PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL

The Piper PA-32R-301 Saratoga II hP / PA-32R-301T Saratoga II 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). 2. 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 PARTS oR PIPeR 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 ensure 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. Piper Aircraft, Inc. expressly disclaims any responsibility for malfunctions, failures, damage or injury caused by use of non-PIPeR approved parts. noTe: 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. Also, Piper Aircraft, Inc. may possess manufacturer’s data which defines minimum type design beyond what may be assumed by an authorized repair entity. When a repair is proposed, it is the responsibility of the repairer per AC 43.13-1 to determine that the proposed repair is not contrary to manufacturer’s data. The repairer or aircraft owner or his agent should contact Piper directly to determine that a proposed repair is not in conflict with minimum type design capability. If you have any question concerning the care of your airplane, be sure to include the airplane serial number in any correspondence to Piper. INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL PAGE 2 Jul 31/13 1A10INTRODUCTION 3. effectivity This maintenance manual is effective for PA-32R-301 Saratoga II hP airplane serial numbers 3246001 and up, and PA-32R-301T Saratoga II TC airplane serial numbers 3257001 and up. This encompasses the model years shown in Chart 1. 4. Serial number explanation example: 32 46 001 SeQUenCe nUMBeR MoDeL CoDe 46 = PA-32R-301 SARAToGA II hP 57 = PA-32R-301T SARAToGA II TC TyPe CeRTIFICATe DeSIGnATIon 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 thru 3246226 2005 3246227 thru 3246232 2006 3246233 thru 3246244 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 thru 3257369 2005 3257370 thru 3257400 2006 3257401 thru 3257439 2007 3257440 thru 3257477 2008 3257478 thru 3257493 CHART 1 MODEL YEARS noTe: The above is provided as a general reference only. INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL PAGE 3 Jul 31/13 1A11 INTRODUCTION 5. Assignment of Subject Material This publication is divided into industry standard, three element, numeric subject groupings as follows: A. System/Chapter - The various groups are broken down into major systems such as environmental Systems, electrical Power, Landing Gear, etc. They are assigned a number, which becomes the first element of the standardized numbering system. Thus, the element “28” of the number 28-40-01 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. 6. Pagination The Chapter - Section (i.e. - 28-40-00) numbering system (explained above) forms the primary page numbering system for this manual. Within each Section, pages are numbered consecutively beginning with Page 1 (i.e. - 28-40-00, Page 1). Additionally, a modified legacy Aerofiche grid numbering system (explained below) will be used to indicate location within the manual until the next complete revision. 7. Aerofiche Grid numbering Piper has ceased production of all Aerofiche (i.e., microfiche) products. The Aerofiche grid numbers will be removed in the next complete revision. In the interim, as partial revisions occur, the Aerofiche grid numbering system may be modified, as explained below, to simplify production. Deviations from the legacy Aerofiche grid numbering system will occur when it becomes necessary to add pages to the manual and will typically take two forms: A. Inserting pages between two existing grids in the same row. When inserting two pages between the existing grids 1A8 and 1A9, the two new pages will be numbered 1A8A and 1A8B. B. Inserting pages at the end of an Aerofiche grid row. The legacy Aerofiche grid numbering system limited page numbers in a row to a maximum of 24 (i.e., row 1A would be numbered 1A1–1A24). That limit no longer applies. Accordingly, if two pages need to be added between any existing grid row end and grid row start (i.e., 1A24 and 1B1), the new pages will simply be numbered 1A25 and 1A26. INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL PAGE 4 Jul 31/13 1A12INTRODUCTION 8. Identifying Revised Material A vertical line (i. e. - change bar) along the left-hand margin of the page (or text column) is used to identify revised text or illustrations. example. 