PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL

Piper PA-32 Saratoga II TC · Pilot's Operating Handbook

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Overview

The PA-32R-301 / 301T Airplane Maintenance Manual is designed for the Piper Saratoga II HP and TC models, specifically for serial numbers 3246001 and up for the HP variant and 3257001 and up for the TC variant. This manual serves as a comprehensive guide for maintenance and continued airworthiness, adhering to Federal Aviation Regulations (FAR) Part 23, Appendix G. It includes detailed instructions for inspections, repairs, and maintenance procedures necessary to ensure the safe operation of these aircraft. The manual emphasizes the importance of using genuine Piper parts and provides guidelines for the inspection of non-Piper approved modifications. It is essential for maintenance personnel and aircraft owners to reference this manual to maintain compliance with airworthiness standards.

This manual is for Piper PA-32R-301 and PA-32R-301T models, effective for specific serial numbers.
Use only genuine Piper parts for maintenance to ensure safety and compliance.
Follow the Instructions for Continued Airworthiness (ICA) for any non-Piper approved modifications.
Chapter 4 outlines mandatory airworthiness limitations and inspection requirements.
Refer to supplementary publications for detailed servicing and parts information.

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Originally published by www.aeroelectric.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type: Pilot's Operating Handbook
Year: 2004
Pages: 1,236
File size: 15 MB
Publisher: www.aeroelectric.com

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In this document

Introduction

The introduction outlines the purpose of the manual, which is to provide instructions for continued airworthiness for the PA-32R-301 and PA-32R-301T models. It emphasizes the need for genuine Piper parts and provides a general overview of the manual's structure.

Effectivity

This section details the specific serial numbers and model years applicable to the PA-32R-301 and PA-32R-301T. It lists the range of serial numbers for each model year, ensuring that users can identify the correct maintenance procedures for their specific aircraft.

Instructions for Continued Airworthiness

This chapter provides critical information regarding the maintenance and inspection of the aircraft. It includes guidelines for non-Piper approved modifications and stresses the importance of adhering to the Instructions for Continued Airworthiness (ICA) published by the STC owner.

Airworthiness Limitations

Chapter 4 contains the Airworthiness Limitations section, which outlines the mandatory inspections and maintenance checks required to maintain the aircraft's airworthiness.

Supplementary Publications

This section lists additional publications that provide further information on servicing, overhaul, and parts for the PA-32R-301 and PA-32R-301T, including parts catalogs and inspection manuals.

Safety notes

Use only genuine Piper aircraft parts or Piper approved parts for maintenance and repair.
Non-Piper approved modifications may affect systems and require separate inspection protocols.

Full document text

Courtesy of Bomar Flying Service www.bomar.biz AIRPLANE MAINTENANCE MANUAL CARD 1 OF 5 PA-32R-301 (S/N’s 3246001 AND UP) PA-32R-301T (S/N’s 3257001 AND UP) THE NEW PIPER AIRCRAFT, INC. PART NUMBER 761-879 February 16, 2004 1A1 TM Saratoga II HP Saratoga II TC 1A2 THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL Published by Technical Publications © The New Piper Aircraft, Inc. 2926 Piper Drive Vero Beach, Florida 32960 U.S.A. Member General Aviation Manufacturers Association Aerofiche Effectivity Page 1 Revised: February 16, 2004 1A3 THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL AEROFICHE REVISION STATUS Revisions to this Maintenance Manual (P/N 761-879) published June 24, 1996 and reissued July 1, 1997 are as follows: Revision Publication Date Aerofiche Card Effectivity ORG950712 June 24, 1996 1, 2, 3, and 4 CR970701 July 1, 1997 1, 2, 3, 4, and 5 PR990715 July 15, 1999 1, 2, 3, 4, and 5 PR011215 December 15, 2001 1 PR020331 March 31, 2002 1 PR040216* February 16, 2004 1, 3, and 5 * PARTIAL REVISION OF MAINTENANCE MANUAL 761-879 Revisions appear in Aerofiche Cards 1, 3, and 5. Accordingly, discard your existing Cards 1, 3, and 5 and replace them with these three cards dated 02/16/04. Consult the Customer Service Information Aerofiche (P/N 1753-755) for current revision dates for this manual. Aerofiche Effectivity Page 2 Revised: July 15, 1999 1A4 THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK Introduction - Cont./Effec. Page 1 Revised: February 16, 2004 1A5 THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL INTRODUCTION TABLE OF CONTENTS / EFFECTIVITY CHAPTER GRID SECTION SUBJECT NO. EFFECTIVITY Introduction 1A7 4R0204 Instructions for Continued Airworthiness 1A7 4R0204 General 1A7 2R1201 Effectivity 1A8 4R0204 Serial Number Explanation 1A9 4R0204 Assignment of Subject Material 1A9 A0799 Pagination 1A9 A0799 Aerofiche Effectivity 1A9 1R0799 Identifying Revised Material 1A10 4R0204 Indexing 1A10 A0799 Accident / Incident Reporting 1A10 4R0204 Warnings, Cautions, and Notes 1A10 1R0799 Supplementary Publications 1A11 A0799 PIPER Publications 1A11 1R0799 Vendor Publications 1A11 4R0204 Chapter/Section Index Guide 1A17 4R0204 List of Illustrations By Subject 1B1 4R0204 List of Charts By Subject 1B7 4R0204 Introduction - Cont./Effec. Page 2 Revised: July 15, 1999 1A6 THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL Introduction Page 1 Revised: February 16, 2004 1A7 INTRODUCTION 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-32R-301/301T Saratoga II HP and TC Maintenance Manual constitutes the Instructions for Continued Airworthiness in accordance with 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). GENERAL 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. — 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. 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-32R Parts Catalog P/N 761-880, and FAR 43 for proper utilization. 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. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL Introduction Page 2 Revised: February 16, 2004 1A8 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. Be sure to supply the correct serial number information in any correspondence or communication concerning your airplane. EFFECTIVITY

