 17, 2007 1A23 PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL LIST OF ILLUSTRATIONS (cont.) FIGURE NO. SUBJECT GRID NO. 27-14. Rigging Rudder and Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2D2 27-15. Rudder and Stabilator Adjustments . . . . . . . . . . . . . . . . . . . . . . . . . . . 2D8 27-16. Method of Securing Trim Cables . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2D8 27-17. Stabilator Controls Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2D10 27-18. Stabilator Rigging . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2D12 27-19. Stall Warning of Flap Microswitch Adjustment . . . . . . . . . . . . . . . . . . 2D18 27-20. Manually Operated Flap System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2D21 27-21. Rigging of Manual Flap Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2D22 27-22. Electrically Operated Flap System . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2E1 27-21. Rigging of Electrically Operated Flap Controls . . . . . . . . . . . . . . . . . . 2E3 27-24. Rigging of Flap Cam-Cable Assembly . . . . . . . . . . . . . . . . . . . . . . . . 2E4 27-25. Stop Screws Adjustment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2E5 28-1. Fuel System Schematic . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2E17 28-2. Fuel Cell Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2E23 28-3. Flush Fuel Cap Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2F6 28-4. Installation of Locking Fuel Cap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2F7 28-5. Fuel Vent and vapor Return Systems . . . . . . . . . . . . . . . . . . . . . . . . . . 2F8 28-6. Fuel Selector Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2F9 28-7. Fuel Pump. Slide Resistor and Filter Installation . . . . . . . . . . . . . . . . . 2F14 28-8. Fuel Filter Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2F15 28-9. Seneca III Fuel Quantity Indicators . . . . . . . . . . . . . . . . . . . . . . . . . . . 2F19 28-10 Seneca IV Fuel Quantity Indicators . . . . . . . . . . . . . . . . . . . . . . . . . . . 2F20 29-1. Schematic Diagram of Prestolite Hydraulic System . . . . . . . . . . . . . . 2G4 29-2. Schematic Diagram of Oildyne Hydraulic System . . . . . . . . . . . . . . . 2G5 29-3. Hydraulic System Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2G8 29-4. Hydraulic Pump Reservoir. Exploded View (Prestolite) . . . . . . . . . . . 2G18 29-5. Test and Adjustments of Hydraulic Pump . . . . . . . . . . . . . . . . . . . . . . 2G21 29-6. Oildyne Hydraulic Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2G24 29-7. Free Fall Valve Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2H3 29-8. Gear Actuating Cylinder . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2H4 29-9. End Gland locking Device . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2H5 29-10. Nose Gear Actuating Cylinder Installation . . . . . . . . . . . . . . . . . . . . . 2H6 30-1. Pneumatic Deice System Installation . . . . . . . . . . . . . . . . . . . . . . . . . . 2H16 30-2. Electric Prop Deice System Installation . . . . . . . . . . . . . . . . . . . . . . . . 2H18 30-3. Heated Pitot and Stall Warning System Installation . . . . . . . . . . . . . . 2H19 30-4. Pneumatic Deicer Boots Operation . . . . . . . . . . . . . . . . . . . . . . . . . . . 2I2 30-5. Seneca III Deicing Control Panel Installation . . . . . . . . . . . . . . . . . . . 2I2 30-5 Seneca IV Deicing Control Panel Installation . . . . . . . . . . . . . . . . . . . 2I2 30-6. Windshield heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2I18 30-7. Propeller Deicing Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2J1 30-8. Wiring Diagram - Electrical Prop Deicing System (Two Blade) . . . . . 2J4 30-9. Wiring Diagram - Electrical Prop Deicing System (Three Blade) . . . . 2J5 30-10. Cycling Sequences Two Blade . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2J6 Cycling Sequences Three Blade . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2J8 30-11. Use of Dial Indicator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2J10 List of Illustrations Page 4 April 17, 2007 1A24 PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL LIST OF ILLUSTRATIONS (cont.) FIGURE NO. SUBJECT GRID NO. 30-12. Measuring Brush Assemblies . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2J10 30-13. Brush Module Assembly 3E1011 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2J11 30-14. Alternate Module Stacking Arrangement . . . . . . . . . . . . . . . . . . . . . . . 2J11 30-15. Tolerances for Brush Assemblies . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2J12 30-16. Centering of Brushes on Slip Rings . . . . . . . . . . . . . . . . . . . . . . . . . . . 2J12 30-17. Brush Block Alignment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2J13 30-18. Modular Brush Assembly 3E2042-1 (2 Bladed Prop) . . . . . . . . . . . . . 2J14 30-19. Modular Brush Assembly 3E2062-2 (3 Bladed Prop) . . . . . . . . . . . . . 2J14 30-20. Installation of Deicer Boot . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2J16 30-21. Wrinkled Deicers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2J20 30-22. Sealer Application (Boot) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2J20 30-23. Two Bladed Propeller Harness Installation . . . . . . . . . . . . . . . . . . . . . 2J22 30-24. Three Bladed Propeller Harness Installation . . . . . . . . . . . . . . . . . . . . 2J23 30-25. Ice Detection Light Schematic . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2K1 32-1. Main Gear Oleo Strut Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3B8 32-2. Main Landing Gear Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3B12 32-2A. Main Gear Trunnion Inspection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3B15 32-3. Aligning Main Gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3B18 32-4. Toe-In/Toe-Out Adjustment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3B19 32-5. Nose Gear Oleo Strut Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3B24 32-6. Nose Gear Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3C4 32-7. Drag Link Installation and Adjustment . . . . . . . . . . . . . . . . . . . . . . . . 3C8 32-8. Service Wear Limits . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3C9 32-9. Tunnel Bracket Installation Inspection . . . . . . . . . . . . . . . . . . . . . . . . . 3C12 32-10. Nose Gear Trunnion Inspection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3C13 32-11. Clamping Rudder Pedals in Neutral Position . . . . . . . . . . . . . . . . . . . . 3C14 32-12. Rudder Pedals at Neutral Angle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3C14 32-13. Nose Wheel Assembly (Typical) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3C21 32-14. Main Wheel Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3C23 32-15. Wheel Brake Assembly – 30-65 and 30-83 . . . . . . . . . . . . . . . . . . . . . 3D1 32-16. Removal and Installation of Anchor Bolts . . . . . . . . . . . . . . . . . . . . . . 3D2 32-17. Brake Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3D4 32-18. Parking Brake Valve Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3D6 32-19. Gar-Kenyon 17000 Toe Brake Cylinder . . . . . . . . . . . . . . . . . . . . . . . . 3D7 32-20. Cleveland 10-30 Toe Brake Cylinder . . . . . . . . . . . . . . . . . . . . . . . . . . 3D7 32-21. Brake Reservoir Bleeding . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3D10 32-22. Bleeding Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3D10 32-23. Adjust Nose Gear Down Limit Switch . . . . . . . . . . . . . . . . . . . . . . . . 3D11 32-24. Adjust Main Gear Down Limit Switch . . . . . . . . . . . . . . . . . . . . . . . . 3D12 32-25. Throttle Warning Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3D15 33-1. Reading and Courtesy Light Assembly (Whelen) . . . . . . . . . . . . . . . . 3E12 33-2. Strobe Installation Connections - Seneca III (Sheet 1 of 2) . . . . . . . . . 3E17 33-2. Strobe Installation Connections - Seneca IV (Sheet 2 of 2) . . . . . . . . . 