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. Change bars in the individual chapter Tables of Contents do not indicate a change to that page, but rather that the information in the actual paragraph has changed. noTe: Change bars are not used in the title pages, list of effective pages, or the Index. Likewise, when a publication is completely revised (i.e. - reissued), change bars will only appear in the Tables of Contents. A. 2007 thru 2011 A revision to a page was defined as any change to the printed matter that existed previously. Revisions, additions and deletions are identified by a change bar opposite only that portion of the printed matter that was changed. B. 2012 and up A revision to a page is defined as a change to the text or illustrations that existed previously. Revisions, additions and deletions are identified by a change bar opposite only the text or illustration that was changed. Reformatted, but otherwise unchanged, text (i.e., paragraph numbering, etc.) is not identified by a change bar. 9. Indexing An alphabetically arranged subject Index follows this introduction to assist the user in locating desired information. In addition, each System/Chapter begins with an individual Table of Contents. 10. List of effective Pages each System/Chapter has a List of effective Pages preceding the Table of Contents to identify the effective revision date for each page in that chapter. 11. 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. 12. 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. INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL PAGE 5 Jul 31/13 1A13 INTRODUCTION 13. Supplementary Publications The following publications/sources provide servicing, overhaul and parts information for the PA-32R-301 / PA-32R-301T airplanes and their various components. Use them to supplement this manual. A. Piper Publications: Part number (1) Parts Catalog 761-880 (2) Progressive Inspection Manuals (50 hour): SARAToGA II hP (S/n’s 3246001 & up) 767-016 SARAToGA II TC (S/n’s 3257001 & up) 767-015 (3) Periodic Inspection Report Forms: SARAToGA II hP (S/n’s 3246001 & up) 230-1047 SARAToGA II TC (S/n’s 3257001 & up) 230-2047 B. Vendor Publications: WARnInG: FAILURe To ConSULT APPLICABLe VenDoR PUBLICATIon(S), When SeRVICInG oR InSPeCTInG VenDoR eQUIPMenT InSTALLeD In PIPeR AIRCRAFT, MAy RenDeR The AIRCRAFT UnAIRWoRThy. (1) AIR ConDITIonInG CoMPReSSoR: Vendor: Climate Control Inc. (or) Sanden International (USA), Inc. 2120 n. 22nd Street 601 South Sanden Blvd. Decatur, Illinois 62526 Wylie, Tx 75098-4999 (217) 422-0055 (972) 442-8400 http://www.ccicompressor.com http://www.sanden.com (2) ALTeRnAToR: Vendor: hartzell engine Technologies Ph: (877) 359-5355 2900 Selma highway (334) 386-5400 Montgomery, Alabama 36108 FAx: (334) 386-5410 http://www.hartzellenginetech.com/ overhaul Manual: Manual oe-A2 (3) 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 (4) BATTeRy: Vendor: Gill/Teledyne Battery Products Ph: (800) 456-0070 840 W. Brockton Ave. Redlands, California 92374 http://www.gillbatteries.com/ INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL PAGE 6 Jul 31/13 1A14INTRODUCTION (5) 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 (6) eLeCTRonIC FLIGhT InSTRUMenT SySTeM (eFIS) 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 Multifunction Display: Document no. AVMFD-167 Data Acquisition Unit: Document no. AVSIU-011 or, Vendor: Garmin International Ph: (913) 397-8200 1200 east 151ST Street olathe, KS 66062 http://www.garmin.com (7) eMeRGenCy LoCAToR TRAnSMITTeR: Vendor: Artex Aircraft Supplies Ph: (800) 547-8901 14405 Keil Road ne Aurora, oregon 97002 http://www.artex.net/ (8) eMeRGenCy BATTeRy: Vendor: Concorde Battery Corporation Ph: (626) 813-1234 2009 San Bernardino Road FAx: (626) 813-1235 West Covina, CA 91790 http://www.concordebattery.com/ Instructions for Continued Airworthiness: Component Maintenance Manual: Document no. 5-0167 INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL PAGE 7 Jul 31/13 1A15 INTRODUCTION (9) enGIne: Vendor: Lycoming engines Ph: (717) 323-6181 652 oliver Street FAx: (717) 327-7101 Williamsport, Pennsylvania 17701 http://www.lycoming.com/ 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-315-10 operators handbook: o-540, Io-540 SeRIeS - P/n 60297-10 TIo-540 Series - P/n 60297-23 (10) enGIne FUeL ConTRoL SySTeMS: Vendor: Precision Airmotive LLC Ph: (360) 651-8282 14800 40th Ave ne FAx: (360) 651-8080 Marysville, WA 98271 http://www.precisionairmotive.com/ (11) 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 (12) 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 (13) GeAR LoCKInG ACTUAToRS, noSe GeAR DooR ACTUAToR, hyDRAULIC PUMP, AnD ALL hyDRAULIC CoMPonenTS: Vendor: Parker hannifin Corp. (See Brakes, above) (14) hI-LoK FASTeneRS AnD TooLS: Vendor: hi-Shear Corporation