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This maintenance manual is effective for PA-32R-301 Saratoga II HP airplanes serial numbers 3246001 and up and PA-32R-301T Saratoga II TC airplanes serial numbers 3257001 and up. This encompasses the following model years: — Note — The following is provided as a general reference only. PA-32R-301 Saratoga II HP: Model Year Serial Numbers 1995 3246001 thru 3246017 1996 3246018 thru 3246059 1997 3246060 thru 3246087 1998 3246088 thru 3246125 1999 3246126 thru 3246153 2000 3246154 thru 3246165 2000.5 3246166 thru 3246181 2001 3246182 thru 3246203 2002 3246204 thru 3246209 2003 3246210 thru 3246217 2004 3246218 and up PA-32R-301T Saratoga II TC: Model Year Serial Numbers Prototype 3257001 1998 3257002 thru 3257075 1999 3257076 thru 3257123 2000 3257124 thru 3257155; less 3257144 2000.5 3257156 thru 3257198; and 3257144 2001 3257199 thru 3257266 2002 3257267 thru 3257296 2003 3257297 thru 3257338 2004 3257339 and up THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL Introduction Page 3 Revised: February 16, 2004 1A9 SERIAL NUMBER EXPLANATION Example: 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 28-40-01 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. 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 “01” of the number 28-40-01 is a subject designator. This element is assigned at the option of the manufacturer and is normally zeroed out by PIPER. Refer to Chapter/Section Index Guide, for a complete breakdown and list. The material is arranged in ascending numerical sequence. PAGINATION The Chapter - Section (i.e. - 28-40-00) numbering system (explained above) forms the primary page numbering system for this manual. Within each Chapter, pages are numbered consecutively beginning with Page 1 (i.e. - Page 28-1). Additionally, the aerofiche grid numbering system (explained below) may also be used to indicate location within the manual. 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. 32 46 001 TYPE CERTIFICATE DESIGNATION MODEL CODE 46 = PA-32R-301 SARATOGA II HP 57 = PA-32R-301T SARATOGA II TC SEQUENCE NUMBER THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL Introduction Page 4 Revised: February 16, 2004 1A10 C. To aid in locating information, the following is provided at the beginning of each aerofiche card: (1) A complete Introduction containing the Chapter/Section Index Guide for all fiche in this set. (2) A complete List of Illustrations for all fiche in this set. (3) A complete List of Charts for all fiche in this set. 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 (i. e. - change bar) along the left- hand margin of the page opposite only that portion of the printed matter that was changed. A change bar in the left-hand margin opposite the footer (i.e. - chapter/section/subject, page number and date), indicates that the text was unchanged but the material was relocated to a different page. Example. — Note — Change bars are not used in the title pages, list of illustrations, or list of charts. 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: Original and Reissue: None Revisions: First: Revision Indication ( 1R Month-Year ) Second: Revision Indication ( 2R Month-Year ) Subsequent revisions follow with consecutive numbers such as 3R, 4R, etc. Added Subject: Revision Identification, (A Month-Year) Deleted Subject: Revision Identification, (D Month-Year) INDEXING Each System/Chapter begins with an individual Table of Contents. 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. WARNINGS, CAUTIONS AND NOTES These adjuncts to the text are used to highlight or emphasize important points when necessary. WARNINGS call attention to use of materials, processes, methods, procedures or limits which must be followed precisely to avoid injury or death to persons. CAUTIONS call attention to methods and procedures which must be followed to avoid damage to equipment. NOTES call attention to methods which make the job easier. Warnings and Cautions shall be located directly above and Notes directly beneath the text and be in line with the paragraphs to which they apply. THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL Introduction Page 5 Revised: February 16, 2004 1A11 SUPPLEMENTARY PUBLICATIONS The following is a list of publications providing servicing, overhaul and parts information on various components on the PA-32R-301/301T airplanes, which you should use to supplement this manual. A. Piper Publications: (1) Parts Catalog - P/N 761-880 (2) Progressive Inspection Manuals (50 hour): P/N 761-881 (pending) for the SARATOGA II HP (S/N’s 3246001 & up), and P/N 761-896 (pending) for the SARATOGA II TC (S/N’s 3257001 & up). (3) Periodic Inspection Report Forms: P/N 230-1047 for the SARATOGA II HP (S/N’s 3246001 & up), and P/N 230-2047 for the SARATOGA II TC (S/N’s 3257001 & up). 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. AIR CONDITIONING COMPRESSOR: Vendor: York Industries (or) Sanden International (USA), Inc. 1750 Toronita Street 601 South Sanden Blvd. York, Pennsylvania 17402 Wylie, TX 75098-4999 (717) 846-1988 (972) 442-8400 http://www.sanden.com ALTERNATOR Vendor: Electro Systems PH - (888) 461-6077 Airport Complex P. O. Box 273 Fort Deposit, Alabama 36032 http://www.kellyaerospace.com/index.htm/ AUTOFLIGHT: Vendor(s): Honeywell (or) S-TEC Corporation One Technology Center One S-TEC Way 23500 W. 105th St., M/D #45 Mineral Wells, Texas 76067-9236 Olathe, Kansas 66061-1950 PH - (940) 325-9406 http://www.bendixking.com/ www.s-tec.com BRAKES: Vendor: Parker Hannifin Corp. PH - (800) 272-5464 Aircraft Wheel and Brake Division 1160 Center Road Avon, Ohio 44011 http://www.parker.com/cleveland/Universe/book.pdf THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL Introduction Page 6 Revised: December 15, 2001 1A12 ELECTRONIC FLIGHT DISPLAY SYSTEM (EFDS) Vendor: Avidyne Corporation PH - (800) 284-3963 55 Old Bedford Road Lincoln, MA 01773 http://www.avidyne.com/index.htm Instructions for Continued Airworthiness Primary Flight Display and Magnetometer/OAT Document No. AVPFD-174 Multifuntion Display Document No. AVMFD-167 Data Acquisition Unit Document No. AVSIU-011 EMERGENCY LOCATOR TRANSMITTER: Vendor: Artex Aircraft Supplies PH - (800) 547-8901 14405 Keil Road NE Aurora, Oregon 97002 http://www.artex.net/ ENGINE: Vendor: Textron Lycoming PH - (717) 323-6181 652 Oliver Street FAX - (717) 327-7101 Williamsport, PA 17701 http://www.lycoming.textron.com/main.html Overhaul Manual: DIRECT DRIVE MODELS - P/N 60294-7 Parts Catalog: IO-540- ..... - K1G5, ..... ENGINES - P/N PC-615 TIO-540-AH1A ENGINES - P/N PC-615-12 Operators Handbook: O-540, IO-540 SERIES - P/N 60297-10 TIO-540 Series - P/N 60297-23 — Note — The above Lycoming publications can be ordered as a set on CD-ROM from Avantext. See www.avantext.com or PH - (800) 998-8857. ELECTRIC FUEL PUMP: Vendor(s): Parker Hannifin Corp. (or) Weldon Pump Airborne Division 640 Golden Oak Parkway 711 Taylor Street Oakwood Village, OH 44146 Elyria, Ohio 44035 PH - (216) 232-2282 PH - (800) 382-8422 http://www.parker.com/cleveland/Universe/book.pdf THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL Introduction Page 7 Revised: February 16, 2004 1A13 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 GEAR LOCKING ACTUATORS, NOSE GEAR DOOR ACTUATOR, HYDRAULIC PUMP, AND ALL HYDRAULIC COMPONENTS: Vendor: Parker Hannifin Corp. (See Brakes, above) HI-LOK FASTENERS AND TOOLS: Vendor: Hi-Shear Corporation PH - (213) 326-8110 2600 Skypark Drive Torrance, California 90509 (213) 326-8110 LIGHTS - NAVIGATION/STROBE LIGHTS STANDBY/MAP: Vendor: Whelen Engineering Co. Inc. PH - (860) 526-9504 Route 145, Winthrop Rd. FAX - (860) 526-2009 Chester, CT 06412 http://www.whelen.com/ MAGNETOS: Vendor: Slick Aircraft Products PH - (815) 965-4700 Unison Industries FAX - (815) 965-2457 Attn: Subscription Dept. 530 Blackhawk Park Ave. Rockford, IL 61104 http://www.unisonindustries.com/index4.html Installation, Operation F1100 MASTER SERVICE MANUAL, and Maintenance 4300/6300 SERIES MAGNETO MAINTENANCE AND Instructions: OVERHAUL MANUAL - L-1363 NAVIGATION, COMMUNICATIONS, AND GPS (NAV/COM/GPS): Vendor: Garmin International PH: - (913) 397-8200 1200 East 151ST Street Olathe, KS 66062 http://www.garmin.com OXYGEN SYSTEM: (TC only) Vendor: Scott Aviation PH - (716) 683-5100 2225 Erie Street Lancaster, New York 14086 http://www.scottaviation.com/ THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL Introduction Page 8 Revised: February 16, 2004 1A14 PROPELLER: Vendor: Hartzell Propellor Inc. PH - (937) 778-4379 One Propellor Place FAX - (937) 778-4321 Piqua, OH 45356-2634 http://www.hartzellprop.com/index2.htm Standard Practices: Manual No. 202A Overhaul and Maintenance: Manual No. 113B Aluminum Blade Overhaul: Manual No. 133C Propeller Owner’s Manual and Logbook: Manual No. 115N PROPELLER GOVERNOR: Vendor: Hartzell Propeller Inc. PH - (937) 778-4379 One Propellor Place FAX - (937) 778-4321 Piqua, OH 45356-2634 http://www.hartzellprop.com/index2.htm Governor Maintenance: Manual No. 130B STANDBY ATTITUDE INDICATOR: Vendor: Mid-Continent Instruments Co., Inc. PH - (316) 630-0101 9400 E. 34 TH Street N. FAX - (316) 630-0723 Wichita, KS 67226 http://www.mcico.com/index.html Installation Manual and Operating Instructions: Manual No. 9015762 STARTER: Vendor: Sky-Tec PH - (800) 476-7896 350 Howard Clemmons Rd. FAX - (817) 573-2252 Granbury, Texas 76048 http://www.skytecair.com VACUUM PUMPS: Vendor: Aero Accessories, Inc. PH - (800) 822-3200 1240 Springwood Avenue Gibsonville, NC 27249 http://www.aeroaccessories.com/index.html VACUUM REGULATORS: Vendor: Parker Hannifin Corporation PH -(800) 382-8422 Airborne Division 711 Taylor St. Elyria, OH 44035 http://www.parker.com/cleveland/Universe/book.pdf THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL Introduction Page 9 Revised: February 16, 2004 1A15 THIS PAGE INTENTIONALLY BLANK THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL Introduction Page 10 Revised: February 16, 2004 1A16 THIS PAGE INTENTIONALLY BLANK THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL Introduction Page 11 Revised: February 16, 2004 1A17 SYSTEM / CHAPTER INDEX GUIDE SYSTEM/ SUB-SYSTEM/ GRID CHAPTER SECTION NO. — Note — The following GAMA Specification No. 2 standard chapters are not included in this Maintenance Manual: 26, 36, 38, 49, 53, 54, 60, 72, 75, 76, 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. 4 AIRWORTHINESS LIMITATIONS 1B11 00 Airworthiness Limitations 5 TIME LIMITS/MAINTENANCE CHECKS 1B17 00 General 10 Time Limits 20 Scheduled Maintenance 30 Special Inspections 50 Unscheduled Maintenance Checks 6 DIMENSIONS AND AREAS 1D21 00 General 7 LIFTING AND SHORING 1E7 10 Jacking 8 LEVELING AND WEIGHING 1E13 10 Weighing and Balancing 20 Leveling 9 TOWING AND TAXIING 1E21 10 Towing 20 Taxiing 10 PARKING AND MOORING 1F5 10 Parking 20 Mooring 11 REQUIRED PLACARDS 1F13 20 Exterior Placards and Markings 30 Interior Placards and Markings 12 SERVICING 1G1 00 General 10 Replenishing 20 Scheduled Servicing 20 STANDARD PRACTICES - AIRFRAME 1H17 00 General THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL Introduction Page 12 Revised: February 16, 2004 1A18 21 ENVIRONMENTAL SYSTEMS 1I7 00 General 40 Heating 50 Cooling 22 AUTO FLIGHT 1L3 10 Autopilot 23 COMMUNICATIONS 1L9 00 General 20 Emergency Locator Transmitter 24 ELECTRICAL POWER 2C1 00 General 30 DC Generation 40 External Power 50 Electrical Load Distribution 25 EQUIPMENT/FURNISHINGS 2E1 10 Flight Compartment 27 FLIGHT CONTROLS 2E13 00 General 10 Aileron and Tab 20 Rudder and Tab 30 Stabilator and Tab 50 Flaps 28 FUEL 2H1 00 General 10 Storage 20 Distribution 40 Indicating 29 HYDRAULIC POWER 2I15 00 General 10 Main 30 ICE AND RAIN PROTECTION 2J13 00 General 30 Pitot and Static SYSTEM / CHAPTER INDEX GUIDE (cont) SYSTEM/ SUB-SYSTEM/ GRID CHAPTER SECTION NO. THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL Introduction Page 13 Revised: February 16, 2004 1A19 31 INDICATING / RECORDING SYSTEMS 2K1 50 Central Warning Systems 32 LANDING GEAR 3C1 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 3G1 00 General 10 Flight Compartment 40 Exterior 34 NAVIGATION AND PITOT/STATIC 3G17 00 General 10 Flight Environment Data / Pitot/Static 20 Attitude and Direction 35 OXYGEN 3H11 00 General 10 Crew / Passenger 37 VACUUM 