Piper seneca PA34-200 753-817 service maintenance manual

PART NUMBER 753-817 October 30, 2003 1A1 AIRPLANE SERVICE MANUAL CARD 1 OF 4 PA-34-200 (S/N’s 34-7250001 THRU 34-7450220) PIPER AIRCRAFT CORPORATION

1A2 Published by Technical Publications © The New Piper Aircraft, Inc. 2926 Piper Drive Vero Beach, Florida 32960 U.S.A. Member General Aviation Manufacturers Association

PIPER SENECA SERVICE MANUAL PAGE 1 Oct 30/03 1A3 AEROFICHE EFFECTIVITY AEROFICHE REVISION STATUS Revisions to this Service Manual 753-817 originally issued April 5, 1971 are as follows: Revision Publication Date Aerofiche Card Effectivity ORG710405 April 5, 1971 N/A CR720613 June 13, 1972 N/A CR031030 * October 30, 2003 1, 2, 3, & 4 * COMPLETE REISSUE OF SERVICE MANUAL 753-817 This is a complete reissue of this publication. Accordingly, replace your existing Aerofiche Card Set (i.e. - Cards 1 and 2) with this set (i.e. - Cards 1, 2, 3, and 4) dated 10/30/03. Consult the Customer Service Information Aerofiche (P/N 1753-755) for current revision dates for this manual.

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PIPER SENECA SERVICE MANUAL PAGE 1 Oct 30/03 1A5 INTRO - LIST OF EFFECTIVE PAGES INTRODUCTION LIST OF EFFECTIVE PAGES SECTION PAGE DATE Intro-List of 1 Oct 30/03 Effective Pages 2 Oct 30/03 Intro-Table of Contents 1 Oct 30/03 2 Oct 30/03 Introduction 1 Oct 30/03 2 Oct 30/03 3 Oct 30/03 4 Oct 30/03 5 Oct 30/03 6 Oct 30/03 7 Oct 30/03 8 Oct 30/03 9 Oct 30/03 10 Oct 30/03 Index 1 Oct 30/03 2 Oct 30/03 3 Oct 30/03 4 Oct 30/03 5 Oct 30/03 6 Oct 30/03 SECTION PAGE DATE

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PIPER SENECA SERVICE MANUAL INTRO - CONTENTS PAGE 1 Oct 30/03 1A7 TABLE OF CONTENTS SUBJECT SECTION PAGE GRID NO. Introduction Instructions for Continued Airworthiness 1 1A9 General 1 1A9 Effectivity 1 1A9 Serial Number Explanation 2 1A10 Assignment of Subject Material 2 1A10 Pagination 2 1A10 Aerofiche Effectivity 2 1A10 Identifying Revised Material 2 1A10 Indexing 2 1A10 List of Effective Pages 3 1A11 Warnings, Cautions, and Notes 3 1A11 Accident / Incident Reporting 3 1A11 Supplementary Publications 3 1A11 PIPER Publications 3 1A11 Vendor Publications 3 1A11 Section Index Guide 9 1A17 Index Index 1 1B1