Ph: (213) 326-8110 2600 Skypark Drive Torrance, California 90509 (15) InADVeRTenT ICe PRoTeCTIon SySTeM (TKS): Vendor: Aerospace Systems and Technologies, Inc. 3213 Arnold Ave. Ph: (785) 493-0946 Salina, Kansas 67401 FAx: (785) 493-0950 http://www.weepingwings.com/ INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL PAGE 8 Jul 31/13 1A16INTRODUCTION (16) 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/ (17) MAGneToS: Vendor: Slick Aircraft Products Ph: (904) 772-1909 Champion Aerospace P.o. Box 686 1230 old norris Road Liberty, SC 29657 http://www.championaerospace.com/ Installation, operation F1100 MASTeR SeRVICe MAnUAL, and Maintenance 4300/6300 SeRIeS MAGneTo Instructions: MAInTenAnCe AnD oVeRhAUL MAnUAL - L-1363 (18) 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 (19) oxyGen SySTeM: (SARAToGA II TC onLy) Vendor: Avox Systems Ph: (716) 683-5100 2225 erie Street Lancaster, new york 14086 http://www.avoxsystems.com/ (20) PRoPeLLeR: Vendor: hartzell Propeller Inc. Ph: (937) 778-4379 one Propeller Place FAx: (937) 778-4321 Piqua, oh 45356-2634 http://www.hartzellprop.com/index2.htm 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 (21) PRoPeLLeR GoVeRnoR: Vendor: hartzell Propeller Inc. Ph: (937) 778-4379 one Propeller Place FAx: (937) 778-4321 Piqua, oh 45356-2634 http://www.hartzellprop.com/index2.htm Governor Maintenance: Manual no. 130B INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL PAGE 9 Mar 21/12 1A17 INTRODUCTION (22) 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 (23) STARTeR: Vendor: See listing under (or) Sky-Tec Alternator, above. 350 howard Clemmons Rd Granbury, Texas 76048 Ph - (800) 476-7896 FAx - (817) 573-2252 http://www.skytecair.com (24) VACUUM PUMPS: Vendor: Aero Accessories, Inc. Ph: (800) 822-3200 1240 Springwood Avenue Gibsonville, nC 27249 http://www.aeroaccessories.com/index.html (25) 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 INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL PAGE 10 Jun 30/07 1A18INTRODUCTION THIS PAGE INTENTIONALLY BLANK INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL PAGE 11 Jan 31/08 1A19 INTRODUCTION 14. Chapter/Section Index Guide noTe: The following GAMA Specification no. 2 standard chapters are not included in this Maintenance Manual: 36, 38, 49, 54, 60, 72, 75 and 83. These chapters are omitted because the subject system is either: not installed in these airplanes; adequately covered in vendor or other manuals; or, for ease of use, has been combined with another chapter. CHAPTER SECTION TITLE GRID NO. 4 AIRWoRThIneSS LIMITATIonS 1C1 00 Airworthiness Limitations 5 TIMe LIMITS/MAInTenAnCe CheCKS 1C9 00 General 10 Time Limits 20 Scheduled Maintenance 30 Special Inspections 50 Unscheduled Maintenance Checks 6 DIMenSIonS AnD AReAS 1F1 00 General 7 LIFTInG AnD ShoRInG 1F17 10 Jacking 8 LeVeLInG AnD WeIGhInG 1G1 10 Weighing 20 Leveling 9 ToWInG AnD TAxIInG 1G11 10 Towing 20 Taxiing 10 PARKInG AnD MooRInG 1G21 10 Parking 20 Mooring 11 PLACARDS AnD MARKInGS 1h7 20 exterior Placards and Markings 30 Interior Placards 12 SeRVICInG 1I5 00 General 10 Replenishing 20 Scheduled Servicing INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL PAGE 12 Jan 31/08 1A20INTRODUCTION CHAPTER SECTION TITLE GRID NO. 20 STAnDARD PRACTICeS - AIRFRAMe 2C1 00 General 20 Painting 21 enVIRonMenTAL SySTeMS 2D3 00 General 20 Distribution 40 heating 50 Cooling 22 AUToFLIGhT 2G5 10 Autopilot 23 CoMMUnICATIonS 2h9 00 General 50 Audio Integrating 60 Static Discharging 24 eLeCTRICAL PoWeR 2I3 00 General 30 DC Generation 40 external Power 60 electrical Load Distribution 25 eQUIPMenT/FURnIShInGS 3C1 10 Flight Compartment 20 Passenger Compartment 60 emergency 26 FIRe PRoTeCTIon 3D11 20 extinguishing 27 FLIGhT ConTRoLS 3D21 00 General 10 Aileron and Tab 20 Rudder and Tab 30 Stabilator and Tab 50 Flaps 28 FUeL 3h3 00 General 10 Storage 20 Distribution 40 Indicating INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL PAGE 13 Jan 31/08 1A21 INTRODUCTION CHAPTER SECTION TITLE GRID NO. 29 hyDRAULIC PoWeR 3J5 00 General 10 Main 30 ICe AnD RAIn PRoTeCTIon 4C1 00 General 10 Airfoil 30 Pitot and Static 60 Propeller 31 InDICATInG / ReCoRDInG SySTeMS 4e11 50 Central Warning Systems 32 LAnDInG GeAR 4F9 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 4J9 00 General 10 Flight Compartment 40 exterior 34 nAVIGATIon 5C1 00 General 10 Flight environment Data 20 Attitude and Direction 50 Dependent Position Determining 35 oxyGen 6C1 10 Crew/Passenger 37 VACUUM 6D5 00 General 10 Distribution 20 Indicating INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL PAGE 14 Jan 31/08 1A22INTRODUCTION CHAPTER SECTION TITLE GRID NO. 39 eLeCTRICAL/eLeCTRonIC PAneLS 6e5 10 Instrument and Control Panels 51 STRUCTUReS 6F19 00 General 10 Investigation, Cleanup and Aerodynamic Smoothness 70 Repairs 80 electrical Bonding 52 DooRS 6h11 00 General 10 Passenger/Crew 30 Cargo 53 FUSeLAGe 6I7 20 Main 55 STABILIZeRS 6I17 20 Stabilator 30 Vertical Stabilizer 40 Rudder 56 WInDoWS 6J15 10 Flight Compartment 20 Passenger Compartment 57 WInGS 7C1 00 General 20 Auxiliary Structure 40 Attach Fittings 50 Flight Surfaces 61 PRoPeLLeRS 7D5 10 Propeller Assembly 20 Controlling 70 STAnDARD PRACTICeS - enGIne 7e1 00 General INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL PAGE 15 Jun 30/07 1A23 INTRODUCTION CHAPTER SECTION TITLE GRID NO. 71 PoWeR PLAnT 7e9 00 General 10 Cowling 20 Mounts 73 enGIne FUeL AnD ConTRoL 7F11 10 Distribution 20 Controlling 74 IGnITIon 7G7 10 electrical Power Supply 20 Distribution 30 Switching 76 enGIne ConTRoLS 7h21 10 Power Control 77 enGIne InDICATInG 7I7 00 General 10 Power 20 Temperature 40 Integrated engine Instrument Systems 78 exhAUST 7J21 00 General 79 oIL 7K7 20 Distribution 30 Indicating 80 STARTInG 8C1 10 Cranking 81 TURBIneS 8C21 20 Turbo-Supercharger 91 ChARTS & WIRInG DIAGRAMS 8e1 10 Charts 21 & Up Wiring Diagrams (Schematics) INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL PAGE 16 Jun 30/07 1A24INTRODUCTION THIS PAGE INTENTIONALLY BLANK INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL PAGE 1 Jul 31/13 1B1 INDEX A Access Plates and Panels: 1F13 Accident/Incident Reporting: 1A12 Aerofiche Grid Code: 1A11 Aileron Balancing: 7C26 Checking Free Play: 7C23 Control System Installation: 3e21 Troubleshooting: 3e14 Installation: 7C24 Tab: 3F3 Air Conditioning Charging Stand hookup: 2e21 Kent Moore J23500: 2e17 RoBInAIR 34700 hookup: 2e23 Compressor Belt Installation: 2F12 Sanden: 2F11 Magnetic Clutch: 2F16 york: 2F9 Magnetic Clutch: 2F18 Condenser Air Scoop Installation: 2F21 evacuation hookup: 2F4 Installation: 2e8 Leak Test: 2F3 Service Valves: 2e9 Test Gauge and Manifold Set: 2F1, 2F2 Torque Specifications: 2e15 Troubleshooting: 2e3 Air Filter Servicing: 1J5 Airworthiness Directives (AD’s): 1C15 Instructions for Continued Airworthiness: 1A9 Limitations: 1C7 Annunciator Description: 4e17 Troubleshooting: 4e18, 4e24 Artex eLT 110-4: 3C19 Inspections: 3C20 Testing: 3C22 Artex Me406 eLT: 3D3 Inspections: 3D2 Testing: 3D6 Troubleshooting: 3D1 Autopilot - See System 55/55x Avidyne entegra eFIS Component Locator: 5D7 Description: 5D3 Instrument Panel: 5D3 Magnetic heading System Calibration: 5I11 Magnetometer: 5I13 Wiring harness: 5D10 Avionics Installation: 2h18 Rack-Mounted: 6e11 B Balancing equipment: 6J4, 6J12 Ball Diameters for Testing hose Restrictions: 2C10 Battery - See electrical Brakes Bleeding: 4I21 Parking Brake: 1h3 Servicing: 1I24 System Installation: 4I17 Leak Check: 4I20 Toe Brake Cylinder: 4I20 Toe Brake Installation: 4I19 Wheel Brake Assembly: 4I13 C Cabin heat: 2D17 Ventilation: 2D11, 2D17 Chapter/Section Index Guide: 1A19 Cherrylock Rivet Removal: 2C9 Circuit Breaker Panel: 6e12 Cleaning: 1I12 Aircraft Finish Care: 1I11 Consumable Materials: 8e23 Control Column Assembly: 3e15 Control Wheel Installation: 3e19 Conversion Tables Decimal: 8e17 Drill Sizes: 8e21 Metric: 8e20 Temperature: 8e18 Weights and Measures: 8e19 Corrosion Control: 6G5 Forms: 6G5 D Definitions Inspections: 1C19 Defrosters: 2D17 Deicing Fluid: 4C7 Doors Baggage Door Lock Tool: 6I5 Cabin: 6h23 Upper Door Latch - Adjustment: 6h24, 6I2 Description: 6h17 Snubber Seals: 6h17 Installation: 6h18 E eFIS - See Avidyne or Garmin eGT Gauge: 7I21 electrical Battery: 2J8 Servicing: 1J2 Bonding: 6h3 Millivolt Drop Test: 6h4 Resistance Index: 6h4 Bonding Straps: 2h23 electrical System Alternator: 2I12 Belt Tension Adjustment: 2I23 Troubleshooting: 2I14 Component Loads: 2J21 Description and operation: 2I9 Load Distribution: 2J21 Standby Alternator: 2J1 Installation: 2J7 Troubleshooting: 2J3 emergency Battery: 2J11 emergency Starting: 2J19 external Power: 2J17 on-Aircraft Checks: 2I20 Schematics #1 GnS nAV/CoM/GPS: 9e24 #2 GnS nAV/CoM/GPS: 9F2 ADF: 9F6 Air Conditioning: 8F19 Alternator Power: 8h1 Ammeter: 8h9 Annunciator: 8J1 Attitude Gyro: 9D22 INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL PAGE 2 Jul 31/13 1B2INDEX electrical (cont.) Schematics (cont.) Audio Panel GMA 340: 8G18 GMA 1347: 8G20 Autopilot: 8G1 Auxiliary Vacuum System: 9F10 Avionics Cooling: 8F17 Lighting: 8F17 Baggage Door Ajar: 9D3 Cabin Temp: 9G6 ChT: 9F19, 9G1, 9G5 Clock, hour Meter, and Baggage Light: 