3E18 33-3. Landing Light Adjustment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3E22 34-1. Pitot-Static System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3F4 List of Illustrations Page 5 April 17, 2007 1B1 PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL LIST OF ILLUSTRATIONS (cont.) FIGURE NO. SUBJECT GRID NO. 34-2. King Radar Altimeter Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3F10 34-3. Bonzer Radar Altimeter Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . 3F10 35-1. Fixed Oxygen System Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3G1 35-2. Test Apparatus for Testing Oxygen System . . . . . . . . . . . . . . . . . . . . . 3G6 35-3. Oxygen Tubing Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3G7 35-4. Installation of Swagelock Fittings . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3G10 35-5. Oxygen Cylinder and Regulator Assembly (S/N’s 34-8133001 thru 34-8333129, 34-8433003 thru 34-8433009, 34-8433011, 34-8433014 thru 34-8433024) . . . . . . . . . . . . . . . . . 3G13 35-6. Oxygen Cylinder and Regulator Assembly (Seneca III models, S/N’s 34-8433001, 34-8433002, 34-8433010, 34-8433012, 34-8433013, 34-8433025 and up, and 3448001 thru 3448037; Seneca IV airplanes S/N’s 3448038 and up) . . . . . . . . . . . . . . . . . 3G14 35-7. Oxygen System Recharge Valve Installation (S/N’s 34-8133001 thru 34-8333129, 34-8433003 thru 34-8433009, 34-8433011, 34-8433014 thru 34-8433024) . . . . . . . . . . . . . . . . . 3G15 35-8. Oxygen System Recharge Valve Installation (Seneca III models, S/N’s 34-8433001, 34-8433002, 34-8433010, 34-8433012, 34-8433013, 34-8433025 and up, and 3448001 thru 3448037, Seneca IV airplanes S/N’s 3448038 and up) . . . . . . . . . . . . . . . . . 3G16 35-9. Oxygen Pressure Gauge Installation . . . . . . . . . . . . . . . . . . . . . . . . . . 3G19 35-10. Oxygen Installation (Portable) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3H3 37-1. Standard Gyro Vacuum System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3H13 37-2. Seneca III Gyro and Pneumatic System (Optional) . . . . . . . . . . . . . . . 3H14 37-3. Seneca IV Gyro and Pneumatic System (Optional) . . . . . . . . . . . . . . . 3H15 37-4 Vacuum Regulator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3H17 39-1. Typical Instrument Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 314 39-2. Seneca III, 14 Volt System Circuit Breaker Panel . . . . . . . . . . . . . . . . 3I7 39-3. Seneca III, 14 Circuit Breaker Installation . . . . . . . . . . . . . . . . . . . . . . 3I8 39-4. Seneca III, 28 Volt System Circuit Breaker Panel . . . . . . . . . . . . . . . . 3I9 39-5. Seneca IV Circuit Breaker Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3I10 39-6. Seneca III, 28 Vdc Models, and Seneca IV Circuit Breaker Panel Installation (28 volt system) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3I11 51-1. Skin Material and Thickness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3I19 51-2. Surface Scratches, Abrasions or Ground-in-Dirt . . . . . . . . . . . . . . . . . 3I24 51-3. Deep Scratches, Shallow Nicks and Small Holes . . . . . . . . . . . . . . . . 3J1 51-4. Mixing of Epoxy Patching Compound . . . . . . . . . . . . . . . . . . . . . . . . . 3J1 51-5. Welding Repair Method . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3J2 51-6. Repairing of Cracks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3J3 51-7. Various Repairs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3J4 51-8. Stress Lines . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3J5 51-9. Repair of Impacted Damage . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3J5 List of Illustrations Page 6 April 17, 2007 1B2 PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL LIST OF ILLUSTRATIONS (cont.) FIGURE NO. SUBJECT GRID NO. 52-1. Snubber Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3J14 55-1. Empennage Assemblies . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3K3 55-2. Blocking Control Cables . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3K6 55-3. Stabilator Balancing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3K7 55-4. Rudder Balancing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3K12 56-1. Windshield Installation (Typical) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3K18 56-2. Side Window Installation. Single Pane (Typical) . . . . . . . . . . . . . . . . . 3K19 56-3. Cabin Door Window Installation (Typical) . . . . . . . . . . . . . . . . . . . . . 3K20 57-1. Wing Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3L5 57-2. Aileron and Flap Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3L11 57-3. Aileron Balance Configuration . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3L13 61-1. Blade Inspection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4B11 61-2. Hartzell Two Bladed Propeller Installation . . . . . . . . . . . . . . . . . . . . . 4B13 61-3. McCauley Three Bladed Propeller Installation . . . . . . . . . . . . . . . . . . 4B14 61-4. Rigging Propeller Governor . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4B19 61-5. Propeller Synchrophaser Installation With Pulse Generator (Seneca III S/N’s 34-8133002 thru 34-8133172) . . . . . . . . . . . . . 4B20 61-6. Pulse Generator Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4B23 61-7. Propeller Synchrophaser Installation (Magnetic Pickup) (S/N’ 34-8133001, 34-8133173 through 34-8633031, 3433001 and up, and 3448001 and up) . . . . . . . . . . . . . . . . . . . . . 4C2 61-8. Magnetic Pickup and Governor Installation . . . . . . . . . . . . . . . . . . . . . 4C3 61-9. Magnet Assemblies . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4C4 61-10. Propeller Unfeathering Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . 4C8 71-1. Engine Cowling Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4C23 71-2. Power Plant Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4D2 71-3. Induction System Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4D5 71-4. Cowl Flap Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4D7 73-1. Schematic Diagram of Fuel Injection System . . . . . . . . . . . . . . . . . . . 4D14 73-2. Fuel Injector Nozzle Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4D15 74-1. Magneto Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4D22 74-2. Contact Spring Inspection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4D24 74-3. Contact Points . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4D24 74-4. Impulse Coupling . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4E2 74-5. Flyweight Clearance of Impulse Coupling . . . . . . . . . . . . . . . . . . . . . 4E2 74-6. Engine Timing Marks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4E4 74-7. Ignition Schematic . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4E9 74-8. Removing Frozen Spark Plug . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4E10 76-1. Engine Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4E19 76-2. Exhaust Bypass Valve Screw . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4E21 76-3. Idle Speed and Mixture Adjustment Points . . . . . . . . . . . . . . . . . . . . . 4E22 76-4. Sectional View of Altitude Compensating Fuel Pump Assembly . . . . 4E24 77-1. Engine Instrument Lines Installation . . . . . . . . . . . . . . . . . . . . . . . . . . 4F8 77-2. Electric Tachometer Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4F12 79-1. Oil Filter Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4F21 List of Illustrations Page 7 April 17, 2007 1B3 PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL LIST OF ILLUSTRATIONS (cont.) FIGURE NO. SUBJECT GRID NO. 80-1. Exploded View of Starting Motor . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4G10 81-1. Removing Compressor Housing From Turbocharger . . . . . . . . . . . . . 4G21 81-2. Measuring Turbine Shaft End Play . . . . . . . . . . . . . . . . . . . . . . . . . . . 4G21 81-3. Measuring Turbine Shaft Radial Play . . . . . . . . . . . . . . . . . . . . . . . . . 