3I17 00 General 10 Distribution 20 Indicating 39 ELECTRICAL/ELECTRONIC PANELS & MULTIPURPOSE PARTS 3J7 10 Instrument and Control Panels 51 STRUCTURES 3J15 00 General 52 DOORS 3K11 00 General 10 Passenger/Crew 30 Cargo SYSTEM / CHAPTER INDEX GUIDE (cont) SYSTEM/ SUB-SYSTEM/ GRID CHAPTER SECTION NO. THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL Introduction Page 14 Revised: February 16, 2004 1A20 55 STABILIZERS 4C1 10 Stabilator 30 Vertical Stabilizer 40 Rudder 56 WINDOWS 4C15 10 Flight Compartment 20 Cabin 57 WINGS 4D1 00 General 20 Auxiliary Structure 40 Attach Fittings 50 Flight Surfaces 61 PROPELLERS 4E1 10 Propeller Assembly 20 Controlling 70 STANDARD PRACTICES - ENGINE 4E13 00 General 71 POWER PLANT 4E19 00 General 10 Cowling 73 ENGINE FUEL SYSTEMS 4F13 10 Distribution 20 Controlling 74 IGNITION 4G1 00 General 10 Electrical Power Supply 20 Distribution 30 Switching 77 ENGINE INDICATING 4H15 00 General 10 Power 20 Temperature 78 EXHAUST 4J1 00 General SYSTEM / CHAPTER INDEX GUIDE (cont) SYSTEM/ SUB-SYSTEM/ GRID CHAPTER SECTION NO. THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL Introduction Page 15 Revised: February 16, 2004 1A21 79 OIL 4J9 20 Distribution 30 Indicating 80 STARTING 4J17 00 General 10 Cranking 81 TURBINES 4L1 00 General 20 Turbo-Supercharger 91 CHARTS & WIRING DIAGRAMS 5C1 00 General 10 Electrical Schematics 95 SPECIAL PURPOSE EQUIPMENT 5I1 00 Special Purpose Equipment APPENDIXES 1 AUTOFLIGHT 5J1 2 ELECTRONIC FLIGHT DISPLAY SYSTEM 5K3 — Note — For Vendor Publications, see Introduction - Supplementary Publications. SYSTEM / CHAPTER INDEX GUIDE (cont) SYSTEM/ SUB-SYSTEM/ GRID CHAPTER SECTION NO. THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL Introduction Page 16 Revised: February 16, 2004 1A22 GRIDS 1A22 THRU 1A24 INTENTIONALLY BLANK THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL List of Illustrations Page 1 Revised: February 16, 2004 1B1 A Access Plates and Panels: 1E6 Aileron Balance Configuration: 4D18 Bellcrank Rigging: 2F9 Bellcrank Rigging Tool: 5I9 Controls: 2F6 Installation: 4D15 Rigging: 2F11 Rigging Limits: 2F10 Rigging Tool: 5I10 Air Conditioning Components Installation: 1K23 Compressor Belt Installation: 1K10 Condenser Air Scoop Installation: 1K20 Expansion Valve: 1K21 Fabricated Oil Dipstick for Sanden Compressor: 1K6 Leak Test: 1J16 Manifold Set Operation: 1J10 Manifold to Recharging/Test Stand Hookup: 1J11 Optional Charging Hookups: 1K1 Robinair 34700 Control Panel and Hose Connections: 1J12 Robinair 34700 Hose Hookup: 1J13 Sanden Compressor Oil Measurement: 1K7 Sanden Magnetic Clutch: 1K15 Service Valves: 1J8 System Installation: 1J2 Test Manifold and Charging Cart: 1J10 Wiring Schematic: 1L2 York Compressor and Fabricated Oil Dipstick: 1K5 York Magnetic Clutch: 1K17 Alternator Belt Installation: 1K10 Diode Testing: 2D5 Exploded View: 2C12 Field Circuit Open or Ground Test: 2C21 Front Housing Assembly: 2D6 Front Housing Components: 2C24 Front Housing Disassembly: 2C24 Housing Disassembly: 2C22 Housings Assembly: 2D8 Internal Relationships of Components: 2C15 Rear Housing Bearing and Brush Assembly Installation: 2D7 Rear Housing Components: 2C23, 2D8 Rear View and Terminal Identification: 2C13 Rectifier Assembly: 2C14 Rectifier Ground and Positive Diode Test: 2C20 Rotor Continuity Test: 2D2 Rotor Ground Test: 2D2 Stator Continuity Test: 2D3 Stator Core and Windings: 2C14 Stator Ground and Negative Diode Test: 2C20 Stator Ground Test: 2D4 Artex ELT: 1L15 Artex ELT-110 Wiring Schematic: 1L16 Autopilot, S-TEC Component Locator 5J14 Installation 5J8 Avidyne Entegra Option Component Locator 5K11 Instrument Panel 5K9 Wiring Harness 5K15 B Baggage Door Lock Tool: 5I8 Balancing Aileron: 4D18 Rudder: 4C14 Stabilator: 4C9 Tool: 5D15 Brakes 30-83 Wheel Brake Assembly: 3F5 Anchor Bolt Installation: 3F7 Removal: 3F6 Hand/Parking Brake Master Cylinder: 3F10 System Installation: 3F9 Toe Brake Cylinder (10-30): 3F13 Toe Brake Installation: 3F11 C Cabin Heater & Defrosters: 1I14 Cherrylock Rivets, Removing: 1H23 Clamping Rudder Pedals: 2F17 Clamping RudderPedals in Neutral: 3D17 Control Cable Inspection Technique: 2E19 Internal Cable Wear: 2E21 Pulley Wear Patterns: 2E23 Wear Patterns, External: 2E20 Control Column Assembly: 2F3 Flex (Universal) Joint Assembly: 2F5 Control Surface Balancing Tool: 5I7 LIST OF ILLUSTRATIONS BY SUBJECT THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL List of Illustrations Page 2 Revised: February 16, 2004 1B2 D Defrosters: 1I14 Doors Adjustment of Upper Door Latch on Forward Cabin Door: 3K20 Snubber Seal Installation: 3K16 Dynafocal Mount: 4F7 E Electrical Schematics Air Conditioning: 5F4 Alternator Power: 5E14 Ammeter: 5F9 Annunciator: 5E2 Attitude Gyro, Electric: 5H6 Baggage Compartment Light: 5F10 Baggage Door Ajar: 5H2 CHT: 5F21, 5H12 Clock: 5F10 Courtesy Lights: 5G13 Data Acquisition Unit: 5H11 DDMP: 5F18 EGT: 5F22, 5H13 Electric Attitude Gyro: 5H6 ELT: 5H6 Engine Digital Display Monitoring Panel: 5F18 Engine Gauge: 5F14 Engine RPM: 5F20, 5H20 Entertainment Console: 5G23 Exceedance Audio Alert: 5H9 External Power: 5H7 Flaps: 5E12 Flood Lights: 5G4 Fuel Flow: 5F22, 5H13 Fuel Pump: 5F8 Fuel Quantity: 5F24, 5H16 Ground Clearance: 5E20 Hour Meter: 5F10 Landing Gear: 5G3 Landing Light(s): 5G7 Low Voltage Monitor: 5F9 Magneto Switch: 5F3 MAP: 5F16, 5H10 Navigation Lights: 5G10 Oil Pressure: 5F23, 5H15 Oil Temperature: 5F23, 5H15 Panel Lights: 5G16 Pitot Heat: 5E13 Power Point: 5H17 Radio Lights: 5G22 Radio Master Switch: 5E19 Reading Lights: 5G13 Recognition Lights: 5G12 RPM: 5F20, 5H10 Stall Warning: 5H3 Standby Attitude Indicator: 5H18 Starter and Accessories: 5E24 Strobe Lights: 5G10 Switch Lights: 5G16 Taxi Light(s): 5G7 TIT: 5F22, 5H14 Turn and Bank: 5G2 VAC: 5F21 Vacuum Inop: 5H5 Vacuum System, Standby: 5G24 Ventilation Blower: 5F7 Empennage Group: 4C6 Engine Installation: 4F5 Engine Instruments: 4I6 DDMP: 4I6, 4I12 Electrical Mode: 4I15 Exceedance Mode - Deleting: 4I16 Exceedance Mode - Viewing: 4I16 Fuel Load Entry: 4I21 Fuel Remaining: 4I20 Fuel To Destination: 4I20 Instrument Exceedance Condition: 4I13 Instrument Failure Condition: 4I13 Instrument Mode: 4I14 Percent Power - Calculating: 4I18 Percent Power - Current: 4I18 Temperature Mode: 4I19 Dual Instrument: 4I11 Single Instrument: 4I11 Engine Mount Installation: 4F7 Engine Timing Marks: 4G7 Exhaust System Inspection Points: 4J6 Exterior Placards and Markings: 1F18 F Flap System: 2G20 Cam Adjustment: 2G24 Installation: 4D15 Rigging Tool: 5H18 Selector and Cable Assembly: 2G22 Stop Screws Adjustment: 2G24 Torque Tube Assembly: 2G23 Flap Compensator Installation 5K1 Flareless Tube Fittings: 1I4 Fuel - Air Bleed Nozzle: 4F18 Fuel Cap Assembly, Locking: 2H24 Fuel Cell Components: 2H15 Fuel Filter Asssembly: 2I2 Fuel Filter Bowl and Screen: 1G10 Fuel Injection System, Schematic: 4F19 Fuel Injector: 4F20 LIST OF ILLUSTRATIONS (cont) BY SUBJECT THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL List of Illustrations Page 3 Revised: February 16, 2004 1B3 Fuel Quantity DDMP: 2I8 DDMP Cal. Menu Flow Chart: 2I10 Dual Gauge: 2I5, 2I8 Gauge Bench Test/Adjust Set- Up: 2I7 Needle Deviation: 2I6 Needle Display Limits at "E": 2I13 Needle Display Limits at "F": 2I13 Fuel System: 2H7 Fuel Tank / Wing Spar Corrosion Inspection: 2H13 H Heater: 1I14 Hose Markings: 1I3 Hydraulic System Installation: 2I22 Pump: 2J2 Schematic: 2I20 I Ignition Harness. See Ignition System, Harness Ignition System Engine Timing Marks: 4G7 Harness Cutting Insulation: 4H4 Driving Tool: 4H5 Flaring out the Shielding: 4H5 Inserting Stripping Tool: 4H4 Installation in Harness Cap: 4H7 Installation of Electrode Screw: 4H7 Installation of Ferrule: 4H5 Installation of Insulator Sleeve: 4H7 Installation of Plug Endnut: 4H5 Installation of Spring: 4H8 Removing Silicone Rubber from Wire: 4H4 Securing Wire inHarness Cap: 4H7 Stripping Tool: 4H4 Magneto(s) Bearing Bar Assembly: 4G21 Bearings, Installation: 4G17 Carbon Brush Assembly: 4G12 Coil Wedges, Removing: 4G16 Exploded View: 4G15 Impulse Coupling: 4G10 Impulse Coupling Pawls: 4G10 Internal Timing: 4G20 Measuring Pawl Clearance: 4G10 Oil Seal Installation: 4G18 Pressurized Magneto Pressure Testing: 4G23 Rotor: 4G9 Rotor Gear Alignment: 4G21 Stop Pin: 4G9 T-100 Assembly and Timing Tool Kit: 4G13 Spark Plugs, Removing Frozen: 4H10 Installing Rod End Bearings: 1H22 Interior Placards and Markings: 1F21 J Jacking: 1E11 L Landing / Pulse Lights Assembly and Relay: 3G10 Landing Gear Free-Fall (Emergency Release) Valve Assembly: 3E17 Main Actuating Cylinder: 3E14 Aligning: 3D1 Down Limit Switch Adjustment: 3F19 End Gland Locking Device: 3E13 Oleo Strut Assembly: 3C16 Removal and Installation: 3C20 Tolerances: 3D4 Nose Actuating Cylinder: 3E12 Adjustment: 3D15 Doors: 3D18 Eccentric Bushing, Adjustment: 3D15 Limit Switches, Adjustment: 3F17 Oleo Strut Assembly: 3D8 Removal and Installation: 3D12 Tolerances: 3D20 Leveling Airplane: 1E17 Line Markings: 1I3 Lubrication Charts Air Conditioning Condenser: 1H16 Baggage Doors: 1H15 Cabin Doors: 1H15 Control System: 1H6 Fuel Selector: 1H14 Landing Gear, Main: 1H2 Landing Gear, Nose: 1H4 Power Plant: 1H12 Propeller: 1H12 Seats: 1H15 LIST OF ILLUSTRATIONS (cont) BY SUBJECT THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL List of Illustrations Page 4 Revised: February 16, 2004 1B4 M Magneto(s). See Ignition System, Magneto(s) Markings - Hose, Tube, & Line: 1I3 Markings, Exterior: 1F18 Markings, Interior: 1F21 Materials and Thickness, Skin: 3J20 Mixture Control Adjustment: 4F23 O Overhead Vent System: 1I14 Overvoltage Relay Check: 2D16 Oxygen System Oxygen Cylinder: 3I6 Recharge Valve Installation: 3I9 Regulator Valve: 3I6 Swageloc Fittings, Installation: 3I3 System Installation: 3H16 Test Apparatus: 3H21 Tubing Installation: 3H23 P Pitch Servo Installation 5J21 Pitot Static System Installation: 2J19, 3G22 Placards, Exterior: 1F18 Placards, Interior: 1F21 Propeller Governor: 4E12 Installation: 4E6 Typical Nicks and Removal Method: 4E5 Pulley Wear Patterns: 2E23 Pulse Lights Assembly and Relay: 3G10 Pump, Hydraulic: 2J2 Motor Electrical Characteristics: 2I21 R Radio Master Switch Schematic: 1L13 Removing Cherrylock Rivets: 1H23 Repairs Thermoplastic Abrasions: 3K2 Cracks: 3K4 Deep Scratches: 3K3 Ground-in-Dirt: 3K2 Impact Damage: 3K7 Mixing Epoxy: 3K3 Shallow Nicks: 3K3 Small Holes: 3K3 Stress Lines: 3K7 Surface Scratches: 3K2 Various Repairs: 3K5 Welding Repair Method: 3K4 Rod End Installation Method: 2E18 Roll Servo Capstan Wrapping 5J16 Roll Servo Installation 5J15 Rudder and Steering Pedal Assembly: 2F20 Rudder Balancing: 4C14 Rudder Controls: 2F15 Rudder Pedals at Neutral Angle: 3D17 Rudder Rigging: 2F17 Rudder Rigging Limits: 2F17 Rudder Rigging Tool: 5I9 Rudder Travel Adjustments: 2F17 Rudder Trim Control: 2F19 S Service Points: 1G9 Servo Clutch Torque Adjustment 5J24 Skin Materials and Thickness: 3J20 Spark Plugs. See Ignition System Stabilator and Tab Rigging Limits: 2G6 Stabilator Attach Brackets: 4C10 Stabilator Balancing: 4C9 Stabilator Controls: 2G4 Stabilator Rigging: 2G13 Stabilator Rigging Tool: 5I11 Stabilator Travel Adjustments: 2G7 Stabilator Trim Controls: 2G9 Securing Trim Cables: 2G8 Wrapping Trim Barrels: 2G12 Starting Motor Exploded View: 4J21 No-Load Test Hook-up: 4K5 Stall-Torque Hook-up: 4K5 Testing Armature for Shorts: 4K3 Testing Fields for Grounds: 4K3 Turning Commutator: 4K3 Station Reference Lines: 1E5 Strobe Light Connections: 3G12 Swageloc Fittings, Installation: 3I3 T Thermoplastic Repairs. See Repairs, Thermoplastic Three View: 1E1 Throttle Control Adjustment: 4F23 Throttle Warning Switch: 3F21 Tire Balancer Fixture: 5I5 Torque Wrench Formula: 1H22 Trim Servo Installation 5J19 Tube Markings: 1I3 Turbocharger Installation: 4L13 Wastegate Adjustment: 4L14 Wastegate Installation: 4L14 LIST OF ILLUSTRATIONS (cont) BY SUBJECT THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL List of Illustrations Page 5 Revised: February 16, 2004 1B5 V Vent System, Overhead: 1I14 Voltage Regulator Check: 2D16 W Weighing: 1E19 Wheel Balancer: 1G21 Wheels Main Wheel Assembly: 3F3 Nose Wheel Assembly: 3F1 Windows Side Window Installation: 4C23 Windshield Installation: 4C21 Wing Installation: 4D10 LIST OF ILLUSTRATIONS (cont) BY SUBJECT THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL List of Illustrations