9C21 Configuration Module: 9G6 Courtesy / Reading Lights: 9C16 Data Acquisition Unit: 9F24 DDMP: 9F20 eGT: 9G2, 9G3 electric Flaps: 8I7 eLT: 8I3 engine Digital Display Monitoring Panel: 9F20 engine Gauge: 9F22 entertainment Console: 9C20 exceedance Audio Alert: 8I17 external Power: 8h21 Flood Lights: 9D4 Fresh Air Blower: 8F15 Fuel Flow: 9G2, 9G3, 9G4, 9G11 Fuel Pump: 8I11 Fuel Quantity: 8I13 GDC 74A ADC: 9e7 GDL 69 Data Link: 8I23 GDU 1040: 9e5 GeA 71 engine/Airframe Unit: 9G7 GIA 63W IAU: 9e8 Ground Clearance: 8G9 GRS 77 AhRS: 9e6 Kn-63 DMe: 9e19 Landing Gear Control: 8J13 Landing Gear Position and Warning: 8J15 Landing / Taxi Lights: 9D7 Low Voltage Monitor: 8h9 Magneto Switch: 9F13 MAP: 9F16, 9F17, 9G6 Multi-Function Display (MFD) Avidyne: 9e3 Garmin G1000: 9e5 navigation and Strobe Lights: 9D12 oAT Probe: 9D19 oil Pressure: 9G9, 9G11 oil Temperature: 9G9, 9G11 overhead Speakers: 8G17 Panel and Switch Lights: 9C9 Pitot heat: 8I21 Power Point: 8I1 Primary Flight Display (PFD) Avidyne: 9e2 Garmin G1000: 9e5 Radio Lights: 9C15 Radio Master Switch: 8G13 Recognition Lights: 9D16 RPM: 9F15, 9F17, 9G11 Skywatch: 9e11, 9e13 Stall Warning: 8I5 Standby Alternator: 8h10 Standby Attitude Indicator: 9D24 Starter and Accessories: 9G13 Stormscope: 9e14 TIT: 9G2, 9G4, 9G5 TKS System: 8I19 Transponder GTx-33: 9e18 GTx-330: 9e17 Turn and Bank Indicator: 9D21 VAC: 9F19 Vacuum Inop: 9F9 Static Wicks: 2h23 Symbols: 8F12, 8F13, 8F14 System Servicing: 1J6 Voltage Regulator: 2J11 Wire Coding: 8F9 electrical/electronic Components Alphabetical Index: 6e17 Locator Illustration: 6e17 eLT. See Artex Model empennage Group: 6J2 engine ChT Probe: 7I23 Description: 7e15 exhaust System - See exhaust System Fuel Air Bleed nozzles: 7F21 Injection System: 7F19 Ignition - See Ignition System Installation: 7e20, 7F8 Instruments Analog Instruments: 7J7 Single / Dual Instrument: 7J7 Cylinder head Temperature Gauge: 7I22 Description: 7I13 eGT Gauge - See eGT Gauge engine Instruments & DDMP: 7J3 Alarm Conditions: 7J9 electrical Mode: 7J10 exceedance Condition: 7J9 exceedance Mode: 7J11 Failure Condition: 7J9 Fuel Mode: 7J13 Instrument Mode: 7J10 Integrated engine Instrumentation Calibration: 7J16 Percent Power: 7J12 Temperature Mode: 7J13 Manifold Pressure Gauge - See MAP Gauge oil Pressure: 7K15 oil Temperature: 7K17 Manifold Pressure Transducer: 7I17 Manifold Pressure vs oil Temperature: 7F24 Mixture Control Adjustment: 7I3 Mount Corrosion Inspection: 7F9 Shock Mounts: 7F6 Serial number Location: 1F7 Standard Practices: 7e7 Starter Bench Tests: 8C12 Description: 8C7 exploded View: 8C8 Troubleshooting: 8C7 INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL PAGE 3 Jul 31/13 1B3 INDEX Tachometer Magnetic Sensor: 7I19 Throttle Control Adjustment: 7I3 Timing Marks: 7G15 Troubleshooting: 7e15 Turbine Inlet Temperature: 7I23 Turbocharger Description: 8D3 Installation: 8D9 nomenclature: 8D6 Troubleshooting: 8D4 Wastegate Adjustment: 8D11 Installation: 8D11 exhaust System 100 hour Inspection: 7K3 Inspection Points: 7K4 extinguishing Portable Fire extinguisher: 3D17 Description: 3D17 Inspection: 3D17 F Fiberglass Repairs - See Repairs - Fiberglass Flaps Control System Installation: 3G19 Rigging and Adjustment: 3G20 Troubleshooting: 3G17 Inspection Flap Torque Tube/Pushrod Distortion Inspection: 3G23 Installation: 7C24 Flareless Tube Fittings: 2C12 Flight Controls: 3e3 Control Cable Inspection: 3e8 Description and operation: 3e3 Flight Control Cable Tension: 3e5 Flight Control Surface Travel: 3e5 Pulleys: 3e11 Standard Practices and Procedures: 3e4 Flight Control Surfaces Rigging Limits: 3e6 Flight Instruments - See also eFIS Airspeed Indicator: 5C22 Altimeter: 5C21 Attitude Indicator: 5D1 Directional Gyro: 5I8 Magnetic Compass: 5I23 Standby Attitude Indicator: 5D2 Turn and Bank Indicator: 5J1 Vertical Speed Indicator: 5C19 Fluid Line Identification: 2C10 Fluid Tubing Support: 2C13 Fuel System: 3h12 Cleaning: 3I7 electric Fuel Pump: 3I12 Fuel Cells - outboard: 3h20 Inspection: 3h20 Installation: 3h22 Removal: 3h20 Repair: 3h23 Testing: 3I3 Fuel Selector Valve and Filter Assembly: 3I8 Installation: 3I8 Removal: 3I8 Fuel Sight-Gauge: 3J1 Fuel System Leakage Inspection: 3I9 Fuel Tanks - Inboard: 3h15 Fuel Tank / Wing Spar Corrosion Inspection: 3h18 Installation: 3h16 Removal: 3h15 Repair: 3h18 Indicating: 3I13 Inspection: 3h15 Locking Fuel Cap: 3I4 Troubleshooting: 3h12 Fuel Tanks: 1I20 Draining Moisture: 1I20 Filling: 1I20 G Garmin G1000 IAS Alerts and Annunciations: 5D20 Calibration GRS 77/GMU 44: 5h14 Magnetic: 5I17 Components: 5e5 Configuration Mode overview: 5F16 