4G21 81-4. Exhaust Bypass Screw . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4G23 81-5. Schematic Diagram of Turbocharger System . . . . . . . . . . . . . . . . . . . . 4G24 NOTE: Refer to Chapter 91 For Electrical Schematic Index 95-1. Control Surfaces Balancing Tool . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5G11 95-2. Tire Balancer Fixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5G12 95-3. Aileron Bellcrank Rigging Tool . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5G13 95-4. Aileron and Flap Rigging Tool . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5G13 95-5. Stabilator Rigging Tool . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5G14 95-6. Rudder Rigging Tool . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5G15 95-7. Heater Plug Gap Adjustment Tool . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5G16 95-8. Fabricated Tool For Baggage Door Lock . . . . . . . . . . . . . . . . . . . . . . . 5G17 List of Illustrations Page 8 April 17, 2007 1B4 PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK List of Charts Page 1 April 17, 2007 1B5 PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL LIST OF CHARTS CHART NO. SUBJECT GRID NO. 601 Leading Particulars and Principal Dimensions . . . . . . . . . . . . . . . . . . 1C5 2001 Maximum Distance Between Fluid Tubing Supports . . . . . . . . . . . . . 1F15 2002 Maximum Allowable Resistance Values . . . . . . . . . . . . . . . . . . . . . . . 1F18 2101 Troubleshooting Heater . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1G3 2102 Blower System Wire Color Codes . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1G9 2103 Inspection (Ignition Unit) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1H2 2104 Temperature Pressure Chart . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1I2 2105 Aluminum Tubing Torque . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1I4 2401 Troubleshooting (Alternator) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1K3 2402 Alternator Specifications . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1K20 2403 Troubleshooting (Battery) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1K21 2404 Hydrometer Reading and Battery Charge Percent . . . . . . . . . . . . . . . . 1L2 2405 Electrolyte Temperatuire Corrections . . . . . . . . . . . . . . . . . . . . . . . . . 1L2 2406 Specific Gravity Temperature Corrections . . . . . . . . . . . . . . . . . . . . . . 1L2 2407 Discharge Rates . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1L3 2408 Electrolyte Freezing Points . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1L4 2409 Electrical System Component Loads . . . . . . . . . . . . . . . . . . . . . . . . . . 1L18 2701 Cable Tension Vs. Ambient Temperature . . . . . . . . . . . . . . . . . . . . . . . 2B23 2702 Troubleshooting Aileron Control System . . . . . . . . . . . . . . . . . . . . . . 2C6 2703 Troubleshooting Rudder Control System . . . . . . . . . . . . . . . . . . . . . . . 2C18 2704 Troubleshooting Stabilator Control System . . . . . . . . . . . . . . . . . . . . . 2D6 2705 Troubleshooting Stabilator Manual Trim Control . . . . . . . . . . . . . . . . 2D7 2706 Troubleshooting Flap Control System . . . . . . . . . . . . . . . . . . . . . . . . . 2D19 2801 Troubleshooting (Fuel System) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2E15 2802 Fuel Quantity Sender Gauge Tolerances (Seneca III) . . . . . . . . . . . . . 2F19 2803 Fuel Quantity Sender Gauge Tolerances (Seneca IV) . . . . . . . . . . . . . 2F20 2901 Leading Particulars, Hydraulic Pump - Prestolite . . . . . . . . . . . . . . . . 2G6 2902 Leading Particulars, Hydraulic Pump - Oildyne . . . . . . . . . . . . . . . . . 2G6 2903 Troubleshooting (Hydraulic System) . . . . . . . . . . . . . . . . . . . . . . . . . . 2G9 2904 Characteristics, Hydraulic Pump Motor - Prestolite . . . . . . . . . . . . . . 2G14 2905 Characteristics, Hydraulic Pump Motor - Oildyne . . . . . . . . . . . . . . . 2G15 3001 Troubleshooting Pneumatic Deice System . . . . . . . . . . . . . . . . . . . . . 2H21 3002 Operating Pressures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2H23 3003 Material and Supplies for Cold Repair . . . . . . . . . . . . . . . . . . . . . . . . . 2I5 3004 Troubleshooting Propeller Deicer System . . . . . . . . . . . . . . . . . . . . . . 2I24 3005 Required Materials for Repair of Propeller Deicer . . . . . . . . . . . . . . . 2J17 3006 Mixing of Material . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2J19 3007 Electrical Resistance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2J19 3201 Troubleshooting Landing Gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3B3 3202 Toe-In Toe-Out Correction Chart . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3B19 3301 Seneca III Annunciator Panel Function Descriptions (14 Volt System) 3E2 3302 Seneca III Annunciator Panel Function Descriptions (28 Volt System) 3E4 3303 Seneca IV Annunciator Panel Function Descriptions . . . . . . . . . . . . . 3E5 3304 Annunciator Panel Troubleshooting . . . . . . . . . . . . . . . . . . . . . . . . . . . 3E7 List of Charts Page 2 April 17, 2007 1B6 PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL LIST OF CHARTS (cont.) CHART NO. SUBJECT GRID NO. 3401 Troubleshooting Vertical Speed Indicator . . . . . . . . . . . . . . . . . . . . . . 3F5 3402 Troubleshooting Altimeter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3F6 3403 Troubleshooting Airspeed Tubes and Indicator . . . . . . . . . . . . . . . . . . 3F11 3404 Troubleshooting Attitude Deviation Indicator . . . . . . . . . . . . . . . . . . . 3F14 3405 Troubleshooting Heading (Directional Gyro) Indicator . . . . . . . . . . . . 3F15 3406 Troubleshooting Magnetic Compass . . . . . . . . . . . . . . . . . . . . . . . . . . 3F16 3407 Troubleshooting Turn Indicator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3F18 3501 Troubleshooting (Oxygen System) . . . . . . . . . . . . . . . . . . . . . . . . . . . 3G3 3502 Fixed Oxygen System Component Limits . . . . . . . . . . . . . . . . . . . . . . 3G11 3503 Filling Pressures for Certain Ambient Temperatures . . . . . . . . . . . . . . 3H1 3504 Portable Oxygen System Component Limits . . . . . . . . . . . . . . . . . . . . 3H2 3701 Troubleshooting Vacuum System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3H10 5101 List of Materials (Thermoplastic Repair) . . . . . . . . . . . . . . . . . . . . . . . 3I23 6101 Propeller Specifications . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4B15 6102 Hartzell Propeller Chamber Pressure Requirements with Temperature for Counterweight Type Propeller . . . . . . . . . . . . . . 4B15 7101 Engine Data . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4C15 7102 Troubleshooting Engine . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4C16 7301 Troubleshooting Fuel Flow Gauge . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4D17 7601 Fuel Flow vs. Engine Speed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4F1 7602 Fuel Flow vs. Fuel Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4F4 7603 Limits - Fuel Flow vs. Brake HP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4F4 7701 Troubleshooting Manifold Pressure Indicator . . . . . . . . . . . . . . . . . . . 4F10 7702 Troubleshooting Electric Tachometer . . . . . . . . . . . . . . . . . . . . . . . . . 4F11 7703 Troubleshooting Exhaust Gas Temperature Gauge . . . . . . . . . . . . . . . 4F15 7704 Troubleshooting Cylinder Head Temperature Gauge . . . . . . . . . . . . . . 4F15 7901 Troubleshooting Engine Oil Pressure Gauges . . . . . . . . . . . . . . . . . . . 4F23 7902 Troubleshooting Engine Oil Temperature Gauges . . . . . . . . . . . . . . . . 4F24 8001 Troubleshooting Starter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4G5 8002 Starting Motor Specifications (TCM 634592) . . . . . . . . . . . . . . . . . . . 4G11 8003 Starting Motor Specifications (TCM 646275) . . . . . . . . . . . . . . . . . . . 