Page 6 Revised: February 16, 2004 1B6 THIS PAGE INTENTIONALLY BLANK THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL List of Charts Page 1 Revised: February 16, 2004 1B7 LIST OF CHARTS BY SUBJECT A A/C System Troubleshooting: 1I21 Vacuum - Evacuating: 1J11 York Compressor Idler Pulley Nominal Offset: 1K12 York Compressor Oil Charge: 1K6 Airspeed Indicator and Tubes, Troubleshooting: 3H3 Altimeter, Troubleshooting: 3H2 Annunciator, Troubleshooting: 2K5 Attitude Indicator, Troubleshooting: 3H5 B Blower System Wire Color Codes: 1I18 C Cable Tension Vs Ambient Temperature: 2E18 Consumable Materials List: 5C15 Conversion Tables: 5C10 D Decimal Conversions: 5C9 Directional Gyro, Troubleshooting: 3H6 E Electrical Symbols: 5D6 Electrical System Component Loads: 2D19 Electrical Wire Coding: 5D5 Engine Instrumentation Calibration: 4I22 Engine, Troubleshooting: 4F1 Extension and Retraction, Troubleshooting: 3E1 F Flare Fitting Torques: 5C5 Fuel Cell Repair Equipment Lists: 2H17 Fuel Quantity Analog Gauge / Sender Tolerances: 2I6 Gauge Bench Test Tolerances: 2I8 Gauge Tolerances: 2I12 Fuel System - Troubleshooting: 2H9 H Hydraulic System: 2I21 Leading Particulars: 2I21 Pump Motor Electrical Characteristics: 2I21 Hydrometer Reading and Battery Charge Percent: 2D11 I Ignition Harness - Spark Plug Coupling Torque: 4H11 L Landing Gear Toe-in / Toe-out Correction: 3D2 Troubleshooting: 3C8 Leading Particulars and Principal Dimensions: 1E2 M Magnetic Compass, Troubleshooting: 3H9 Magnetos, Troubleshooting: 4G6 Maximum Allowable Resistance Values: 1I5 Maximum Distance Between Supports for Fluid Tubing: 1I6 N Nut Torques: 5C7 O Oxygen System Component Limits: 3H21 Filling Pressure vs. Temperature: 3I15 Troubleshooting: 3H17 P Propeller Torque Limits: 4E7 R Recommended Nut Torques: 5C7 Recommended Torque Specifications: 1J7 Refrigerant Temperature vs. Pressure: 1J4 S Sanden Compressor Oil Level vs. Mounting Angle: 1K7 Servo Clutch Torque: 5J23 Spark Plug - Ignition Harness Coupling Torque: 4H11 Starting Motor Service Test Specifications: 4K5 Structural Inspection and Replacement: 1B23 THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL List of Charts Page 2 Revised: February 16, 2004 1B8 T Thermoplastic Repair List of Materials: 3K1 Thread Lubricants: 1G23 Toe-in / Toe-out Correction: 3D2 Torque Specifications: 1J7 Torque - Spark Plug - Ignition Harness Coupling Torque: 4H11 Troubleshooting: 2H9 Aileron Control System: 2F1 Air Conditioning System: 1I21 Airspeed Indicator and Tubes: 3H3 Altimeter: 3H2 Annunciator: 2K5 Attitude Indicator: 3H5 CHT Gauge: 4I3 Directional Gyro: 3H6 EGT Gauge: 4I2 Electrical System: 2C7 Engine: 4F1 Extension and Retraction: 3E1 Fuel System: 2H9 Landing Gear: 3C8 Magnetic Compass: 3H9 Magnetos: 4G6 Manifold Pressure Gauge: 4H21 Oil Pressure Gauge: 4H23 Oil Temperature Indicator: 4I1 Oxygen System: 3H17 Rudder Control System: 2F13 Stabilator Control System: 2G1 Starter: 4J22 Tachometer: 4H22 Turbocharger: 4L6 Turn and Bank Indicator: 3H10 Vacuum System: 3I21 Vertical Speed Indicator: 3H1 Turn and Bank Indicator, Troubleshooting: 3H10 V Vacuum System, Troubleshooting: 3I21 Vendor Addresses: 5D1 Vertical Speed Indicator, Troubleshooting: 3H1 Y York Compressor Idler Pulley Nominal Offset: 1K12 York Compressor Oil Charge: 1K6 LIST OF CHARTS (cont) BY SUBJECT THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL List of Charts Page 3 Revised: February 16, 2004 1B9 THIS PAGE INTENTIONALLY BLANK THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL List of Charts Page 4 Revised: February 16, 2004 1B10 THIS PAGE INTENTIONALLY BLANK THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL 1B11 CHAPTER AIRWORTHINESS LIMITATIONS 4 THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL 1B12 THIS PAGE INTENTIONALLY BLANK THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL 4-Cont./Effec. Page 4-3 Revised: February 16, 2004 1B13 CHAPTER 4 - AIRWORTHINESS LIMITATIONS TABLE OF CONTENTS / EFFECTIVITY 4-00-00 AIRWORTHINESS LIMITATIONS .........................1B15 4R0204 CHAPTER/ GRID SECTION SUBJECT NO. EFFECTIVITY THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL 4-Cont./Effec. Page 4-4 Revised: February 16, 2004 1B14 THIS PAGE INTENTIONALLY BLANK THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL 4-00-00 Page 4-5 Revised: February 16, 2004 1B15 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. No limitations, related to fatigue life of the airplane and its components, have been established for the PA-32R-301 nor the PA-32R-301T: 2. 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 dispositioned of in accordance with the applicable FARs. Piper recommends life limited parts with no time and/or cycles remaining be completely destroyed. — Note — Refer to the LIMITATIONS in the Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual for a detailed delineation of the flight limitations of the airplane. THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL 4-00-00 Page 4-6 Revised: February 16, 2004 1B16 THIS PAGE INTENTIONALLY BLANK 1B17 THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL CHAPTER TIME LIMITS / MAINTENANCE CHECKS 5 THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL 1B18 THIS PAGE INTENTIONALLY BLANK THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL 5-Cont./Effec. Page 5-3 Revised: February 16, 2004 1B19 CHAPTER 5 - TIME LIMITS / MAINTENANCE CHECKS TABLE OF CONTENTS / EFFECTIVITY 5-00-00 GENERAL .....................................................1B21 4R0204 5-10-00 TIME LIMITS .................................................1B23 4R0204 5-20-00 SCHEDULED MAINTENANCE.............................1C1 2R1201 Description ......................................................1C1 2R1201 Definitions ......................................................1C1 4R0204 Inspection Requirements.......................................1C3 4R0204 Annual / 100 Hour Inspection ..............................1C3 4R0204 Progressive Inspection ......................................1C4 2R1201 Overlimits Inspection .......................................1C4 4R0204 Annual / 100 Hour Inspection Procedure .....................1C4 4R0204 Scheduled Maintenance ........................................1C7 4R0204 SARATOGA II HP (S/N’s 3246001 & up)................1C7 4R0204 Propeller Group...........................................1C7 4R0204 Engine Group .............................................1C7 4R0204 Cabin and Cockpit Group ...............................1C10 4R0204 Fuselage and Empennage Group .......................1C10 4R0204 Wing Group ..............................................1C12 4R0204 Landing Gear Group.....................................1C12 4R0204 Special Inspections ......................................1C13 4R0204 Operational Inspection ..................................1C14 4R0204 General ...................................................1C14 4R0204 Notes......................................................1C15 4R0204 SARATOGA II TC (S/N’s 3257001 & up) ...............1C19 4R0204 Propeller Group ..........................................1C19 4R0204 Engine Group ............................................1C19 4R0204 Turbocharger Group .....................................1C22 4R0204 Cabin and Cockpit Group ...............................1C22 4R0204 Fuselage and Empennage Group .......................1C23 4R0204 Wing Group ..............................................1C24 4R0204 Landing Gear Group .....................................1D1 4R0204 Special Inspections .......................................1D2 4R0204 Operational Inspection ...................................1D2 4R0204 General ....................................................1D3 4R0204 Notes ......................................................1D4 4R0204 CHAPTER/ GRID SECTION SUBJECT NO. EFFECTIVITY THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL 5-Cont./Effec. Page 5-4 Revised: February 16, 2004 1B20 CHAPTER/ GRID SECTION SUBJECT NO. EFFECTIVITY CHAPTER 5 - TIME LIMITS / MAINTENANCE CHECKS TABLE OF CONTENTS / EFFECTIVITY (continued) 5-30-00 SPECIAL INSPECTIONS.....................................1D9 4R0204 Flight Hours.....................................................1D9 A0204 Calendar Year ..................................................1D10 A0204 Per Specific Operation/Operating Environment.............1D12 4R0204 Operation in High Dust or Industrial Pollution ..........1D12 4R0204 Operation in High Salt or High Humidity ................1D13 4R0204 Operation in Extreme Cold ................................1D14 4R0204 Operation from Soft or Unusual Terrain ..................1D14 4R0204 5-50-00 UNSCHEDULED MAINTENANCE CHECKS ............1D15 2R1201 Lightning Strike................................................1D15 4R0204 Engine Events ..................................................1D16 2R1201 Severe Turbulence, Hard or Overweight Landing...........1D17 4R0204 THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL 5-00-00 Page 5-5 Revised: February 16, 2004 1B21 GENERAL. The New Piper Aircraft, Inc. (Piper) takes a continuing interest in having the owner get the most efficient use from his airplane, and keeping the airplane in the best mechanical condition. To that end, Piper publishes a recurring maintenance schedule which is supplemented with Service Bulletins, Service Letters and Service Spares Letters as required. (a) The recurring maintenance schedules for the PA-32R-301/301T Saratoga II HP and TC are provided in 5-20-00. (b) Piper Service Bulletins are of special importance and Piper considers compliance mandatory. These are sent to the latest U.S. registered owners and Piper Service Centers. (c) Service Letters deal with product improvements and service hints pertaining to the aircraft. They are sent to Piper Service Centers and sometimes directly to owners, so they can properly service the aircraft and keep it up to date with the latest changes. Owners should give careful attention to the service letter information. (d) Service Spares Letters, which are sent only to Piper Service Centers, offer improved parts, kits and optional equipment which were not available originally and which may be of interest to the owner. — Note — Piper mails Service Bulletins, Service Letters, and P.O.H. Revisions to the registered owner’s name and address as shown on the Aircraft Registration Certificate. If the aircraft is based and/or operated at a different location (or locations) and/or by a person (or persons) other than those recorded on the aircraft registration, then the registered owner(s) is responsible for forwarding these Bulletins and Letters to the operating location(s) or person(s). Changes in aircraft registration may take a substantial amount of time to be recorded by the Federal Aviation Administration and received by Piper to change the mailing address. Owners and operators should make arrangements to keep abreast of service releases during this interim period through their Piper Service Center. The Federal Aviation Administration (FAA) publishes Airworthiness Directives (AD’s) that apply to specific aircraft. They are mandatory changes and are to be complied within a time limit set by the FAA. When an AD is issued, it is sent to the latest registered owner of the affected aircraft and also to subscribers of the service. The owner is solely responsible for being aware of and complying with airworthiness directives. — Note — A searchable database of AD’s is available on the FAA website. See the “Airworthiness DIrectives” link at “www1.faa.gov”. Additionally, Avantext offers a free email notification service for new AD’s as well as the last six weeks worth of AD’s at “www.avantext.com”. An owner should periodically check with a Piper Service Center to find out the latest information to keep his aircraft up to date. THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL 5-00-00 Page 5-6 Revised: February 16, 2004 1B22 The New Piper Aircraft, Inc. has a subscription service for the Service Bulletins, Service Letters, and Service Spares Letters. This service is offered to interested persons such as owners, pilots, and mechanics at a nominal fee and may be obtained through Piper Service Centers. Owners residing outside of the United States are urged to subscribe to this service since Piper cannot otherwise obtain the addresses of foreign owners. Maintenance Manuals and Illustrated Parts Catalogs are also available through Piper Service Centers and Distributors world wide. THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL 5-10-00 Page 5-7 Revised: February 16, 2004 1B23 TIME LIMITS. 