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PIPER SENECA SERVICE MANUAL PAGE 1 Oct 30/03 1A9 INTRODUCTION INTRODUCTION 1. INSTRUCTIONS FOR CONTINUED AIRWORTHINESS. WARNING : INSTRUCTIONS FOR CONTINUED AIRWORTHINESS (ICA) FOR ALL NON-PIPER APPROVED STC INSTALLATIONS ARE NOT INCLUDED IN THIS MANUAL. WHEN A NON-PIPER APPROVED STC INSTALLATION IS INCORPORATED ON THE AIRPLANE, THOSE PORTIONS OF THE AIRPLANE AFFECTED BY THE INSTALLATION MUST BE INSPECTED IN ACCORDANCE WITH THE ICA PUBLISHED BY THE OWNER OF THE STC. SINCE NON-PIPER APPROVED STC INSTALLATIONS MAY CHANGE SYSTEMS INTERFACE, OPERATING CHARACTERISTICS AND COMPONENT LOADS OR STRESSES ON ADJACENT STRUCTURES, THE PIPER PROVIDED ICA MAY NOT BE VALID FOR AIRPLANES SO MODIFIED. The PIPER PA-34-200 Seneca Service Manual constitutes the Instructions for Continued Airworthiness. Section I contains the Airworthiness Limitations and the Inspection Program is in Section III. 2. GENERAL. WARNING : USE ONLY GENUINE PIPER AIRCRAFT PARTS OR PIPER AIRCRAFT APPROVED PARTS OBTAINED FROM PIPER APPROVED SOURCES, IN CONNECTION WITH THE MAINTENANCE AND REPAIR OF PIPER AIRPLANES. Genuine PIPER parts are produced and inspected under rigorous procedures to insure airworthiness and suitability for use in PIPER airplane applications. Parts purchased from sources other than PIPER, even though identical in appearance, may not have had the required tests and inspections performed, may be different in fabrication techniques and materials, and may be dangerous when installed in an airplane. Additionally, reworked or salvaged parts or those parts obtained from non-PIPER approved sources, may have service histories which are unknown or cannot be authenticated, may have been subjected to unacceptable stresses or temperatures or may have other hidden damage not discernible through routine visual or nondestructive testing. This may render the part, component or structural assembly, even though originally manufactured by PIPER, unsuitable and unsafe for airplane use. THE NEW PIPER AIRCRAFT, INC. expressly disclaims any responsibility for malfunctions, failures, damage or injury caused by use of non-PIPER approved parts. NOTE : THE NEW PIPER AIRCRAFT, INC. expressly reserves the right to supersede, cancel and/or declare obsolete any part, part numbers, kits or publication that may be referenced in this manual without prior notice. In any question concerning the care of your airplane, be sure to include the airplane serial number in any correspondence. 3. EFFECTIVITY. This maintenance manual is effective for PA-34-200 Seneca airplane serial numbers 34-7250001 thru 34-7450220. This encompasses the following model years: NOTE : The following is provided as a general reference only. Model Year Serial Numbers 1972 34-7250001 thru 34-7250360 1973 34-7350001 thru 34-7350353 1974 34-7450001 thru 34-7450220

PIPER SENECA SERVICE MANUAL PAGE 2 Oct 30/03 1A10 INTRODUCTION 4. SERIAL NUMBER EXPLANATION. Example: 5. ASSIGNMENT OF SUBJECT MATERIAL. This publication is divided into logical subject groupings based on aircraft system or task function. Refer to paragraph 14, Section Index Guide, for a complete breakdown and list. The material is arranged in ascending numerical sequence. 6. PAGINATION. The Section (i.e. - I, II, III, etc.) numbering system forms the primary page numbering system for this manual. Within each Section, pages are numbered consecutively beginning with Page 1 (i.e. - Section III, Page 1). Additionally, the aerofiche grid numbering system (explained below) is also used to indicate location within the 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 Service 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 at the beginning of each aerofiche card: (1) A complete Introduction containing the Section Index Guide for all fiche in this set. (2) A complete subject Index for all fiche in this set. 8. IDENTIFYING REVISED MATERIAL. A revision to a page is defined as any change to the printed matter that existed previously. Revisions, additions and deletions are identified by a vertical line along the left-hand margin of the page opposite only that portion of the printed matter that was changed. A vertical line in the left-hand margin opposite the footer (i.e. - chapter/section/subject, page number and date), indicates that the text was unchanged but the material was relocated to a different page. Example. 9. INDEXING. An alphabetically arranged subject Index follows this introduction to assist the user in locating desired information. In addition, each System/Chapter begins with an individual Table of Contents. 34 72 50 001 TYPE CERTIFICATE DESIGNATION MODEL CODE 50 = PA-34-200 SENECA SEQUENCE NUMBER MODEL YEAR

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Piper seneca PA34-200 753-817 service maintenance manual

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