4G11 8101 Troubleshooting Turbocharger . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4G15 8102 Turbocharger Nomenclature . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4G16 9101 Flare Fitting Torques . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5B7 9102 Recommended Torque Values . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5B8 9103 Conversion Tables . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5B11 9104 Decimal Conversions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5B15 9105 Decimal Millimeters Equivalents of Drill Sizes . . . . . . . . . . . . . . . . . . 5B16 9106 List of Consumable Materials . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5B17 9107 Electrical Wire Coding . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5B22 9108 Electrical Symbols . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5B23 1B7 PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL CHAPTER 4 AIRWORTHINESS LIMITATIONS 1B8 PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 4-Cont./Effec. Page 1 April 17, 2007 1B9 CHAPTER 4 - AIRWORTHINESS LIMITATIONS TABLE OF CONTENTS/EFFECTIVITY CHAPTER/ SECTION SUBJECT GRID NO. EFFECTIVITY 4-00-00 AIRWORTHINESS LIMITATIONS 1B11 2R0407 Limitations 1B11 A0407 Inspections 1B11 A0407 Life Limited Parts Marking and Disposition 1B11 A0407 PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 4-Cont./Effec. Page 2 April 17, 2007 1B10 THIS PAGE INTENTIONALLY BLANK 4-00-00 Page 1 April 17, 2007 1B11 PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL AIRWORTHINESS LIMITATIONS NOTE: The Airworthiness Limitations section is FAA approved and specifies maintenance required under §§ 43.16 and 91.403 of the Federal Aviation Regulations unless an alternative program has been FAA approved. 1. LIMITATIONS (PIR-TCDS A7SO, Rev. 17.) NOTE: Refer to the LIMITATIONS section in the Pilot’s Operating Handbook for a detailed delineation of the flight limitations of the airplane. The following limitations related to the fatigue life of the airplane and its components have been established for the PA-34-220T Seneca III /IV airplane: The bolt and stack-up that connect the upper drag link to the nose gear trunnion are required to be replaced every 500 hours time-in-service. The part numbers are as follows: (1) P/N 400-274 (AN7-35) bolt or P/N 693-215 (NAS6207-50D) bolt; (2) P/N 407-591 (AN960-716L) washer, as applicable; (3) P/N 407-568 (AN 960-716) washer, as applicable; (4) P/N 404-396 (AN 320-7) nut; and (5) P/N 424-085 cotter pin. 2. INSPECTIONS Refer to 5-20-00 for Piper’s recommended Inspection Program. 3. LIFE LIMITED PARTS MARKING AND DISPOSITION 14 CFR Part 43.10, Disposition of Life-Limited Aircraft Parts requires that proper procedures are followed when removing life limited parts with time and/or cycles remaining on them as well as the disposition of life limited parts with no time and/or cycles left. Life limited parts defined by Type Certificate (TC) are listed in paragraph 1, above. Other parts which are replaced or rebuilt at specified intervals are listed in Chapter 5. A. Parts that are removed prior to accumulating their life limit, are to be marked with indelible ink or marker with the part number, serial number and accumulated life status as defined in 14 CFR Part 43.10 in a manner that does not affect part structural integrity, i.e. - no surface deformation such as vibration/etching allowed. B. Parts that have accumulated the life limit shall be disposed of in accordance with the applicable FARs. Piper recommends life limited parts with no time and/or cycles remaining be completely destroyed. 4-00-00 Page 2 April 17, 2007 1B12 PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL CHAPTER 5 TIME LIMITS / MAINTENANCE CHECKS (MOVED TO GRID 5I1) 1B13 1B14 PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL GRIDS 1B14 THRU 1C2 INTENTIONALLY BLANK CHAPTER 6DIMENSIONS AND AREAS 1C3 CHAPTER 6 - DIMENSIONS AND AREAS TABLE OF CONTENTS/EFFECTIVITY CHAPTER SECTION SUBJECT GRID NO. EFFECTIVITY SUBJECT 6-10-00 DIMENSIONS 1C5 6-20-00 STATION REFERENCE LlNES 1C9 6-20-00 WEIGHT AND BALANCE DATE 1C9 6-20-00 SERIAL NUMBER PLATE 1C9 6-30-00 ACCESS PLATES AND INSPECTION PROVISIONS 1C11 PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 6- Cont./Effec. Page 1 Reissued: November 29, 1993 1C4 PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 6-10-00 Page 1 Reissued: November 29, 1993 1C5 DIMENSIONS The principal airplane dimensions are shown in Figure 6-1 and are listed in Chart 601. CHART 601. LEADING PARTICULARS AND PRINCIPAL DIMENSIONS MODEL PA-34-220T SENECA III and IV ENGINE Manufacturer Continental Model - Left (12V) TSIO-360-KB (CW) Model - Right (12V) LTSIO-360-KB (CCW) TSIO-360-KB-1A TSIO-360-KB2 TSIO-360-KB2 Model - Left (24V) TSIO-360-KB11 (CW) Model - Right (24V) LTSIO-360-KB7 (CCW) Model - Left, with primer standard (24V) TSIO-360-KB28 (CW) Model - Right, with primer standard (24V) LTSIO-360-KB14 (CCW) FAA Type Certificate E9CE Rated Horsepower ( Sea Level) Max. Takeoff - 5 minute maximum 220 HP Max. Continuous 200 HP Rated Speed - RPM Max. Takeoff - 5 minute maximum 2800 RPM Max. Continuous 2600 RPM Oil SAE Number See Lubrication Chart Oil Sump Capacity 8 U.S. quarts Fuel: Aviation Grade - Minimum Octane 100 or 100LL Fuel Injector Continental Magnetos. Scintilla Left (Left Engine) 10-79020-18L Right (Right Engine) 10-79020-19R Magnetos: (Bendix Pressurized) 79020-118 Left (Left Engine) S6LN-25 Right (Right Engine) S6RN-25 Magneto Timing 20° BTC Magneto Point Clearance .018 + .006 Spark Plugs (Shielded): Refer to latest revision of Teledyne Continental Aircraft Engine Service Bulletin M77-10 Spark Plug Gap Setting .015 to .019 Firing Order: Left Engine 1-6-3-2-5-4 Right Engine 1-4-5-2-3-6 Starter - Prestolite (12-volt): Left Engine MCL-6501 Right Engine MCL-6501 PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 6-10-00 Page 2 Reissued: November 29, 1993 1C6 CHART 601. LEADING PARTICULARS AND PRINCIPAL DIMENSIONS (continued) MODEL PA-34-220T SENECA III and IV ENGINE (continued) Starter - Prestolite (28-volt): Left Engine 646275 Right Engine 646275 Alternator - Prestolite (65 amp) ALX-9402 Alternator - Teledyne Critten (60 amp) Left Engine 649280 or 653344 Right Engine 649280 or 653344 Alternator Voltage Regulator - Lamar (12V) B-00288-1 Alternator Control Unit - Lamar (28V) B-00382-1 Alternator Overvoltage Relay, (12V) WICO DIVISION, Prestolite FOC-4002B PROPELLER Manufacturer Hartzell McCauley Hub Model: Left Engine BHC-C2YF-2CKUF (Left Eng.) 1 3AF32C508 Right Engine BHC-C2YF-2CLKUF (Right Eng.) 1 3AF32C509 Blade Model: Left Engine FC8459-8R 82NFA-6 Right Engine FJC8459-8R L82NFA-6 Diameter, Minimum 75 in. 75 in. Blade Angle, Low Pitch (High RPM) 12.6° ± 0.2° 11.0° ± 0.2° Blade Angle, High Pitch (Low RPM) 80° to 81.5° 81.0° to 83.5° Governor Models: Left Engine E-3-7 Right Engine E-3-7L (E-8-7L) 2 FUEL SYSTEM Fuel Tank 49 gal./wing 64 gal./wing 3 Total Capacity (Both Wings) 98 gal. 128 gal. 3 Total Usable Fuel 93 gal. 123 gal. 3 1 Propellers To Be Mounted In Pairs Only. Do Not Mix With Other Propellers. 