Description: 5D12 Displays: 5D12 Inspections: 5e2 Lighting Setup: 5I1 Cockpit: 5I4 Magnetic heading System Calibration: 5I17 Post-Installation Setup: 5F16 Required equipment List: 5J2 Shield Block Installation: 5F15 Spider Grounds: 5F14 System Communications: 5D13 engine / Airframe Interface: 5D16 Flight Instrumentation Interface: 5D15 hierarchy: 5G8 navigation / Communications Interface: 5D17 Testing AhRS / ADC Backup Path: 5h24 Aircraft Interface: 5h6 Display Failure: 5h24 emergency Power: 5h16 engine / Airframe: 5h14 GIA 63W: 5h10 GIA Failure: 5h23 GMA 1347: 5h9 GPS Failure: 5h23 GRS 77/GMU 44: 5h13 GTx 33: 5h11 Initial Display: 5h2 optional Systems: 5h19 S-TeC 55x Interface: 5h16 Wiring harness: 5F24 Troubleshooting: 5D18 engine / Airframe SensorFailures: 5D23 GDC 74A: 5F5 GDL 69/69A: 5F11 GDU 1040: 5e6 GeA 71: 5e23 GIA 63W: 5e14 GMA 1347: 5e12 GMU 44: 5F9 GRS 77: 5F7 GTx 33: 5F1 LRU Failures: 5D21 Software Load / Configuration: 5G7 INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL PAGE 4 Jul 31/13 1B4INDEX GMA-340 Adjustment: 2h19 Audio Panel: 2h17 Functional Test: 2h17 Removal and Installation: 2h17 GnS 430/530 Post Installation Setup: 5J6 GTx-330 Post Installation Setup: 5J12 H heated Pitot-Static Mast: 4C7, 4e1 hose Specifications: 8e22 hose, Tube, and Line Markings: 2C11 hydraulic System Installation: 3J14 Pump: 3J18 Servicing: 1J2 Schematic Diagram: 3J12 Servicing: 3J21 Testing: 3J21 I Ice Protection: 4C5 Ignition System Description: 7G13 Ignition harness: 7h9 harness Cap: 7h13 Stripping Tool: 7h10 Magnetos: 7G14 100 hour Inspection: 7G14 500 hour Inspection and Cleaning: 7G17 Bearing Bar: 7h4 Bearings: 7h1 Carbon Brush Assembly: 7G20 Coil Wedge: 7h1 exploded View: 7G22 Impulse Coupling Pawl Clearance: 7G18 Pawls: 7G18 Internal Timing: 7h4 oil Seal: 7h1 Rotor and Stop Pin: 7G17 Rotor Gear: 7h4 Testing: 7h6 Timing to engine: 7G14 Timing Tool Kit: 7G21 Troubleshooting: 7G14 Spark Plugs: 7h14 Coupling Torque: 7h16 Inspection And Cleaning: 7h15 Inadvertent Ice Protection System - See TKS Inspection. See also System Chapter/Section Definitions: 1C19 Procedures 100 hour Standby Alternator: 2J2 Aft Wing Attach Fitting 100 hour: 6I13 Aileron nose Rib Assembly 100 hour: 7C27 Alternate Air Door: 1J5 Artex eLT 110-4: 3C20 Artext Me406 eLT: 3D2 Control Cable: 3e8 Dye Penetrant: 2C14 electrical Bonding: 6h3 engine Mount 100 hour: 7F5 Corrosion, Immersion in Water: 7F9 exhaust System 100 hour: 7K3 Fire extinguisher, Portable: 3D17 Flap Torque Tube/Pushrod Distortion Inspection: 3G23 Flexible hoses: 2C10 Fuel Cells outboard (Bladder-type): 3h20 Fuel Pump, electric: 3I12 Fuel System: 3h15 Leakage: 3I9 Fuel Tank / Wing Spar Corrosion: 3h18 Garmin G1000 eFIS 1000 hour: 5e4 Annual / 100 hour: 5e2 Magnetos 100 hour: 7G14 500 hour: 7G17 nylon Tubing Couplings: 2C15 oxygen System: 6C10 Propeller: 1J6 Spark Plugs: 7h15 Stabilator Control System Special: 3e12 Wing Aft Attach Fitting: 7C19 Wing Rib Assembly W.S. 49.25 100 hour: 7C9 500 hour: 7C9 Requirements: 1C21 Annual / 100 hour Inspection: 1C21 Procedure: 1C22 overlimits Inspection: 1C21 Per event Flaps extended Above Maximum Flap extension Speed: 1e17 Flood Damage: 1e18 hard or overweight Landing: 1e16 Lightning Strike: 1e15 Severe Turbulence: 1e16 Progressive Inspection: 1C21 Special: 1e5 Unscheduled: 1e15 Instruments Face-Mounted: 6e11 Introduction: 1A5 J Jacking: 1F23 L Landing Gear Description: 4F17 emergency Release: 4I5 extension and Retraction Functional Test: 4h23 Troubleshooting: 4h17 Limit Switches: 4J1 Main Actuating Cylinder: 4I5 Adjustment: 4G11 Aligning: 4G13 Door: 4G15 Installation: 4G8 oleo Strut: 4G4 Toe-In and Toe-out Correction: 4G14 Tolerances: 4G16 INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL PAGE 5 Jul 31/13 1B5 INDEX nose Actuating Cylinder: 4I4 Adjustment: 4h6 Alignment: 4h6 Doors: 4h8 Installation: 4h2 oleo Strut: 4G22 Tolerances: 4h10 Servicing: 1I22 Tire Balance: 1J6 Troubleshooting: 4F19 Warning: 4J4 operational Check: 4J5 Leveling Airplane: 1G9 Life Limited Parts: 1C17 Lights exterior Landing Lights: 4J19 navigation Lights: 4K3 Recognition Lights: 4K3 Strobe Light: 4K4 Interior Annunciator Lamp Replacement: 4J17 Dimmer Control: 4J17 Locking Airplane: 1h3 Lubrication Application of Grease: 1J10 Application of oil: 1J10 Charts: 1J10 Air Conditioning: 1K4 Baggage Doors: 1K3 Cabin Doors: 1K3 Control System: 1J18 Fuel Selector: 1K2 Main Landing Gear: 1J14 nose Landing Gear: 1J16 Power Plant: 1J24 Propeller: 1J24 Seats: 1K3 M Magnetic heading Systems: 5I9 Magnetos - See Ignition System MAP Gauge: 7I15 Markings - See Placards Mooring: 1h5 