Piper Seneca III / IV (PA-34-220T) Airplane Maintenance Manual

AIRPLANE MAINTENANCE MANUAL CARD 1 OF 5 PA-34-220T SENECA III PA-34-220T SENECA IV THIRD EDITION PIPER AIRCRAFT CORPORATION (PART NUMBER 761-751) REVISED: FEBRUARY 5, 1997 1A1

Published by Technical Publications Piper Aircraft Corporation 2926 Piper Drive Vero Beach, Florida 32960 U.S.A. Member of GAMA General Aviation Manufacturers Association 1A2

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 32-40-01. This number could be assigned by the manufacturer to fit the coverage requirements of the publication. Example: CHAPTER/SYSTEM SUB-SYSTEMS LANDING GEAR WHEELS AND BRAKES 32-40-01 INDIVIDUAL UNITS NOSE WHEEL REMOVAL 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-34-220T Parts Catalog P/N 761 750 and FAR 43 for proper utilization. WARNINGS, CAUTIONS, and NOTES are used throughout this manual to 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. PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL Introduction Page 1 Reissued: November 29, 1993 1A3

AEROFICHE EXPLANATION AND REVISION STATUS The Maintenance Manual information incorporated in this set of Aerofiche cards has been arranged in accordance with the general specifications of Aerofiche adopted by the General Aviation Manufacturer's Association, (GAMA). 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. Conversion of Aerofiche alpha/numeric code numbers: First number is the Aerofiche card number. Letter is the horizontal line reference per card. Second number is the vertical line reference per card. Example: 2J16 = Aerofiche card number two of given set, Grid location J16. To aid in locating the various chapters and related service information desired, the following is provided: 1. A complete manual System/Chapter Index Guide is given for all fiche in this set. 2. A complete list of Illustrations is for all fiche in this set following System/Chapter Index. 3. A complete list of Charts is for all fiche in this set following list of illustration. 4. A complete list of paragraph titles and appropriate Grid location numbers is given at the beginning of each Chapter relating to the information within that Chapter. 5. Identification of Revised Material: 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, 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. 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 Indication, ( 1R Month-Year) Second Revision: Revision Indication, (2R Month-Year) All subsequent revisions will follow with consecutive revision numbers such as 3R, 4R, etc., along with the appropriate month-year Added Subject: Revision Identification, (A Month-Year) Deleted Subject: Revision Identification, (D Month-Year) PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL Introduction Page 2 Reissued: November 29, 1993 1A4

PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL Introduction Page 3 Reissued: November 29, 1993 Interim Revision: February 5, 1997 1A5 AEROFICHE EXPLANATION AND REVISION STATUS (CONTINUED) 6. Revisions to Maintenance Manual 761 751 issued December 19, 1980, are as follows: Effectivity Publication Date Aerofiche Card Effectivity ORG801219 December 19, 1980 1, 2 and 3 CR891220 December 20, 1989 1, 2, 3 and 4 CR931129 November 29, 1993 1, 2, 3, 4 and 5 IR970205 * February 5, 1997 1 and 3 * INTERIM REVISION Chapter 5 of Card 1 and Chapter 32 of Card 3 have been revised. There are no other changes included in this maintenance manual. Please discard your current Cards 1 and 3 and replace them with the revised ones. The date on Aerofiche cards can not preceed the date noted for the respective card effectivity. Consult the latest Aerofiche card in the series for current Aerofiche card effectivity.

PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL Introduction Page 4 Reissued: November 29, 1993 1A6 SERIAL NUMBER INFORMATION The serial numbers of the PA-34-220T Seneca III airplanes covered by this Maintenance Manual are as follows: 34-8133001 through 34-8133277 34-8233001 through 34-8233205 34-8333001 through 34-8333129 34-8433001 through 34-8433088 34-8533001 through 34-8533069 34-8633001 through 34-8633031 3433001 and up 3448005 through 3448037 The serial numbers of the PA-34-220T Seneca IV airplanes covered by this Maintenance Manual are as follows: 3448038 and up SERIAL NUMBER EXPLANATION The serial number on the Manufacturer’s Identification Plate is based on either a 3 or 4 set numbering system. In the 4- set system, the first set defines the Type Certificate Designation, the second set is the Model Year, the third set is the Model Code, and the fourth set is the Model Sequence Number (within a model year). The 3-set system omits the model year and begins a new sequence with 3433001. This new sequence continues without renumbering for a new year. EXAMPLE: 34 81 33 001 34 33 001 TYPE CERTIFICATE DESIGNATION TYPE CERTIFICATE DESIGNATION MODEL YEAR MODEL CODE (33 = PA-34-220T) MODEL SEQUENCE NUMBER MODEL SEQUENCE NUMBER MODEL CODE (33 = PA-34-220T)