2 With Synchrophaser Installation Only 3 With Optional Fuel Tanks Installed on Seneca III; Standard on Seneca IV PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 6-10-00 Page 3 Reissued: November 29, 1993 1C7 CHART 601. LEADING PARTICULARS AND PRINCIPAL DIMENSIONS (continued) MODEL PA-34-220T SENECA III and IV LANDING GEAR Thread (Width From Each Tire Center) 11.1 ft. Turning Radius 60.4 ft. Nose Gear Strut Combination Air-Oil Nose Tire Pressure 40 PSI @ Gross Weight, 34 PSI 4 Nose Gear Travel 27 degrees LEFT or RIGHT Main Gear Strut Combination Air-Oil Main Tire Pressure 55 PSI @ Gross Weight, 46 PSI 4 Brakes Cleveland 30-65 or 30-83 4 Tires: Main 6.00 x 6, 8 ply or Nylon TT 4 Nose 6.00 x 6, 6 ply or Nylon TT 4 4 With Heavy Duty Brakes, Wheels And Either B.F. Goodrich Nylon T. T. Type III Tires Or McCleary Air Hawk Type III. Figure 6-1. Seneca III and IV Three View PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 6-10-00 Page 4 Reissued: November 29, 1993 1C8 C400 POH STATION REFERENCE LINES In order to facilitate the location of various components of the airplane which require maintenance and ser- vicing, a method utilizing fuselage station (Sta.) wing station of buttock line (BL), or waterline (WL) designa- tions is frequently employed in this manual. (Refer to Figure 6-2). Fuselage stations, buttock lines, and water- lines are reference points measured by inches in the vertical or horizontal direction from a given reference line which indicates station locations of structural members of the airplane. WEIGHT AND BALANCE DATA When figuring various weight and balance computations, the empty weight, static and gross weight, and center of gravity of the airplane may be found in the Weight and Balance Form of the Airplane Flight Manual. SERIAL NUMBER PLATE The serial number plate is located on the fuselage near the leading edge of the stabilator. The serial num- ber should always be used when referring to the airplane on service or warranty matters. PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 6-20-00 Page 1 Reissued: November 29, 1993 1C9 Figure 6-2 Station Reference Lines PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 6-20-00 Page 2 Reissued: November 29, 1993 1C10 B.L. 81.35 B.L. 76.98 W.S. 144.08 N.S. 67.5 W.S. 232.95 W.S. 24.24 B.L. 0 W.S. 71.52 N.B.L. 0 W.S. 240.32 N.S. 82.26 N.S. 36.5 F.S. -27.5 W.L. 19.75 F.S. 165.72 W.L. 52.83 W.L. 0.58 F.S. 53.6 F.S. 138.63 F.S. 24.58 F.S. 49.5 F.S. 109.73 W.L. 107.25 F.S. 187.8 F.S. 184.96 F.S. 275.23 F.S. 285.84 W.L. 95.13 W.L. 61.03 F.S. 293.08 3050 ACCESS PLATES AND INSPECTION PROVISIONS The access and inspection provisions for the airplane are shown in Figure 6-3. The component to be serviced or inspected through each opening is identified in the illustration. All Access plates and panels are secured by either metal fasteners or screws. To enter the aft section of the fuselage, remove the rear trim panel. Figure 6-3 Access Plates and Panels PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 6-30-00 Page 1 Reissued: November 29, 1993 1C11 SKETCH C SKETCH D 2 1 4 3 1 4 2 5 3 1. VENTILATING AIR INTAKE 2. FAIRING FIN 3. BATTERY, BRAKE RESERVOIR, ELECTRONIC EQUIPMENT, HYDRAULIC POWER PACK 4. RUDDER TRIM TAB SCREW 5. STABILATOR AND RUDDER STOPS, STABILATOR TRIM TAB SCREW 1. FAIRING FIN 2. VENTILATING AIR INTAKE 3. STABILATOR AND RUDDER STOPS, STABILATOR TRIM TAB SCREW 4. COMBUSTION HEATER, COMBUSTION AIR INTAKE Figure 6-3 Access Plates and Panels (continued) PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 6-30-00 Page 2 Reissued: November 29, 1993 1C12 1 3 2 11 10 9 8 11 5 9 6 3 4 2 7 1 10 2 3 4 3 2 6 14 7 15 8 12 9 15 15 1 1 11 11 10 10 14 12 13 1 2 1 6 2 3 4 5 5 SKETCH E SKETCH F SKETCH B SKETCH A 1. WING TIP 2. CAP, FUEL TANK ASSEMBLY 3. FAIRING 4. OIL FILLER DOOR 5. FAIRING 6. LINES, WIRES, CABLES 7. COWL, INBOARD 8. SPINNER, PROPELLER 9. PROPELLER RECHARGE VALVE 10. COWL, OUTBOARD 11. HATCH, NACELLE 1. FUEL GAUGE SENDER 2. COWL FLAP 3. PROPELLER RECHARGE VALVE 4. SPINNER, PROPELLER 5. ENGINE OIL DRAIN 6. LINES, WIRES, CABLES 7. FAIRING 8. DOOR, MAIN GEAR, LANDING 9. COVER, GEAR ATTACHMENT FITTING 10. ELECTRIC WIRING 11. FUEL VALVE 12. COVER, BELLCRANK AND CONTROL CABLE 13. WING TIP 14. STALL WARNING & DEICER BOOTS 15. PITOT HEAT WIRING - AILERON CABLES DEICER LINES 1. DOOR, NOSE GEAR, LANDING 2. HYDRAULIC PRESSURE SWITCH, NOSE GEAR ACTUATING CYLINDER AND LIMIT SWITCH, VOLTAGE REGULATORS 1. BATTERY 2. NOSE LANDING GEAR 3. MAIN SPAR 4. BRAKE RESERVOIR 5. EXTERNAL POWER PLUG 6. RADIO GRIDS 1C13 THRU 1C15 INTENTIONALLY LEFT BLANK PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 1C13 CHAPTER 7 LIFTING AND SHORING 1C16 CHAPTER 7 - LIFTING AND SHORING TABLE OF CONTENTS/EFFECTIVITY CHAPTER SECTION SUBJECT GRID NO. EFFECTIVITY 7-00-00 GENERAL 1C18 7-00-00 Jacking 1C18 PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 7- Cont./Effec. Page 1 Reissued: November 29, 1993 1C17 GENERAL Jacking the airplane is necessary to perform servicing of the landing gear and the operations. The jacking operation can be performed through the use of conventional tripod jacks, or in other situations, (emergency, post-accident lifting), slings or air bags should be used. If wing and/or fuselage shoring is required, make sure the support is contoured to conform with the surface it is supporting. JACKING (Refer to Figure 7-1.) 1. Align the jacks under the wings with their respective pads on the wing front spar. 2. Attach a tail stand with approximately 600 pounds ballast, to the tail skid. — CAUTION — ENOUGH SUPPORT BALLAST MUST BE ADDED TO THE TAILSTAND TO PREVENT THE AIRPLANE FROM TIP- PING FORWARD ON ITS NOSE SECTION. MAKE SURE TO ACCOUNT FOR SOMEONE IN THE FUSELAGE IF APPLICABLE. 3. Carefully raise jacks until all three wheels are clear of the surface. — CAUTION — IF THE HYDRAULIC SYSTEM IS TO BE SERVICED AT THIS POINT, THE FREE FALL KNOB SHOULD BE PULLED OUT. FOR FURTHER INFORMATION, REFER TO CHAPTER 32. Figure 7-1. Jacking Arrangement PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 7-00-00 Page 1 Reissued: November 29, 1993 1C18 3033 GRIDS 1C19 THRU 1C21 INTENTIONALLY LEFT BLANK PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 1C19 CHAPTER 8 LEVELING AND WEIGHING 1C22 CHAPTER 8 - LEVELING AND WEIGHING TABLE OF CONTENTS/EFFECTIVITY CHAPTER SECTION SUBJECT GRID NO. EFFECTIVITY 8-10-00 LEVELING 1C24 8-20-00 WEIGHING 1D1 PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 8 - Cont./Effec. Page 1 Reissued: November 29, 1993 1C23 LEVELING (Refer to Figure 8-1.) The airplanes are provided with a means for longitudinal and lateral leveling. The airplanes may be leveled while on jacks, during the weighing procedure while the wheels are on the scales, or while the wheels are on the ground. To level the airplane for purposes of weighing or rigging, the following procedures may be used: 1. To longitudinally level the airplane, partially withdraw the two leveling screws located immediately below the left front side window. Place a level on these screw heads and adjust the jacks until the level is centered. Should the airplane be either on scales or on the floor, first block the main gear oleos to full extension; then deflate the nose wheel until the proper position is reached. 2. To laterally level the airplane, place a level across the baggage compartment floor along the rear bulk- head. Raise or lower one wing tip by deflating the appropriate tire on the high side of the airplane or adjust either jack until the bubble of the level is centered. Figure 8-1. Leveling Airplane PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 8-10-00 Page 1 Reissued: November 29, 1993 1C24 LONGITUDINALLY LATERALLY LEVELING SCREWS A368 WEIGHING (Refer to Figure 8-2.) The airplane may be weighed by the following procedure: 1. Position a scale and ramp in front of each of the three wheels. 2. Secure the scales from rolling forward and tow the airplane onto the scales. 3. Remove the ramp so as not to interfere with the scales. 