1. Refer to 4-00-00 for the FAA-approved airworthiness limitations section. It sets forth each mandatory replacement time, structural inspection interval, and related structural inspection procedure required for type certification. 2. Refer to 5-20-00 for Piper’s recommended Inspection Program. It includes the frequency and extent of the inspections required for the continued airworthiness of the airplane. 3. Inspections required by Flight Hour or Calendar Year, if due, are included as part of the Annual / 100 Hour Inspection and/or the Progressive Inspection Event cycles, and are listed individually in 5-30-00. THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL 5-10-00 Page 5-8 Revised: February 16, 2004 1B24 THIS PAGE INTENTIONALLY BLANK THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL 5-20-00 Page 5-9 Revised: February 16, 2004 1C1 SCHEDULED MAINTENANCE This section provides instructions for conducting inspections. For repair or replacement instructions of those components found to be unserviceable during inspections, refer to the chapter(s) covering the applicable airplane system. — WARNING — GROUND THE MAGNETO PRIMARY CIRCUIT (P LEAD), BEFORE PERFORMING ANY MAINTENANCE OPERATION ON ENGINE. 1. DESCRIPTION. — WARNING — FAILURE TO CONSULT APPLICABLE VENDOR PUBLICATION(S), WHEN SERVICING OR INSPECTING VENDOR EQUIPMENT INSTALLED IN PIPER AIRCRAFT, MAY RENDER THE AIRCRAFT UNAIRWORTHY. (SEE INTRODUCTION - SUPPLEMENTARY PUBLICATIONS.) The recurring maintenance schedules for the PA-32R-301 Saratoga II HP and PA-32R-301T Saratoga II TC are provided herein as Annual / 100 Hour Inspections. Progressive Inspection Programs will be available from Piper Distributors in a separate manual form. Piper inspection programs comply with the Federal Aviation Regulations Parts 43, 91 and 135. The owner/operator is primarily responsible for maintaining the airplane in an airworthy condition, including compliance with all applicable Airworthiness Directives and conformity with the requirements in FAR 91.409, 91.411 and 91.413. The first overhaul or replacement of components should be performed at the given periods. The condition of various components can then be used as criteria for determining subsequent periods applicable to the individual airplane, depending on usage, providing the owner/operator has an established Part 91 Progressive Inspection Program (see 91.409(d)) or Part 135 Approved Aircraft Inspection Program (see 135.419). The time periods given for inspections of various components are based on average usage and environmental conditions. — Note — The listed inspection, overhaul and replacement schedules do not guarantee that a particular item or component will reach the listed time without malfunction. Unique operating conditions encountered by individual airplanes cannot be controlled by the manufacturer. 2. DEFINITIONS. A. Inspections - Must be performed only by Certified Mechanics who are qualified on this aircraft, utilizing acceptable methods, techniques and practices to determine physical condition and detect defects. (1) Routine Inspection - Consists of a visual examination or check of the aircraft and its components and systems without disassembly. (2) Detailed Inspection - Consists of a thorough examination of the aircraft, appliance, component, or system; with disassembly as necessary to determine condition. THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL 5-20-00 Page 5-10 Revised: February 16, 2004 1C2 (3) Special Inspection - Involves those components, systems or structure which by their application or intended use require an inspection peculiar to, more extensive in scope or at a time period other than that which is normally accomplished during an event or annual inspection. B. Checks - Can be performed by pilots and/or mechanics who are qualified on this aircraft and consists of examinations in the form of comparisons with stated standards for the purpose of verifying condition, accuracy and tolerances. C. Approved Inspection - Means a continuing airworthiness inspection of an airplane and its various component and systems at scheduled interval in accordance with procedures approved by the FAA under FAR Part 91.409(d) or Part 135.419. D. Tests - Operation of aircraft components, appliances or systems to evaluate functional performance. (1) Operational Test - A task to determine that an item, is fulfilling its intended purpose.The task does not require quantitative tolerances. This is a fault finding task. (2) Functional Test - A quantitative check to determine, if one or more functions of an item performs within specified limits. This test may require the use of supplemental bench test equipment. (3) In addition, each of the above tests must be performed by an FAA Certified Repair Station with appropriate ratings or by a Certified Mechanic who is qualified on this aircraft. The recording of the above function must be made in the permanent aircraft records by the authorized individual performing the test. E. Bench Test - Means removal of component from the aircraft to inspect for cleanliness, impending failure, need for lubrication, repair or replacement of parts and calibration to at least the manufacturers specifications using the manufacturers recommended test equipment or standards or the equivalent. Each bench test will be performed by a Piper Service Center, FAA Certified Repair Station with appropriate rating or by a certified mechanic. This test will be performed at the scheduled interval regardless of any bench test performed on a particular component while being repaired/overhauled before scheduled interval bench test. After the component is installed into the aircraft, an operational test of the component and its related system should be performed to ensure proper function. Serviceable parts that were issued to the component will be filed in the aircraft permanent records. The person performing the check must make appropriate entries in the aircraft’s permanent maintenance record. F. Maintenance - The word maintenance as defined by FAR Part 1, means “inspection, overhaul, repair, preservation and the replacement of parts, but excludes preventive maintenance.” G. On Condition Maintenance - A primary maintenance process having repetitive inspections or tests to determine the condition of units, systems, or portions of structure with regard to continued serviceability (corrective action is taken when required by item condition.) THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL 5-20-00 Page 5-11 Revised: February 16, 2004 1C3 H. Time - as used in this manual. (1) Time-in-service for aircraft components, unless otherwise specified, is a cumulative total of flight hours or calendar time calculated from the time a new or overhauled component was first installed in any aircraft, and including: (a) the aircraft time that elapses from the initial installation to the first removal, if any; and, (b) the aircraft time that elapses from each subsequent installation to each subsequent removal, if any; or, (c) the calendar time elapsed since the installation. — Note — Dates stamped on individual components at the time of manufacture are typically applied to determine shelf life - i.e. the maximum time allowed from manufacture/ assembly/cure until actually installed in an aircraft and are not relevant. Do not, however; ignore markings applied to life-limited parts when removed with time and/or cycles remaining on them. (2) Aircraft time, flight hours, or aircraft hours are the “Hobbs Time” shown on, or calculated from, the installed “Hour Meter.” 3. INSPECTION REQUIREMENTS. — 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. A. Annual / 100 Hour Inspection. (See paragraph 4.) Owners/operators may maintain the airplane solely under FAR 91.409 (a) and (b) inspection requirements. The 100 hour inspection cycle is a complete inspection of the airplane and is identical in scope to an annual inspection. Inspections must be accomplished by persons authorized by the FAA. THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL 5-20-00 Page 5-12 Revised: February 16, 2004 1C4 B. Progressive Inspection. The Progressive Inspection program was designed to permit the best utilization of the aircraft through the use of a planned inspection schedule. This schedule is prepared in a manual form, which will be available from Piper Distributors: P/N 761-881 (pending) for the SARATOGA II HP (S/N’s 3246001 & up), and P/N 761-896 (pending) for the SARATOGA II TC (S/N’s 3257001 & up). Refer to Piper's Customer Service Information Aerofiche P/N 1761-755 for a checklist to ensure obtaining latest issue. — Note — The 50 Hour Progressive Inspection Manuals (P/N’s 761-881 and 761-896) referenced above will not be stand-alone documents. They will consitute snapshots of the Airworthiness Limitations and Inspection sections of the Instructions for Continued Airworthiness (ICA) and will be current only at the time of printing. Use them as follows: (1) Owners/operators desiring to establish a Part 91 Progressive Inspection Program (PIP) (see 91.409(d)) or a Part 135 Approved Aircraft Inspection Program (AAIP) (see 135.419) should use the appropriate Progressive Inspection Manual as a template for submission to their regional FAA office. (2) Service centers conducting Event Cycle inspections under a FAA-approved PIP or AAIP can use the appropriate Progressive Inspection Manual as a working check-off list/form, provided they verify its currency against the FAA-approved PIP or AAIP. C. Overlimits Inspection. If the airplane has been operated so that any of its components have exceeded their maximum operational limits, special inspections may be required by Piper and/or the component manufacturer. See 5-50-00. 4. ANNUAL / 100 HOUR INSPECTION PROCEDURE. A. Scheduled Maintenance (i.e. - paragraphs 5 and 6) (1) The required periodic inspection procedures are listed in paragraphs 5 (PA-32R-301) and 6 (PA-32R-301T). These inspection procedures are broken down into major groups which include Propeller, Engine, Cabin and Cockpit, Fuselage and Empennage,Wing, Landing Gear, Operational Inspection and General. The first column in each group lists the inspection or procedure to be performed. The second column is divided into two sub-columns indicating the required inspection intervals of 50 hours or 100 hours. Each inspection or operation is required at each of the inspection intervals indicated by a circle (O). When vendor publications specify times outside the 100 hour cycle, it will be indicated as: in the inspection interval columns, or listed as a special inspection in 5-30-00, or both. As req'd by “applicable vendor publication.” THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL 5-20-00 Page 5-13 Revised: February 16, 2004 1C5 (2) Refer to the applicable chapter of this manual for instructions on how to gain access to remove any item that must be removed and is not completely accessible. (3) Inspection Report Forms. To help in the performance of periodic inspections, Inspection Report forms are available through Piper Dealers: P/N 230-1047 for the SARATOGA II HP (S/N’s 3246001 & up), and P/N 230-2047 for the SARATOGA II TC (S/N’s 3257001 & up). — Note — Service centers conducting Part 91 Annual / 100 Hour Inspections can use the Inspection Report Forms (P/N’s 230-1047 and 230-2047), as working check-off lists, provided they verify their currency against an up-to-date copy of the ICA (i.e. - this Maintenance Manual, see 4-00-00 and 5-20-00). (4) In addition to inspection intervals required in scheduled maintenance (i.e. - paragraphs 5 and 6), preflight inspection must also be performed. (5) References to maintenance manual applicable areas are per the “chapter - system/sub-system” assignment of subject material numbering system. B. Special Inspections (See 5-30-00.) C. Unscheduled Maintenance (See 5-50-00.) THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL 5-20-00 Page 5-14 Revised: February 16, 2004 1C6 THIS PAGE INTENTIONALLY BLANK THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL 5-20-00 Page 5-15 Revised: February 16, 2004 1C7 A. PROPELLER GROUP —WARNING — USE EXTREME CAUTION WHEN ROTATING PROPELLER BY HAND; PROPELLER MAY KICK BACK. PRIOR TO ROTATING PROPELLER ENSURE BOTH MAGNETO SWITCH(S) ARE OFF (GROUNDED). IF MAGNETO(S) ARE NOT GROUNDED, TURNING PROPELLER MAY START ENGINE. 