761-888 PIPER SENECA IV V Maintenance Manual PA-34-220T

PART NUMBER 761-888 April 28, 2006 1A1 AIRPLANE MAINTENANCE MANUAL CARD 1 OF 7 PA-34-220T (SN’s 3447001 THRU 3447029) (SN’s 3449001 AND UP) THE NEW PIPER AIRCRAFT, INC.

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

Apr 28/06 AEROFICHE EFFECTIVITY 1A3 THE NEW PIPER AIRCRAFT, INC. PA-34-220T, SENECA IV / V MAINTENANCE MANUAL AER OFICHE REVISION ST A TUS Revisions to Maintenance Manual (P/N 761-888) issued July 12, 1995, are as follows: Re vision Pub lication Date Aerofiche Card Eff ectivity ORG950712 November 7, 1996 1, 2, 3, 4 and 5 PR980415 April 15, 1998 1, 2, 3, 4 and 5 PR981115 November 15, 1998 1, 2, 3, 4 and 5 PR020531 May 31, 2002 1 CR050819 August 19, 2005 1, 2, 3, 4, 5, 6 and 7 PR051107 November 7, 2005 1, 2, 4 and 5 PR060428* April 28, 2006 1, 2, 3, 4, 5, 6 and 7 * PARTIAL REVISION OF MAINTENANCE MANUAL 761-888 Revisions appear in Aerofiche Cards 1, 2, 3, 4, 5, 6, and 7. Accordingly, discard your existing Aerofiche Cards and replace them with the cards dated April 28, 2006. Consult the Customer Service Information Aerofiche (P/N 1753-755) for current revision dates for this manual.

Aug 19/05 AEROFICHE EFFECTIVITY 1A4 THE NEW PIPER AIRCRAFT, INC. PA-34-220T, SENECA IV / V MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK

THE NEW PIPER AIRCRAFT, INC. PA-34-220T, SENECA IV / V MAINTENANCE MANUAL PAGE 1 Apr 28/06 1A5 INTRO - LIST OF EFFECTIVE PAGES INTR ODUCTION LIST OF EFFECTIVE P A GES CHAPTER SECTION P A GE D A TE Intro-List of 1 Apr 28/06 Effective Pages 2 Aug 19/05 Intro-Table of Contents 1 Apr 28/06 2 Aug 19/05 Introduction 1 Aug 19/05 2 Apr 28/06 3 Apr 28/06 4 Apr 28/06 5 Apr 28/06 6 Apr 28/06 7 Apr 28/06 8 Apr 28/06 9 Apr 28/06 10 Nov 7/05 11 Apr 28/06 12 Aug 19/05 13 Aug 19/05 14 Aug 19/05 Index 1 Apr 28/06 2 Apr 28/06 3 Apr 28/06 4 Apr 28/06 5 Apr 28/06 6 Apr 28/06 7 Apr 28/06 8 Aug 19/05 CHAPTER SECTION P A GE D A TE

THE NEW PIPER AIRCRAFT, INC. PA-34-220T, SENECA IV / V MAINTENANCE MANUAL PAGE 2 Aug 19/05 INTRO - LIST OF EFFECTIVE PAGES 1A6 THIS PAGE INTENTIONALLY BLANK

THE NEW PIPER AIRCRAFT, INC. PA-34-220T, SENECA IV / V MAINTENANCE MANUAL PAGE 1 Apr 28/06 1A7 INTRO - CONTENTS T ABLE OF CONTENTS SUBJECT SECTION P A GE GRID NO . Introduction Instructions for Continued Airworthiness 1 1A9 General 1 1A9 Effectivity 2 1A10 Serial Number Explanation 2 1A10 Assignment of Subject Material 2 1A10 Pagination 3 1A11 Aerofiche Effectivity 3 1A11 Identifying Revised Material 3 1A11 Indexing 3 1A11 List of Effective Pages 3 1A11 Warnings, Cautions, and Notes 4 1A12 Accident / Incident Reporting 4 1A12 Supplementary Publications 4 1A12 PIPER Publications 4 1A12 Vendor Publications 4 1A12 Chapter/Section Index Guide 9 1A17 Index Index 1 1B1

THE NEW PIPER AIRCRAFT, INC. PA-34-220T, SENECA IV / V MAINTENANCE MANUAL PAGE 2 Aug 19/05 1A8 INTRO - CONTENTS THIS PAGE INTENTIONALLY BLANK

THE NEW PIPER AIRCRAFT, INC. PA-34-220T, SENECA IV / V MAINTENANCE MANUAL PAGE 1 Aug 19/05 1A9 INTRODUCTION INTR ODUCTION 1. Instr uctions f or Contin ued Airw or thiness W ARNING : 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-34-220T Seneca IV / V Maintenance Manual constitutes the Instructions for Continued Airworthiness (ICA) as required by Federal Aviation Regulations (FAR) Part 23, Appendix G. Chapter 4 contains the Airworthiness Limitations section (4-00-00) and the Inspection Program is in Chapter 5 (5-20-00). 2. Gener al This publication is prepared in accordance with the General Aviation Manufacturers Association (GAMA) Specification No. 2, with respect to the arrangement and content of the System/Chapters within the designated Chapter/Section-numbering system. W ARNING : 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. This manual generally 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 761-887, and FAR 43 for proper use. 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. NO TE : 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. Eff ectivity This maintenance manual is effective for PA-34-220T Seneca IV airplanes, serial numbers 3447001 thru 3447029, and Seneca V airplanes, serial numbers 3449001 and up. This encompasses the following model years: NO TE : The following is provided as a general reference only. Model Ser ial Numbers Model Y ear Seneca IV 3447001 thru 3447012 1995 3447013 thru 3447029 1996 Seneca V 3449001 Prototype 3449002 thru 3449041 1997 3449042 thru 3449096 1998 3449097 thru 3449151 1999 3449152 thru 3449195 2000 3449196 thru 3449231 2001 3449232, 2002 3449237 thru 3449239, and 3449241 thru 3449268 3449269, 3449273, and 2003 3449275 thru 3449300 3449301 thru 3449310 2004 3449311 thru 3449322 2005 3449323 and Up 2006 4. Ser ial Number Explanation Example: 5. Assignment of Subject Mater ial 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 28-40-01 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 28-40-01 concerns itself with the indicating section of the fuel system. THE NEW PIPER AIRCRAFT, INC. PA-34-220T, SENECA IV / V MAINTENANCE MANUAL PAGE 2 Apr 28/06 1A10 INTRODUCTION 34 49 001 TYPE CERTIFICATE DESIGNATION MODEL CODE 47 = SENECA IV 49 = SENECA V SEQUENCE NUMBER

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761-888 PIPER SENECA IV V Maintenance Manual PA-34-220T

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