4. If the airplane is to be weighed for weight and balance computations, level the airplane. Figure 8-2. Weighing Airplane PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 8-20-00 Page 1 Reissued: November 29, 1993 1D1 3031 GRIDS 1D2 THRU 1D4 INTENTIONALLY LEFT BLANK PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 1D2 CHAPTER 9 TOWING AND TAXIING 1D5 CHAPTER 9 - TOWING AND TAXIING TABLE OF CONTENTS/EFFECTIVITY CHAPTER SECTION SUBJECT GRID NO. EFFECTIVITY SUBJECT 9-10-00 TOWING 1D7 9-20-00 TAXIING 1D8 PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 9 - Cont./Effec. Page 1 Reissued: November 29, 1993 1D6 TOWING The airplane may be moved either by using the nose wheel steering bar that is stowed below the forward ledge of the baggage compartment or by using power equipment that will not damage or cause excess strain to the nose gear steering assembly. The tow bar engages front axle inside fork. — CAUTION — WHEN TOWING WITH POWER EQUIPMENT, DO NOT TURN THE NOSE GEAR IN EITHER DIRECTION BEYOND ITS STEERING RADIUS LIMITS AS THIS WILL RESULT IN DAMAGE TO THE NOSE AND STEERING MECHANISM. WHEN MOVING THE AIRCRAFT FORWARD BY HAND, AVOID PUSHING ON THE TRAILING EDGE OF THE AILERONS AS THIS WILL CAUSE THE AILERON CON- TOUR TO CHANGE RESULTING IN AN OUT-OF-TRIM CONDITION. In the event towing lines (rope) are necessary, they should be attached to both main gear struts as high up on the tubes as possible. Lines should be long enough to clear the nose and/or tail by not less than15 feet, and a qualified person must ride in the pilot's seat to maintain control by use of the brakes. TAXIING Before attempting to taxi the airplane, ground personnel must be checked out by a qualified pilot or other responsible person. Each starting and shutdown procedures should be covered as well. When it is ascertained that the propeller back blast and taxi areas are clear, apply power to start the taxi roll and perform the follow- ing checks: 1. Taxi forward a few feet and apply brakes to determine their effectiveness. 2. Taxi with propellers set in low pitch, high rpm setting. 3. While taxiing, make slight turns to ascertain the effectiveness of steering. 4. Observe wing clearances when taxiing near buildings or other stationary objects. If possible, station a guide outside the airplane to observe. 5. When taxiing on uneven ground, look for and avoid holes and ruts. 6. Do not operate the engines at high rpm when running up or taxiing over ground containing loose stones, gravel, or any loose material that may cause damage to the propeller blades. — NOTE — Refer to Figure 9-1 for aircraft turning distance. PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 9-10-00 Page 1 Reissued: November 29, 1993 1D7 Figure 9-1 Airplane Turning Radius (Distance) PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 9-20-00 Page 1 Reissued: November 29, 1993 1D8 60.4 FT.(18.4m) C105 GRIDS 1D9 THRU 1D11 INTENTIONALLY LEFT BLANK PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 1D9 CHAPTER 10 PARKING AND MOORING 1D12 CHAPTER 10 - PARKING AND MOORING TABLE OF CONTENTS/EFFECTIVITY CHAPTER SECTION SUBJECT GRID NO. EFFECTIVITY SUBJECT 10-10-00 PARKING 1D14 10-20-00 MOORING 1D14 PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 10 - Cont./Effec. Page 1 Reissued: November 29, 1993 1D13 PARKING When parking the airplane, ensure that it is sufficiently protected against adverse weather conditions and presents no danger to other aircraft. When parking the airplane for any length of time or overnight, it is recommended that it be moored. 1. To park the airplane, head it into the wind, if possible. 2. Set the parking brake by pulling back the brake lever and depressing the knob attached to the left side of the handle; then release the handle. To release the parking brake, pull back on the brake lever to disen- gage the catch mechanism, and allow the handle to swing forward. — NOTE — Care should be taken when setting brakes that are overheated. During cold weather, accumulated moisture may freeze the discs and lining together if the aircraft is parked with the brakes set. MOORING The airplane is moored to ensure its immovability, protection, and security under various weather condi- tions. The following procedure gives the instructions for proper mooring of the airplane. 1. Head the airplane into the wind, if possible. 2. Block all wheels. 3. Lock the aileron and elevator controls using the seat belt or control surface blocks. 4. Secure the-down ropes to the wing tie-down rings and the tail skid at approximately 45 degree angle to the ground. — NOTE — Use square or bowline knots. Do not use slip knots. Additional preparations for high winds include using tie-down ropes from the landing gear legs, and securing the rudder. PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 10-10-00 Page 1 Reissued: November 29, 1993 1D14 GRIDS 1D15 THRU 1D17 INTENTIONALLY LEFT BLANK PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 1D15 CHAPTER 11 REQUIRED PLACARDS 1D18 CHAPTER 11 - REQUIRED PLACARDS TABLE OF CONTENTS/EFFECTIVITY CHAPTER SECTION SUBJECT GRID NO. EFFECTIVITY SUBJECT 11-20-00 PLACARDS AND MARKINGS 1D20 11-20-00 EXTERIOR PLACARDS 1D20 11-30-00 INTERIOR PLACARDS 1D21 11-30-10 MEYERCORD DECALS 1D24 11-30-10 General 1D24 11-30-10 Removal of meyercord decals 1D24 11-30-10 Installation of Meyercord decals 1D24 PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 11 - Cont./Effec. Page 1 Reissued: November 29, 1993 1D19 PLACARDS AND MARKINGS EXTERIOR PLACRDS Figure 11-1. Exterior Placards and Decals PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 11-20-00 Page 1 Reissued: November 29, 1993 1D20 1 1 3 2 4 4 5 6-7 6-7 5 14 15 11 12-13 16 10 9 3 8 1. SILKSCREEN - Do Not Push 2. PLACARD - ELT Warning 3. SILKSCREEN - Static Vent 4. SILKSCREEN - No Step 5. DECAL - Avgas 6. PLACARD - Oil Specifications 7. PLACARD - Winterization Information 8. SILKSCREEN - Piper~Aire (Optional) 9. DECAL - Seneca III Logo 10. PLATE - Airplane Nameplate 11. PLACARD - Oleo Service Instructions, Main Gear 12. PLACARD - Oleo Service Instructions, Nose Gear 13. PLACARD - Tow Limitations 14. SILKSCREEN - Alignment Alert Bar 15. PLACARD - 14 or 28 Volt External Power 16. SIKLSCREEN - Level Points 17. SILKSCREEN - Door Release 17 INTERIOR PLACARDS Figure 11-2. Interior Placards and Decals (Sheert 1 of 4) PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 11-30-00 Page 1 Reissued: November 29, 1993 1D21 1 2-3 4 5 6-7-8 24 9-10 11 12 13 14 14 18-19 15-16 17 29 27-28 30 26 31 25 23 20-21-22 1. PLACARD - Stabilator Balance Weight 16. PLACARD - Fuel Level Line, Reservoir 2. PLACARD - Baggage Limitations 17. PLACARD - Hydraulic Fluid Specification 3. PLACARD - Cabin Bulkhead 18. PLACARD - Propeller Synchrophaser 4. PLACARD - Aft Cabin Door Release 19. PLACARD - Takeoff and Landing Operation 5. PLACARD - Table Stowage 20. PLACARD - Door, Open 6. PLACARD - Fuel Selector (46.5 Gallons Per Side) 21. PLACARD - Door, Latch PLACARD - Fuel Selector (61.5 Gallons Per Side) 22. PLACARD - Forward Cabin Door Release 7. PLACARD - Heater Control 23. PLACARD - Sump Drain 8. PLACARD - Heater, Flight and Ground Operation 24. PLACARD - Oxygen Bottle Installation 9. PLACARD - Cabin Air, Pull Off 25. PLACARD - External Power 10. PLACARD - Vent Fan (3 Position) 26. PLACARD - Baggage Limitations 11. PLACARD - Flap Lever 27. PLACARD - Light Switch, Baggage Door 12. PLACARD - Pitot Drain 28. PLACARD - Unlatch 13. PLACARD - Control Wheel (Transponder Ident) 29. PLACARD - Storm Window 14. PLACARD - Oil Drain Probe Location 30. PLACARD - Oil Drain Probe 15. PLACARD - Brake Reservoir 31. PLACARD - Press Ball To Unlatch Figure 11-2. Interior Placards and Decals (Sheert 2 of 4) PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 11-30-00 Page 2 Reissued: November 29, 1993 1D22 1 2 3 4 5 9 10 11 12 13 14 15 16 17 18 19 20 8 7 6 FWD 21 25 AFT 24 23 22 SENECA III INSTRUMENT PANEL. SEE SHEET 4 OF 4 FOR SENECA IV PANEL. Figure 11-2. Interior Placards and Decals (Sheert 3 of 4) PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 11-30-00 Page 3 Reissued: November 29, 1993 1D23 1. PLACARD - Compass Erratic 14. PLACARD - Primer L & R 2. PLACARD - Radio Master 15. PLACARD - Optional Fuel Primer System 3. PLACARD - Alternate Static Source 16. PLACARD - Phone/Mike 4. PLACARD - Surface/Propeller Deice 17. PLACARD - Park Brake Pull 5. PLACARD - Phone/Mike 18. PLACARD - Registration Number 6. PLACARD - Air Conditioner 19. PLACARD - Airspeed Limits 7. PLACARD - Optional Electric Flap Position 20. PLACARD - Annunciator Press-To-Test 8. PLACARD - Right and Left Alternator 21. PLACARD - Heater/Fan Operation 9. PLACARD - Alternate Air 22. PLACARD - Elevator Trim 10. PLACARD - Propeller Synchrophaser 23. PLACARD - Rudder Trim 11. PLACARD - Throttle, Propeller, Mixture Control 24. PLACARD - Fuel Controls 12. PLACARD - Emergency Gear Extender 25. PLACARD - Cowl Flaps 13. PLACARD - Lights Dimmer THIS SPACE INTENTIONALLY LEFT BLANK Figure 11-2. Interior Placards and Decals (Sheert 4 of 4) PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 11-30-00 Page 4 Reissued: November 29, 1993 1D24 L START R 1 2 3 4 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 5 22 23 24 25 26 27 28 29 30 31 SENECA IV INSTRUMENT PANEL (SERIAL NUMBERS 3448038 AND UP) 30 29 1. PLACARD – Speed Limitations 2. PLACARD – Airplane Registration 3. PLACARD – Day - Night 4. PLACARD – Press To Test 5. PLACARD – Avoid Continuous Ground operation ............. 