1. Inspect spinner and back plate for cracks, dents, missing screws, and security ........................... O O 2. Inspect blades for nicks and cracks............................................................................................... O O 3. Check for grease and oil leaks ...................................................................................................... O O 4. Lubricate propeller per Lubrication Chart in maintenance manual.............................................. O O 5. Inspect spinner mounting brackets for cracks and security .......................................................... O 6. Inspect propeller mounting bolts for security and safety. Recheck torque values if safety is broken..................................................................................... O 7. Inspect hub parts for cracks and corrosion ................................................................................... O 8. Rotate blades and check for tightness in hub pilot tube ............................................................... O 9. Inspect complete propeller and spinner assembly for security, chafing, cracks, deterioration, wear, and correct installation...................................................................... O 10. Overhaul or replace propeller governor. (See Note 36.)............................................. 11. Overhaul propeller. (See Note 37.) ............................................................................. B. ENGINE GROUP —WARNING — IF MAGNETO(S) ARE NOT GROUNDED, TURNING PROPELLER MAY START ENGINE. USE EXTREME CAUTION WHEN ROTATING PROPELLER BY HAND; PROPELLER MAY KICK BACK. PRIOR TO ROTATING PROPELLER ENSURE BOTH MAGNETO SWITCH(S) ARE OFF (GROUNDED). — Note — Read Note 5 prior to completing the following items. 1. Remove engine cowl and inspect for internal and external damage. (See Note 26.).................... O O 2. Clean and inspect cowling for cracks, distortion, and loose or missing fasteners........................ O 3. Drain oil sump .............................................................................................................................. O O 4. Clean suction oil strainer at oil change; inspect strainer for foreign particles.............................. O O As req'd by Hartzell Svc. Ltr. No. 61 5. SCHEDULED MAINTENANCE - SARATOGA II HP (S/N’s 3246001 & up) Refer to Notes 1, 2, 3, and 4 before performing the following inspections. Inspection Interval (Hrs) NATURE OF INSPECTION 50 100 THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL 5-20-00 Page 5-16 Revised: February 16, 2004 1C8 B. ENGINE GROUP (cont.) 5. Change full flow, cartridge type, oil filter element; inspect element for foreign particles. (See Note 7.).................................................................................................................. O O 6. Inspect oil temperature sender unit for leaks and security............................................................ O 7. Inspect oil lines and fitting for leaks, security, chafing, dents, and cracks ................................... O O 8. Clean and inspect oil radiator cooling fins ................................................................................... O 9. Fill engine with oil per information on cowl or lubrication chart, 12-20-00................................ O O 10. Clean engine with approved solvents ........................................................................................... O —CAUTION — USE CAUTION NOT TO CONTAMINATE VACUUM PUMP WITH CLEANING FLUID. (REFER TO LATEST REVISION TEXTRON LYCOMING SERVICE INSTRUCTION NO. 1221.) 11. Inspect condition of spark plugs. Clean and adjust gap as required; adjust per latest revision Textron Lycoming Service Instruction No. 1042................................................... O — NOTE — IF FOULING OF SPARK PLUGS IS APPARENT, ROTATE BOTTOM PLUGS TO UPPER PLUGS. 12. Inspect spark plug cable leads ..................................................................................................... O O 13. Check cylinder compression. (Refer to AC 43.13-1, latest revision.).......................................... O 14. Inspect cylinders for cracked or broken fins. (See Note 9.)......................................................... O — Note — Textron Lycoming requires a Valve Inspection be made after every 400 hours of operation. (See 5-30-00.) 15. Inspect rocker box covers for evidence of oil leaks. If found, replace gasket; torque cover screws 50 inch-pounds............................................................................................. O O 16. Inspect ignition harness and insulators for high tension leakage and continuity.......................... O 17. Check magneto points for proper clearance.. ............................................................................... O 18. Inspect magneto for oil seal leakage............................................................................................. O 19. Inspect magnetos to engine timing ............................................................................................... O 20. Remove air filter and clean per Chapter 12. Replace as required. (See Note 30.)........................ O O 21. Clean fuel injector inlet line screen .............................................................................................. O O 22. Inspect condition of alternate air valve and housing .................................................................... O O 23. Inspect intake seals for leaks and clamps for tightness. (Torque clamps 40-50 in.-lbs.).............. O O 5. SCHEDULED MAINTENANCE - SARATOGA II HP (S/N’s 3246001 & up) (CONTINUED) Refer to Notes 1, 2, 3, and 4 before performing the following inspections. Inspection Interval (Hrs) NATURE OF INSPECTION 50 100 THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL 5-20-00 Page 5-17 Revised: February 16, 2004 1C9 B. ENGINE GROUP (cont.) 24. Inspect all air inlet duct hoses. Replace as required. .................................................................... O O 25. Inspect condition of flexible fuel lines ......................................................................................... O 26. Inspect fuel system for leaks......................................................................................................... O 27. Inspect engine-driven and electric fuel pumps for operation........................................................ O 28. Overhaul or replace engine-driven and electric fuel pumps. (See Note 11.).............. 29. Inspect and operationally test engine driven and auxiliary vacuum pumps and lines. (See Notes 12 and 33; and 500 Hour special inspection, 5-30-00.) ............................. O 30. Inspect throttle, alternate air, mixture, and propeller governor controls for security, travel, and operation condition ................................................................................. O 31. Inspect exhaust stacks, connections and gaskets. Replace gaskets as required. (Refer to Chapter 78) ................................................................................................................... O O 32. Inspect muffler, heat exchange, and baffles. (Refer to Chapter 78.)............................................. O O 33. Inspect breather tube for obstructions and security ...................................................................... O 34. Inspect crankcase for cracks, leaks, and security of seam bolts ................................................... O 35. Inspect engine mounts for cracks and loose mounting ................................................................. O 36. Inspect all engine baffles ............................................................................................................. O 37. Inspect rubber engine mount bushings for deterioration. (Replace as required.) ......................... O 38. Inspect firewall seals..................................................................................................................... O 39. Inspect condition and tension of alternator drive belt. (Refer to Chapters 21 and 24 if air conditioning is installed)....................................................... O O 40. Lubricate alternator idler pulley (if installed); remove front grease seal and add grease. (Refer to lubrication chart, 12-20-00.) (Disregard if sealed bearing is installed) ...................................................................................... O 41. Inspect condition of alternator and starter .................................................................................... O 42. Inspect security of alternator or mounting.................................................................................... O 43. Check air conditioning compressor oil level. (See Note 14.) ....................................................... O 44. Inspect condition of compressor belt and tension. (Refer to Chapter 21.) ................................... O O 45. Inspect compressor clutch security and wiring. (See Note 15.).................................................... O 46. Inspect compressor mounting for cracks, corrosion, and security................................................ O 47. Check fluid in brake reservoir. Fill as required............................................................................. O O 48. Inspect and lubricate all controls. (Refer to 12-20-00.)................................................................ O 49. Complete overhaul of engine or replace with factory rebuilt. (See Lycoming Service Bulletin No. 240.)................................................................. 50. Install engine cowl ........................................................................................................................ O O Engine Overhaul or 5 yrs. 5. SCHEDULED MAINTENANCE - SARATOGA II HP (S/N’s 3246001 & up) (CONTINUED) Refer to Notes 1, 2, 3, and 4 before performing the following inspections. Inspection Interval (Hrs) NATURE OF INSPECTION 50 100 As req'd by Lycoming Svc. Instr. No. 1009 THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL 5-20-00 Page 5-18 Revised: February 16, 2004 1C10 C. CABIN AND COCKPIT GROUP 1. Inspect cabin entrance, doors, and windows for damage, operation, and security ....................... O 2. Inspect windows for scratches, crazing, and condition................................................................. O 3. Check window and door seals for deterioration, cracks, and voids. (Refer to Chapter 56.)......... O 4. Inspect upholstery for tears........................................................................................................... O 5. Inspect seats, seat belts, shoulder harnesses, security brackets, and bolts. (See Seat Belt and Shoulder Harness Inspection, 25-10-00.) ....................................................... O 6. Inspect trim operation ................................................................................................................... O 7. Inspect rudder pedals .................................................................................................................... O 8. Inspect parking brake valve and brake handle for operation and cylinder leaks .......................... O 9. Inspect control wheels, column, pulleys, and cables. (See Notes 16 and 32.).............................. O 10.Inspect electric flap screw jack and attachments for condition and lubrication............................ O 11. Check landing, navigation, strobe, cabin, and instrument lights .................................................. O O 12. Inspect instruments, lines, and attachments. (See Note 28.)