Muffler - See exhaust System N nylon Tubing Coupling: 2C14 O oil System: 1J8 oil Sump: 1I21 olive Clenching: 2C15 outside Air Temperature: 5C23 oxygen System Cylinder: 6C7, 6C11, 6C17, 6C18 Description: 6C7 Inspection: 6C10 Installation: 6C8 on/off Control: 6C7, 6C23 outlets: 6C7, 6C10, 6C11, 6C22 Pressure Gauge: 6C7, 6C10, 6C11, 6C21 Recharge Valve: 6C7, 6C11, 6C19, 6C20 Regulator Valve: 6C7, 6C11, 6C18 Swageloc Fittings: 6C15 Troubleshooting: 6C9 Tubing Installation: 6C13 P Painting: 2C21 Parking: 1h3 Parking Brake: 1h3 Piper Publications: 1A13 Pitot heat: 4C7, 4e1 Pitot/Static System Description: 5C13 Installation: 5C14 Placards exterior: 1h15 Interior: 1h20 entertainment Console: 1I3 Instrument Panel: 1h22 Propeller Governor Control Arm: 7D19 Installation: 7D12 Torque Limits: 7D11 Typical nicks and Removal Methods: 7D14 Propeller Deicing: 4e5 Propeller Governor: 7D20 Adjustment: 7D19 Publications Piper: 1A13 Vendor: 1A13 R Repairs Fiberglass: 6G13 Impacted Damage: 6G22 Metal / Wire Stitching: 6G23 Stress Lines: 6G21 Thermoplastic: 6G15 Cracks: 6G19 Deep Scratches: 6G16 epoxy Patching Compound: 6G17 List of Materials: 6G18 Surface Scratches: 6G16 Welding Repair: 6G17 Various: 6G20 Restraint System: 3C10 Revisions Aerofiche Revision Status: 1A3 Identifying Revised Material: 1A12 Rod end Bearing Installation: 2C8 Rudder Control System Installation: 3F11 Rigging and Adjustment: 3F13 Troubleshooting: 3F9 Rudder Balancing: 6J12 Trim Control System Installation: 3F15 Rigging and Adjustment: 3F16 S Safety Walk Installation: 6G23 Seats Seat Back Lock: 3C7 Serial number effectivity: 1A10 explanation: 1A10 Location: 1F7 Service Points: 1I19 Skin Material Specifications: 6G2 Spark Plugs - See Ignition System Stabilator: 6J5 Attach Brackets: 6J7 Control System Installation: 3G2 Rigging and Adjustment: 3G4 Troubleshooting: 3F23 Stabilator Balancing: 6J6 Stabilator Trim Tab: 6J5 INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL PAGE 6 Jul 31/13 1B6INDEX Stabilator (cont.) Trim Control System Installation: 3G8 Rigging and Adjustment: 3G12 Stall Strips - See TKS: 4C9 Stall Warning System: 3G13 Functional Tests: 3G13 Standard Practices Airframe: 2C5 Station Reference Lines: 1F12 Steering Pedal Assembly: 3F17 Structures Description: 6G1 Switches overhead Panel: 6e13 Push on/oFF: 6e14 Radio Master: 2h15 Rocker-Type: 6e13 System 55/55x: 2G11 Flap Compensator: 2h6 GPSS: 2G15 Pitch Servo: 2h1 Pressure Transducer: 2G18 Roll Servo: 2G20 Servo Clutch Torque Adjustment: 2h4 Trim Monitor: 2G18 Trim Servo: 2G22 Troubleshooting: 2G15 T Taxiing: 1G19 Testing A/C Leaks: 2F3 Artex eLT 110-4: 3C22 Artex Me406 eLT: 3D6 Garmin 1000 eFIS: 5h2 GMA-340 Functional Test: 2h17 hydraulic System: 3J21 Magnetos: 7h6 Stall Warning System: 3G13 Thermoplastic Repairs - See Repairs - Thermoplastic Three View: 1F7 Tires Servicing: 1J1 TKS: 4C9 Drain Valve: 1J3 electrical Schematic: 4D21 Fluid Quantity Sender: 4D9 Fluid Tank: 4D7 Fluid Tank Strainer: 4D8 Porous Panel: 4C17 Finishing with Sealant: 4C24 Installation: 4C21 Stall Strips: 4D1 Propeller Boot: 4e8 Propeller Installation: 4e7 Propeller Slinger Ring: 4e6 Proportioning Unit Port Usage: 4D14 Pump and Drain Valve: 4D5 System Servicing: 1J2 Test Apparatus: 4C14 Troubleshooting: 4C10 Torque Conversion: 8e16 Torque Wrench Formula: 2C8 Towing: 1G17 Troubleshooting Aileron Control System: 3e14 Air Conditioning System: 2e3 Airspeed Indicator: 5C22 Alternator System: 2I15 Altimeter: 5C21 Annunciator: 4e18, 4e24 Artex Me406 eLT: 3D1 Attitude Indicator: 5D1 Directional Gyro: 5I8 engine: 7e16 engine Instrument & DDMP: 7J2 exhaust Gas Temperature Gauge: 7I21 extension and Retraction: 4h17 Flap Control System: 3G17 Garmin 1000 eFIS: 5D18 Inadvertent Ice Protection System (TKS): 4C11 Landing Gear: 4F19 Magnetic Compass: 5I24 Manifold Pressure Gauge: 7I15 oil Pressure Gauge: 7K15 oil Temperature Indicator: 7K17 oxygen System: 6C9 RSA Fuel Injection System: 7F17 Rudder Control System: 3F9 Stabilator Control System: 3F23 Standby Alternator Regulator: 2J3 Starter: 8C9 Strobe Lights: 4K4 Tachometer: 7I16 TKS Fault Isolation: 4C11 TKS Tubing: 4D20 Turbocharger: 8D4 Turbocharger - See engine, Turbocharger Turn and Bank Indicator: 5J1 Vacuum System: 6D12 Vertical Speed Indicator: 5C19 V Vacuum System Description: 6D11 Filter: 6D15 Gauge: 6D15, 6e1 Inspection: 6D16 Pump: 6D16 Pump Fittings: 6D17 Regulator: 6D18 Service: 6D18, 6e1 Switch: 6e2 Troubleshooting: 6D12 Vendor Contact Information: 8F7 Publications: 1A13 Vertical Stabilizer: 6J9 W Weeping Wings - See TKS Weighing Airplane: 1G7 Wheels Balancer: 1J7 Main Assembly: 4I10A