6. PLACARD – Ammeter 7. PLACARD – L Alt. Amps - R.Alt Amps 8. PLACARD – KLN-90 Dataloader 9. PLACARD – Circuit Breaker 10. PLACARD – Circuit Breaker 11. PLACARD – Circuit Breaker 12. PLACARD – Circuit Breaker 13. PLACARD – Circuit Breaker 14. PLACARD – Circuit Breaker 15. PLACARD – Circuit Breaker 16. PLACARD – Circuit Breaker 17. PLACARD – Warning - Air Conditioner Must Be Off........... 18. PLACARD – Flap Travel 19. PLACARD – Alternate Static Source. 20. PLACARD – Windshield Panel Heat 21. PLACARD – Warning - This Aircraft is not 22. PLACARD – Gear Up-Down Maximum Speeds 23. PLACARD – Emergency Gear Extension 24. PLACARD – GPS Limited To VFR Use Only 25. PLACARD – Oxygen - Pull ON 26. PLACARD – Dimming – Switch - Panel - Avionics 27. PLACARD – GPS 28. PLACARD – Park Brake Pull 29. PLACARD – Phone 30. PLACARD – Mike 31. PLACARD – L Primer R MEYERCORD DECALS GENERAL Decals installed on the instrument panel of the Seneca IV are Meyercord type manufacturered by Mark-It, 1055 Paramount Tarkway, Batavia. IL 60510. The following procedures should be followed in the event one or more of these decals must be replaced. REMOVAL OF MEYERCORD DECALS CAUTION Do not use lacquer thinner on any panel that has been painted with enamel or lacquer. Seneca IV panels are painted at the factory with polyurethane paints. 1. Remove placard to be replaced with of clean cloth dampened with lacquer thinner. CAUTION Mark-it J-70 solvent will remove enamel, lacquer, and polyutherane based paint products if liquid is dropped onto painted and not removed immediately. a. If panel is painted with enamel or lacquer use a clean cloth dampened with Mark-It J-70 solvent to remove placard to be replaced. INSTALLATION OF MEYERCORD DECALS 1. Brush or wipe a fluid coat of Mark-It C-175 solution on surface to receive decal. 2. Mix a solution consisting of 2 parts water and 1 part J-70 solvent. 3. Submerge decal in the mixed J-70 solution for approximately 3 to 5 seconds. 4. Remove decal from mixed solution and lay in position 5. Using a rubber squeegee, squeegee0.00 from center to edges to remove excess solution. 6. Wait approximately 1 to 1 1/2 minutes, then remove backing paper. 7. Using a damp sponge, remove excess solution from face of decal and surrounding area. PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 11-30-10 Page 1 Reissued: November 29, 1993 1E1 GRID 1E2 INTENTIONALLY LEFT BLANK PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 11-30-10 Page 2 Reissued: November 29, 1993 1E2 CHAPTER 12SERVICING 1E3 CHAPTER 12 - SERVICING TABLE OF CONTENTS/EFFECTIVITY CHAPTER SECTION SUBJECT GRID NO. EFFECTIVITY 12-00-00 GENERAL 1E6 12-00-00 Aircraft Finish Care 1E6 12-00-00 Cleaning 1E6 12-00-00 Cleaning Exterior Surfaces 1E6 12-00-00 Cleaning Windshield and Windows 1E6 12-00-00 Cleaning Interior 1E7 12-00-00 Cleaning Carpets 1E8 12-00-00 Engine Washing 1E8 12-00-00 Cleaning Surface Deicing Equipment 1E8 12-00-00 Cleaning Landing Gear 1E9 12-10-00 REPLENISHING 1E10 12-10-00 Servicing Fuel System 1E10 12-10-00 Draining Fuel System 1E10 12-10-00 Filling Fuel Tanks 1E10 12-10-00 Handling of Dirt and Moisture in Fuel System 1E10 12-10-00 Servicing Oil System 1E13 12-10-00 Draining Oil Sump 1E13 12-10-00 Recommendations for Changing Oil 1E13 12-10-00 Filling Oil Sump 1E13 12-10-00 Oil Screen (Suction) 1E14 12-10-00 Oil Filter (Full Flow) 1E14 12-20-00 SCHEDULED SERVICING 1E15 12-20-00 Servicing Oleo Struts 1E15 12-20-00 Filling Nose Gear Oleo Strut 1E15 12-20-00 Filling Main Gear Oleo Strut 1E16 12-20-00 Inflating Oleo Strut 1E18 12-20-00 Servicing Steering Bungees 1E18 12-20-00 Brake System 1E18 12-20-00 Filling Brake Cylinder Reservoir 1E19 12-20-00 Draining Brake System 1E19 12-20-00 Tires 1E19 12-20-00 Tire Balancing 1E19 PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 12 - Cont./Effec. Page 1 Reissued: November 29, 1993 1E4 CHAPTER 12 - SERVICING TABLE OF CONTENTS/EFFECTIVITY CHAPTER SECTION SUBJECT GRID NO. EFFECTIVITY 12-20-00 SCHEDULED SERVICING (cont) — 12-20-00 Hydraulic System 1E20 12-20-00 Hydraulic Pump Reservoir 1E20 12-20-00 Battery 1E20 12-20-00 Induction Air Filter 1E20 12-20-00 Removal of Air Filter 1E20 12-20-00 Service Instructions (Inspection & Replacement) 1E21 12-20-00 Installation of Air Filter 1E21 12-20-00 Fuel System 1E21 12-20-00 Lubrication Instructions 1E21 12-20-00 Application of Oil 1E22 12-20-00 Application of Grease 1E22 12-20-00 Lubrication Charts 1E22 PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 12 - Cont./Effec. Page 2 Reissued: November 29, 1993 1E5 GENERAL This chapter covers all routine servicing of airplane, scheduled and non-scheduled, including replenish- ment of fuel, oil, hydraulic fluid, oxygen, tire pressure, lubrication requirements, servicing of oleo struts with air and oil, etc. Pay special attention to all WARNINGS or CAUTIONS. AIRCRAFT FINISH CARE CLEANING — WARNING — DO NOT USE GASOLINE, KEROSENE, ALCOHOL, BEN- ZENE, CARBON TETRACHLORIDE, THINNER, ACETONE, OR WINDOW CLEANING SPRAYS TO CLEAN AIRPLANE. CLEANING EXTERIOR SURFACES The airplane should be washed with a mild soap and water solution. Harsh abrasives or alkaline soaps or detergents could scratch painted or plastic surfaces or corrode metal. Cover areas where a cleaning solution could cause damage. To wash the airplane use the following procedure: 1. Flush away loose dirt with water. 2. Apply cleaning solution with a soft cloth, a sponge or a soft brush. 3. To remove exhaust stains, allow the solution to remain on the surface longer. 4. To remove stubborn oil and grease stains, use a soft cloth dampened with naphtha. 5. Rinse all surfaces thoroughly. 6. Any good automotive wax may be used to protect and preserve painted surfaces. Soft cleaning cloths or a chamois should be used to prevent scratches when cleaning or polishing. A heavier coat of wax on leading surfaces will reduce the abrasion problems in these areas. Refer to surface de-ice cleaning procedures. CLEANING WINDSHIELD AND WINDOWS — CAUTION — USE ONLY WATER AND MILD SOAP WHEN CLEANING THE HEATED WINDSHIELD. USE OF ANY OTHER CLEANING AGENT OR MATERIAL MAY CAUSE DISTORTION OR DAMAGE TO WINDSHIELD COATINGS. 1. Remove dirt, mud and other loose particles from exterior surfaces with clean water. 2. Wash interior and exterior window surfaces with mild soap and warm water. Use a soft cloth or sponge in a straight back and forth motion. Do not rub harshly. 3. Remove oil and grease with a cloth dampened with Plexiglas Polish and Cleaner, P/N 403D or similar substance conforming to Federal Specification (P-P-560) or kerosene. 4. Rinse windows thoroughly and dry with soft lint-free cloth. PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 12-00-00 Page 1 Reissued: November 29, 1993 1E6 — WARNING — DO NOT USE GASOLINE, ALCOHOL, BENZENE, CARBON TETRACHLORIDE, THINNER, ACETONE, STRONG SOL- VENTS OR WINDOW CLEANING SPRAYS. DO NOT USE PLASTIC CLEANER ON HEATED GLASS WINDSHIELDS. 5. A superficial scratch or mar in plastic can be removed by polishing out the scratch with jeweler's rouge. 6. When windows are clean, apply a thin coat of polishing wax. Rub lightly with a soft cloth. Do not apply wax to heated windshields with electrical heating elements. 7. Apply REPCON repellent or equivalent to windows and windshield to improve visibility during flights through rain. Apply only according to manufacturer’s instructions. (Refer to Chapter 91, Consumable Materials.) CLEANING INTERIOR 1. Vinyl interior surfaces may be cleaned with a damp cloth and mild soap and water solution. 