......................................................... O 13. Inspect gyro operated instruments and electric turn and bank. (Overhaul or replace as required.) ................................................................................................ O 14. Replace central air filter................................................................................................................ O 15. Clean or replace vacuum regulator filter....................................................................................... O 16. Inspect altimeter and transponder for installation/certification per latest revision of AC43.13-1 and tested/inspected per FAR’s 91.411 and 91.413, respectively. (See Two (2) Year special inspection, 5-30-00.) ........................................................................... O 17. Inspect and test ELT per FAR 91.207. (See Testing ELT, 23-20-00.)........................................... O 18. Inspect operation of fuel selector valve. ....................................................................................... O 19. Inspect fuel valve drain lever cover for security. Check that door opens and closes freely and prevents operation of lever when closed ........................................................... O O 20. Inspect condition of heater controls and ducts.............................................................................. O 21. Inspect condition and operation of air vents ................................................................................. O 22. Inspect condition of air conditioning ducts................................................................................... O 23. Remove and clean air conditioning evaporator filter .................................................................... O D. FUSELAGE AND EMPENNAGE GROUP 1. Remove inspection plates and panels ........................................................................................... O 2. Check forward and rear wing attach bolts and fittings for corrosion. (Refer to Chapter 57.) ...... O 3. Inspect baggage doors, latches, and hinges for operation and security ........................................ O O 4. Inspect battery, box or shelf, and cables. Flush box as required and fill battery per instructions on box or in Chapter 24........................... O 5. Inspect electronic installations...................................................................................................... O 5. SCHEDULED MAINTENANCE - SARATOGA II HP (S/N’s 3246001 & up) (CONTINUED) Refer to Notes 1, 2, 3, and 4 before performing the following inspections. Inspection Interval (Hrs) NATURE OF INSPECTION 50 100 THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL 5-20-00 Page 5-19 Revised: February 16, 2004 1C11 D. FUSELAGE AND EMPENNAGE GROUP (cont.) 6. Inspect skins, bulkheads and stringers for damage....................................................................... O 7. Inspect antenna mounts and electric wiring.................................................................................. O 8. Check hydraulic pump fluid level. Fill as required....................................................................... O O 9. Inspect hydraulic pump lines for damage and leaks ..................................................................... O 10. Inspect air conditioning system for refrigerant leaks. (See Note 14.) .......................................... O 11. Inspect refrigerant level in sight gauge of receiver-dehydrator. (Refer to Chapter 21.) ............... O O 12. Inspect air conditioner condenser air scoop for condition and rigging. (See Note 38.) ............... O O 13. Inspect fuel lines, valves, and gauges for damage and operation ................................................. O 14. Remove, drain, and clean fuel strainer bowl and screen located in bottom of selector valve ...... O 15. Inspect security of all lines ........................................................................................................... O 16. Inspect vertical fin and rudder surfaces for damage ..................................................................... O 17. Inspect rudder hinges, sector and attachments for damage, security, & operation....................... O 18. Inspect vertical fin attachments for security ................................................................................. O 19. Inspect rudder control stops to ensure stops have not loosened and locknuts are tight................ O 20. Inspect rudder hinge bolts for excess wear. Replace as required.................................................. O 21. Inspect stabilator surfaces for damage.......................................................................................... O 22. Inspect stabilator tab hinges, horn, and attachments for damage, security, and operation ........... O 23. Inspect stabilator attachments and attach brackets for corrosion, rust, and security. Repair as required. (Refer to Stabilator Attach Brackets Corrosion Inspection, 55-10-00) ......... O 24. Inspect stabilator and tab hinge bolts and bearings for excess wear. Replace as required ........... O 25. Inspect stabilator control stops to ensure stops are not loose. Ensure bolts and locknuts are tight........................................................................................................................... O 26. Inspect rudder and stabilator cables and check all cable tensions using a tensiometer. (See Notes 16 & 18.)..................................................................................................................... O 27. Inspect stabilator trim mechanism, stabilator trim cables, turnbuckles, guides, and pulleys for safety, damage, and operation. (See Note 16.) ........................................ O 28. Lubricate per lubrication chart, 12-20-00 ..................................................................................... O O 29. Inspect anti-collision light for security and operation .................................................................. O O 30. Inspect security of Autopilot bridle cable clamps. (See Note 16.) ............................................... O 31. Inspect all control cables, air ducts, electrical leads, lines, radio antenna leads, and attaching parts for security, routing, chafing, deterioration, wear, and correct installation. (See Note 16.)......................................................................................... O 32. Inspect ELT battery for condition/date per FAR 91.207............................................................... O 33. Inspect ELT installation and antenna for condition and security. Replace antenna if bent or damaged ............................................................................................. O 34. Install inspection plates and panels............................................................................................... O 5. SCHEDULED MAINTENANCE - SARATOGA II HP (S/N’s 3246001 & up) (CONTINUED) Refer to Notes 1, 2, 3, and 4 before performing the following inspections. Inspection Interval (Hrs) NATURE OF INSPECTION 50 100 THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL 5-20-00 Page 5-20 Revised: February 16, 2004 1C12 E. WING GROUP 1. Remove inspection plates and fairings ......................................................................................... O 2. Inspect surfaces and tips for damage, loose rivets, and conditions of walkway........................... O 3. Inspect aileron hinges and attachments. (See Note 34.) ............................................................... O 4. Inspect aileron control stops to ensure stops have not loosened and locknuts are tight ............... O 5. Inspect aileron cables, pulleys, and bellcranks for damage and operation, and cable tensions. (See Note 16.)................................................................................................ O 6. Inspect pitot tube for damage and condition................................................................................. O — CAUTION — SEVERE BURNS CAN RESULT FROM COMING IN CONTACT WITH A HEATED PITOT TUBE. 7. Check pitot heat ............................................................................................................................ O 8. Inspect flaps and attachments for damage and operation ............................................................. O 9. Inspect condition of bolts used with hinges. Replace as required ................................................ O 10. Lubricate per lubrication chart, 12-20-00 ..................................................................................... O O 11. Inspect wing attachment bolts and brackets. (See Note 19.) ........................................................ O 12. Inspect fuel tanks and lines for leaks and water. (See Note 20.) .................................................. O 13. Inspect fuel tanks for minimum octane markings......................................................................... O 14. Inspect fuel cell vents ................................................................................................................... O 15. Inspect all control cables, air ducts, electrical leads, lines, and attaching parts for security, routing, chafing, deterioration, wear, and correct installation. (See Note 16.) ......... O 16. Install inspection plates and fairings............................................................................................. O F. LANDING GEAR GROUP 1. Check oleo struts for proper extension and evidence of fluid leakage. See Landing Gear, 12-10-00 ......................................................................................................... O O 2. Inspect nose gear steering control and travel ................................................................................ O 3. Inspect wheel alignment ............................................................................................................... O 4. Put airplane on jacks. (Refer to Chapter 7.).................................................................................. O 5. Inspect tires for cuts, uneven or excessive wear, and slippage ..................................................... O 6. Remove wheels, clean, inspect, and repack bearings ................................................................... O 7. Inspect wheels for cracks, corrosion, and broken bolts ................................................................ O 8. Check tire pressure........................................................................................................................ O O 9. Inspect brake lining and disc for wear .......................................................................................... O 10. Inspect brake backing plates for cracks ........................................................................................ O 11. Inspect condition of brake and hydraulic lines ............................................................................. O 12. Inspect shimmy dampener operation ............................................................................................ O 5. SCHEDULED MAINTENANCE - SARATOGA II HP (S/N’s 3246001 & up) (CONTINUED) Refer to Notes 1, 2, 3, and 4 before performing the following inspections. Inspection Interval (Hrs) NATURE OF INSPECTION 50 100 THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL 5-20-00 Page 5-21 Revised: February 16, 2004 1C13 F. LANDING GEAR GROUP (cont.) 13. Inspect gear forks for damage....................................................................................................... O 14. Inspect oleo struts for fluid leaks and scoring .............................................................................. O 15. Inspect gear struts, attachments, torque links, retraction links, and bolts for condition and security ............................................................................................................. O 16. Inspect down lock for operation and adjustment .......................................................................... O 17. Inspect torque link bolts and bushings. Rebush as required. ........................................................ O 18. Inspect drag and side brace link bolts. Replace as required. ........................................................ O 19. Inspect gear doors and attachments .............................................................................................. O 20. Inspect warning horn and light for operation................................................................................ O 21. Check normal-emergency gear retraction operation..................................................................... O 22. Retract gear-inspect doors for clearance and operation................................................................ O 23. Inspect anti-retraction system ....................................................................................................... O 24. Inspect actuating cylinders for leaks and security. (See Note 31.) ............................................... O 25. Inspect all hydraulic lines, electrical leads, and attaching parts for security, routing, chafing, deterioration, wear, and correct installation .................................. O 26. Inspect position indicator switch and electrical leads for security ............................................... O 27. Lubricate per lubrication chart, 12-20-00 ..................................................................................... O O 28. Ensure that landing gear is down and locked; remove airplane from jacks.................................. O G. SPECIAL INSPECTIONS See 5-30-00 ................................................................................................................................... O O 5. SCHEDULED MAINTENANCE - SARATOGA II HP (S/N’s 3246001 & up) (CONTINUED) Refer to Notes 1, 2, 3, and 4 before performing the following inspections. Inspection Interval (Hrs) NATURE OF INSPECTION 50 100 THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL 5-20-00 Page 5-22 Revised: February 16, 2004 1C14 H. OPERATIONAL INSPECTION — Note — Refer to Note 22 prior to starting engine or taxiing airplane. 1. Check fuel pump and fuel tank selector........................................................................................ O O 2. Check fuel quantity, pressure, and flow readings ......................................................................... O O 3. Check oil pressure and temperature.............................................................................................. O O 4. Check alternator output................................................................................................................. O O 5. Check manifold pressure .............................................................................................................. O O 6. Check alternate air ........................................................................................................................ O O 7. Check parking brake ..................................................................................................................... O O 8. Check vacuum gauge .................................................................................................................... O O 9. Check gyros for noise and roughness ........................................................................................... O O 10. Check cabin heater operation........................................................................................................ O O 11. Check magneto switch operation.................................................................................................. O O 12. Check magneto rpm variation....................................................................................................... O O 13. Check throttle and mixture operation ........................................................................................... O O 14. Check propeller smoothness ......................................................................................................... O O 15. Check propeller governor action................................................................................................... O O 16. Check engine idle.......................................................................................................................... O O 17. Check annunciator light panel ...................................................................................................... O O 18. Check electronic equipment operation ......................................................................................... O O 19. If installed, check operation of autopilot, including automatic pitch trim, and manual electric trim. (See Note 23.) ...................................................................................... O O 20. Check air conditioner compressor clutch operation ..................................................................... O O 21. Check air conditioner condenser scoop operation ........................................................................ O O 22. Fly airplane, check Landing Gear System. (See Note 24.)........................................................... O O I. GENERAL 1. Aircraft conforms to FAA Specification....................................................................................... O O 2. All latest revisions of Airworthiness Directives complied with.................................................... O O 3. All latest revisions of Manufacturers’ Service Bulletins and Letters complied with.................... O O 4. Check for proper Pilot’s Operating Handbook ............................................................................. O O 5. Aircraft papers in proper order ..................................................................................................... O O 5. SCHEDULED MAINTENANCE - SARATOGA II HP (S/N’s 3246001 & up) (CONTINUED) Refer to Notes 1, 2, 3, and 4 before performing the following inspections. Inspection Interval (Hrs) NATURE OF INSPECTION 50 100 THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL 5-20-00 Page 5-23 Revised: February 16, 2004 1C15 5. SCHEDULED MAINTENANCE - SARATOGA II HP (S/N’s 3246001 & up) (CONTINUED) J. NOTES 1. Refer to Piper's Customer Service Information Aerofiche P/N 1753-755 for latest revision dates to Piper Inspection Reports/Manuals and this maintenance manual. References to Chapter/Section are to the appropriate Chapter or Section in this manual. — 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. 2. Inspections or operations are to be performed as indicated by a “O” at the 50 or 100 hour inspection interval. Inspections or operations (i.e. - component overhauls/replacements, etc.) required outside the 100 hour cycle are listed as special inspections in section 5-30-00. Inspections must be accomplished by persons authorized by the FAA. (a) The 50 hour inspection accomplishes preventive maintenance, lubrication and servicing as well as inspecting critical components. (b) The 100 hour inspection is a complete inspection of the airplane, identical to an annual inspection. — Note — A log book entry should be made upon completion of any inspections. 3. Piper Service Bulletins are of special importance and Piper considers compliance mandatory. In all cases, see Service Bulletin/Service Letter Index P/N 762-332 or Service Bulletin/Service Letter Aerofiche Set P/N 1762-331 to verify latest revision. 4. Piper Service Letters are product improvements and service hints pertaining to servicing the airplane and should be given careful attention. 5. Inspections given for the power plant are based on the engine manufacturer’s operator’s manual ( Textron Lycoming Part No. 60297-10 ) for this airplane. Any changes issued to the engine manufacturer’s operator’s manual shall supersede or supplement the inspections outlined in this report. 6. Overhaul as required and at engine overhaul. In no case may Slick 6300 series magneto's time-in- service exceed engine TBO. 7. Refer to latest revision of Textron Lycoming Service Bulletin No. 480. THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL 5-20-00 Page 5-24 Revised: February 16, 2004 1C16 5. SCHEDULED MAINTENANCE - SARATOGA II HP (S/N’s 3246001 & up) (CONTINUED) J. NOTES (cont.) 8. Not used. 9. Check cylinders for evidence of excessive heat indicated by burned paint on the cylinders. This condition is indicative of internal damage to the cylinder and, if found, its cause must be determined and corrected before the airplane is returned to service. Heavy discoloration and appearance of seepage at the cylinder head and barrel attachment area is usually due to emission of thread lubricant used during assembly of the barrel at the factory, or by slight gas leakage which stops after the cylinder has been in service for a while. This condition is neither harmful nor detrimental to engine performance and operation. If it can be proven that leakage exceeds these conditions, the cylinder must be replaced. 10. Not used. 11. Replace at engine overhaul or 5 years, whichever comes first. For engine overhaul, refer to latest revision of Textron Lycoming Service Bulletin No. 240 and Textron Lycoming Service Instruction 1009. 12. Complete vacuum system inspection of airplanes equipped with the Auxiliary Vacuum Pump/ Motor Assembly (4A3-1), requires gaining access under the floorboard on the right side of the forward baggage compartment, where this assembly is located. 13. Not used. — CAUTION — ENVIRONMENTAL REGULATIONS MAY REQUIRE SPECIAL EQUIPMENT AND PROCEDURES BE USED WHEN CHARGING AIR CONDITIONING SYSTEMS. 14. The compressor oil level should not be checked unless a refrigerant leak has occurred or system pressure has been released, requiring an addition of refrigerant to the system. 15. Clean any traces of oil from the clutch surface. 16. Examine cables for broken strands by wiping them with a cloth for their entire length. Visually inspect the cable thoroughly for damage not detected by the cloth. Replace any damaged or frayed cables. See Control Cable Inspection, 27-00-00, or the latest edition of FAA AC 43.13-1. 17. Not used. 18. Maintain cable tensions specified in Chapter 27. 19. Check torque at forward and aft spar attach per Chapter 57, Figure 57-1. 20. Sloshing of fuel tanks not approved. 21. Not used. 22. Refer to Section 4 of the Pilot's Operating Handbook for preflight and flight check list. 23. Refer to Pilot's Operating Handbook Supplement for preflight and flight check and for intended function in all modes. 5. SCHEDULED MAINTENANCE - SARATOGA II HP (S/N’s 3246001 & up) (CONTINUED) J. NOTES (cont.) THE NEW PIPER AIRCRAFT, INC. PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUAL 5-20-00 Page 5-25 Revised: February 16, 2004 1C17 24. Fly airplane to check landing gear system in accordance with instructions given in Chapter 32, Operational Check of Retractable Landing Gear System. 25. Not used. 26. In S/N’s 3246001 thru 3246070 only, ensure the requirements of Piper Service Bulletin No. 1005 (latest revision) have been complied with and an appropriate maintenance log entry was made. 27. Not used. 28. In S/N’s 3246001 thru 3246087 only, ensure the requirements of Piper Service Bulletin No. 1015 (latest revision) have been complied with and an appropriate maintenance log entry was made. 29. In S/N’s 3246001 thru 3246144 only, ensure the requirements of Piper Service Bulletin No. 1020 (latest revision) have been complied with and an appropriate maintenance log entry was made. 30. In S/N’s 3246001 thru 3246117 only, ensure the requirements of Airworthiness Directive No. 99-05-09 (see also Piper Service Bulletin No. 1022 (latest revision)) have been complied with and an appropriate maintenance log entry was made. 31. In S/N’s 3246001 thru 3246115 only, ensure the requirements of Piper Service Bulletin No. 1023 (latest revision) have been complied with and an appropriate maintenance log entry was made. 32. In S/N’s 3246001 thru 3246112 only, ensure the requirements of Piper Service Bulletin No. 1024 (latest revision) have been complied with and an appropriate maintenance log entry was made. 33. In S/N’s 3246001 thru 3246120 only, ensure the requirements of Piper Service Bulletin No. 1026 (latest revision) have been complied with and an appropriate maintenance log entry was made. 34. In S/N’s 3246102 thru 3246121 only, ensure the requirements of Piper Service Bulletin No. 1028 (latest revision) have been complied with and an appropriate maintenanc

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