VENDOR PUBLICATIONS — WARNING — WHEN SERVICING OR INSPECTING VENDOR EQUIPMENT INSTALLED IN PIPER AIRCRAFT, IT IS THE USER’S RESPONSIBILITY TO REFER TO THE APPLICABLE VENDOR PUBLICATION. ENGINE: Overhaul Manual = 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-30553 Teledyne Continental Motors - Aircraft Products Division Mobile, Alabama 36601 PROPELLER: Overhaul Instructions = HARTZELL COMPACT CONSTANT SPEED and FEATHERING PROPELLER- P/N 117 D - Hartzell Propeller Inc. 1 Propeller Place Piqua, Ohio 45356 Service Manual = McCAULEY C500 SERVICES FULL FEATHERING CONSTANT SPEED PROPELLER- P/N 7512 01 - McCauley Accessory Division 335 McCauley Drive P.O. Box 430 Vandalia, Ohio 45377 MAGNETOS: Installation, Operation and Maintenance Instructions = S6LN-25P IGNITION SYSTEM- P/N L-928 Bendix Electrical Components Division Sidney, New York 13838 VOLTAGE CONTROL: Overhaul Manual and Illustrated Parts List: LAMAR INC. POWER EQUIPMENT DIVISION 71 Inidel Aveneu P. O. Box 251 Rancocas, New Jersey 08073 PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL Introduction Page 5 Reissued: November 29, 1993 1A7

VENDOR PUBLICATIONS (CONTINUED) AUTOFLIGHT (continued) Flight Control: Bendix/King System Flight Line KFC 150 Installation Manual P/N 006-0287-00 System Flight Line KFC 200 Maintenance Manual: P/N 006-5134-01 Vendor Address: Bendix/King Radio Corporation 400 N. Rogers Road Olathe, Kansas 66062 WHEELS AND BRAKES: Installation, Maintenance and Overhaul Manual: Cleveland Parker Hannifin Corporation Aircraft Wheel and Brake Division 1160 Center Road Avion, Ohio 44011 KEVLAR: A Guide to Cutting and Machining Kevlar Aramid: KEVLAR Special Products E.I. DuPont De Nemours & Co. Inc. Textile Fibers Department Centre Road Building Wilmington, Delaware 19898 CORROSION INHIBITING COMPOUND: DINOL International 25200 Malvina Box 1065 Warren, Michigan 48090 OXYGEN SYSTEM Components: Scott Aviation 225 Erie Street Lancaster, New York 14086 FIRE EXTINGUISHER (PORTABLE) Polk Fire Extinguisher Service, Inc. P. O. Box 384 Lakeland, Florida 33802 PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL Introduction Page 6 Reissued: November 29, 1993 1A8

PIPER PUBLICATIONS AUTOFLITE: AutoFlight II Service Manual = Piper P/ N 761 481 Pitch Trim Service Manual = Piper P/N 753 771 AutoControl IIIB and Altimatic IIIB Service Manual = Piper P/N 753 502 Altimatic IIIC Service Manual = Piper P/N 761 602 PARTS CATALOG: 761 750 PROGRESSIVE INSPECTION 50 HOUR EVENT: 761 837 PERIODIC REPORT 230 1061 PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL Introduction Page 7 Reissued: November 29, 1993 1A9

SYSTEM/CHAPTER INDEX GUIDE — NOTE — The following chapters are not applicable to this Maintenance Manual: 31, 36, 38, 49, 53, 54, 60, 72, 78, and 83. SYSTEM/ SUB-SYSTEM/ CHAPTER SECTION TITLE GRID NO. 4 AIRWORTHINESS LIMITATIONS 1B5 00 General 5 TIME LIMITS/MAINTENANCE CHECKS 1B11 10 Time Limits 20 Scheduled Maintenance Checks 50 Programmed Inspection 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 Jacking 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 Meyercord Decals PIPER AIRCRAFT PA-34-220T AIRPLANE MAINTENANCE MANUAL Introduction Page 8 Reissued: November 29, 1993 1A10 SYSTEM/CHAPTER INDEX GUIDE SYSTEM/ SUB-SYSTEM/ CHAPTER SECTION TITLE GRID NO.

Piper Seneca III / IV (PA-34-220T) Airplane Maintenance Manual

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