2. Leather may be cleaned with a mild hand soap and water solution or with a saddle soap. Follow the pre- cautions which apply to the cleaning of any fine leather product. Avoid saturation and never use deter- gents or harsh cleaning solutions on leather. — CAUTION — USE OF COMMON HOUSEHOLD CLEANERS AND POLISHES ON WOOD LAMINATED SURFACES COULD BE VERY HARMFUL. 4. Wood laminated surfaces should be maintained using only a high grade furniture wax. 5. All upholstery fabrics are Scotchguard treated and may be cleaned as follows: Spilled oily and watery liquids will generally bead up on the fabric and can be blotted away leaving little or no stain. Blot spills up as quickly as possible with an absorbent cloth, tissue or sponge. If the material is a solid or semi-solid, such as butter, remove the excess by gently scraping with a table knife. Often, blotting will remove all traces of stain but if the staining agent is not completely removed by blotting, the following techniques are suggested: Water-based stains such s ketchup, milk, ice cream, coffee: Wipe the stain with a cloth wet with water containing a detergent or ammonia (4 fluid ounces of ammonia to one gallon of water). repeat if necessary. Oil based stains such as salad dressing, butter or mayonnaise may be removed by either of the following procedures: Apply “Texize K-2R Spot Remover” by spraying or rubbing into the fabric and let dry. Vacuum off the residual powder. Repeat if necessary or wet a cloth with a solvent type spot cleaner such as “Energine” or “Renuzit” and wipe or gently rub the stained area. Turn cloth and rewet with solvent often. Repeat until stain disappears. To remove residual detergent left on the fabric, wipe the entire fabric surface with a cloth dampened with water. The cloth should be rinsed in clean water several times. This procedure will ensure that the treatment will continue to function. — NOTE — It is best to test the cleaner on an inconspicuous portion of the fabric to test for discoloration. Also avoid soaking or harsh rubbing. PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 12-00-00 Page 2 Reissued: November 29, 1993 1E7 CLEANING CARPETS — WARNING — SOLVENT CLEANERS REQUIRE ADEQUATE VENTILA- TION. Use a small whisk broom or vacuum cleaner to remove dirt. For soiled spots, use a nonflammable dry cleaning fluid. Floor carpets may be removed and cleaned like any household carpet. ENGINE WASHING Before cleaning the engine compartment, place strips of tape on the magneto vents to prevent any solvent from entering these units. 1. Place a pan under the engine to catch waste. — CAUTION — DO NOT SPRAY SOLVENT INTO THE ALTERNATOR, STARTER, VACUUM PUMP, AIR INTAKE AND ALTER- NATE AIR INLETS. 2. With the engine cowling removed, spray or brush the engine with solvent or a mixture of solvent and degreaser, as desired. It may be necessary to brush areas that were sprayed where heavy grease and dirt deposits have collected in order to clean them. 3. Allow the solvent to remain on the engine from five to ten minutes; then rinse the engine clean with additional solvent and allow to dry. — CAUTION — DO NOT OPERATE ENGINE UNTIL EXCESS SOLVENT HAS EVAPORATED OR OTHERWISE BEEN REMOVED. 4. Remove the protective covers from the magnetos. 5. Lubricate controls, bearing surfaces, etc., per Lubrication Charts. (Refer to Chapter 12.) CLEANING SURFACE DEICING EQUIPMENT The deice boots should be cleaned when the aircraft is washed using a mild soap and water solution. In cold weather, wash the boots with the airplane inside a warm hangar if possible. If the cleaning is to be done outdoors, heat the soap and water solution before taking it out to the airplane. If difficulty is encountered with the water freezing on boots, direct a flow of warm air along the region being cleaned, using a portable type ground heater. As an alternate cleaning solvent, use benzol or non-leaded gasoline. Moisten the cleaning cloth in the sol- vent, scrub lightly and then with a clean dry cloth, wipe dry so that the cleaner does not have time to soak into the rubber. PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 12-00-00 Page 3 Reissued: November 29, 1993 1E8 — CAUTION — PETROLEUM PRODUCTS SUCH AS THESE ARE INJURI- OUS TO RUBBER AND THEREFORE SHOULD BE USED SPARINGLY IF AT ALL. When deice boots are clean, a coating of B.F. Goodrich Icex should be applied. Icex is compounded to lower the strength of adhesion between ice and rubber surface of the deice boots. CLEANING LANDING GEAR Before cleaning landing gear, place plastic cover or similar material over wheel and brake assembly. 1. Place can under gear to catch waste. 2. Spray or brush gear area, as required, with solvent or mixture of solvent and degreaser. 3. Allow solvent to remain on gear for 5 to 10 minutes. Rinse gear with additional solvent and allow to dry. 4. Remove cover from wheel and remove catch can. 5. Lubricate gear per lubrication chart in Chapter 12. THIS SPACE INTENTIONALY LEFT BLANK PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 12-00-00 Page 4 Reissued: November 29, 1993 1E9 REPLENISHING SERVICING FUEL SYSTEM The fuel filter, mounted to the wing station 82.92 rib, should be cleaned at intervals of 50 hours or every 90 days, whichever comes first. Servicing of the filter is as follows: 1. Move the system's fuel selector valve to its off position. 2. Just outboard of the nacelle (refer to Figures 12-1 and 12-2), and under the wing, remove the access panel forward of the main spar at wing station 91.0. 3. With the drain cup, drain any fuel still in the bowl from the drain valve under the wing. 4. Disconnect the filter drain line from the bowl and cap the line. 5. Cut the safety wire and remove cap nut from bottom of bowl. 6. Remove bowl and O-ring seal from body. 7. Remove the check and retaining nuts from the stud, and slide the filter down off the stud. 8. The filter discs and washers need not be separated for normal cleaning. If necessary, proceed as follows: a. Remove retainer cup from outer tube. b. Slide discs and washers from outer tube. DO NOT use a sharp tool (screwdriver, etc.) to separate them. DRAINING FUEL SYSTEM The bulk of the fuel may be drained from the system by removing the flush type drain valve at the inboard end of each fuel tank. The remaining fuel in the system may be drained through the fuel filters and the two drains located on the lower right side of the fuselage inboard to the flaps. FILLING FUEL TANKS Each fuel system is filled through a single filler neck in its outboard tank. The standard fuel system involves two 24.5 gallon tanks per side comprising a total of 49 gallons per side. With the optional system, an additional bladder cell of 15 gallons is added per side giving a total of 64 gallons per side. Anti-icing additives complying with MIL-1-27686, may be added when filling the system. Refer to the next paragraph for the proper method. HANDLING OF DIRT AND MOISTURE IN FUEL SYSTEM — CAUTION — WHEN USING ADDITIVES, MAKE SURE THE CORRECT PROCEDURES ARE FOLLOWED. WHEN REFUELING, OBSERVE ALL SAFETY PRECAUTIONS AND USE FUEL SPECIFIED ON FILLER PLACARD. — CAUTION — MAKE SURE THAT ANTI-ICING ADDITIVE IS DIRECTED INTO THE FLOWING FUEL STREAM, STARTING AFTER, AND STOPPING BEFORE THE FUEL FLOW. DO NOT PERMIT ADDITIVE TO COME IN DIRECT CONTA C T WITH PAINTED SURFACES OR INTERIOR SURFACES OF TANKS. PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 12-10-00 Page 1 Reissued: November 29, 1993 1E10 Figure 12-1. Service Points PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL 12-10-00 Page 2 Reissued: November 29, 1993 1E11 1 8 5 2 4 12 9 4 7 5 12 1 10 14 11 8 6 9 2 3 3 1716 13 15 14 19 20 18 13 1. FUEL FILLERS 11. MAIN GEAR TIRES 2. FUEL INJECTORS 12. INDUCTION AIR FILTERS 3. ENGINE OIL FILL 13. ENGINE OIL SUCTION SCREEN 4. ENGINE OIL FILTERS 14. PROPELLER AIR CHARGE 5. FUEL FILTERS 15. BRAKE RESERVOIR 6. INSTRUMENT AIR FILTERS 16. NOSE GEAR STRUT 7. FUEL SYSTEM DRAINS 17. NOSE GEAR TIRE 8. FUEL METERING CONTROL UNIT 18. EXTERNAL POWER RECEPTACLE 9. OIL DIPSTICK 19. BATTERY 10. MAIN GEAR STRUT 20. HYDRAULIC RESERVOIR Figure 12-