nose Assembly: 4I9 Windows Storm Window: 6J23 Windows and Windshields Windows: 6K1 Installation: 6K1 Windshield: 6J21 Defrost: 2D17 Installation: 6J22 Wing Description: 7C7 Installation: 7C16, 7C21 Tip: 7C13 INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL PAGE 7 Jun 30/07 1B7 INDEX THIS PAGE INTENTIONALLY BLANK INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL PAGE Mar 21/12 1B8INDEX PAGE 8 Jun 30/07 GRIDS 1B8 THRU 1B24 INTENTIONALLY BLANK INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL 1C1 CHAPTER 4AIRWORTHINESS LIMITATIONS INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL 1C2 THIS PAGE INTENTIONALLY BLANK INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL PAGE 1 Mar 21/124 - LIST OF EFFECTIVE PAGES1C3 CHAPTER 4 LIST OF EFFECTIVE PAGES CHAPTER SECTION PAGE DATE 4-List of 1 Mar 21/12 effective Pages 2 Jun 30/07 4-Table of Contents 1 Mar 21/12 2 Jun 30/07 4-00-00 1 Mar 21/12 2 Jun 30/07 CHAPTER SECTION PAGE DATE INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL PAGE 2 Jun 30/07 4 - LIST OF EFFECTIVE PAGES 1C4 THIS PAGE INTENTIONALLY BLANK INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL PAGE 1 Mar 21/12 1C5 4 - CONTENTS CHAPTER 4 - AIRWORTHINESS LIMITATIONS TABLE OF CONTENTS SUBJECT SECTION PAGE GRID NO. AIRWoRThIneSS LIMITATIonS 4-00-00 1 1C7 Approved Mandatory Replacement Times for Type Certification 1 1C7 Approved Mandatory Structural Inspection Intervals 1 1C7 Inspection Procedures for those Approved Mandatory Structural Inspection Items 1 1C7 INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL PAGE 2 Jun 30/07 1C64 - CONTENTS THIS PAGE INTENTIONALLY BLANK INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL PAGE 1 Mar 21/12 1C7 4-00-00 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. Approved Mandatory Replacement Times for Type Certification (PIR-TCDS-A3So, Rev. 32.) 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. Approved Mandatory Structural Inspection Intervals none. 3. Inspection Procedures for those Approved Mandatory Structural Inspection Items none. INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL PAGE 2 Jun 30/07 1C84-00-00 THIS PAGE INTENTIONALLY BLANK INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL 1C9 CHAPTER 5TIME LIMITS / MAINTENANCE CHECKS INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL 1C10 THIS PAGE INTENTIONALLY BLANK INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL PAGE 1 Jul 31/135 - LIST OF EFFECTIVE PAGES1C11 CHAPTER 5 LIST OF EFFECTIVE PAGES CHAPTER SECTION PAGE DATE 5-List of 1 Jul 31/13 effective Pages 2 Jun 30/07 5-Table of Contents 1 Jul 31/13 2 Jul 31/13 5-00-00 1 Jul 31/13 2 Jun 30/07 5-10-00 1 Jul 31/13 2 Jun 30/07 5-20-00 1 Mar 21/12 2 Dec 31/09 3 Mar 21/12 4 Mar 21/12 5 Jun 30/07 6 Jun 30/07 7 Mar 21/12 8 Jul 31/13 9 Jul 31/13 10 Jul 31/13 11 Jul 31/13 12 Mar 21/12 13 Mar 21/12 14 Mar 21/12 15 Jul 31/13 16 Jul 31/13 17 Jul 31/13 18 Jul 31/13 19 Jul 31/13 20 Jun 30/07 21 Mar 21/12 22 Jul 31/13 23 Jul 31/13 24 Jul 31/13 25 Jul 31/13 26 Jul 31/13 27 Mar 21/12 28 Mar 21/12 29 Jul 31/13 30 Jul 31/13 CHAPTER SECTION PAGE DATE 5-20-00 (cont.) 31 Jul 31/13 32 Jul 31/13 33 Jul 31/13 34 Jun 30/07 5-30-00 1 Jul 31/13 2 Jul 31/13 3 Jul 31/13 4 Jul 31/13 5 Jul 31/13 6 Jul 31/13 7 Jul 31/13 8 Jul 31/13 9 Jul 31/13 10 Jul 31/13 5-50-00 1 Jan 31/08 2 Jan 31/08 3 Jan 31/08 4 Jan 31/08 5 Jan 31/08 6 Jun 30/07 7 Jun 30/07 8 Jun 30/07 9 Jun 30/07 10 Jun 30/07 INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL PAGE 2 Jun 30/07 5 - LIST OF EFFECTIVE PAGES 1C12 THIS PAGE INTENTIONALLY BLANK INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL PAGE 1 Jul 31/13 1C13 5 - CONTENTS GeneRAL 5-00-00 1 1 C 1 5 TIMe LIMITS 5-10-00 1 1C17 General 1 1C17 Life Limited Parts Marking and Disposition 1 1C17 SCheDULeD MAInTenAnCe 5-20-00 1 1C19 Description 1 1C19 Definitions 1 1C19 Inspection Requirements 3 1C21 Annual / 100 hour Inspection 3 1C21 Progressive Inspection 3 1C21 overlimits Inspection 3 1C21 Annual / 100 hour Inspection Procedure 4 1C22 Scheduled Maintenance 4 1C22 Special Inspections (see 5-30-00) 4 1C22 Unscheduled Maintenance (see 5-50-00) 4 1C22 Scheduled Maintenance - Saratoga II hP (S/n’s 3246001 & up) 7 1D1 Propeller Group 7 1D1 engine Group 7 1D1 Cabin and Cockpit Group 9 1D3 Fuselage and empennage Group 10 1D4 Wing Group 11 1D5 Landing Gear Group 12 1D6 Special Inspections 13 1D7 operational Inspection 13 1D7 General 14 1D8 notes 14 1D8 Service Publications List - Saratoga II hP 17 1D11 Scheduled Maintenance - Saratoga II TC (S/n’s 3257001 & up) 21 1D15 Propeller Group 21 1D15 engine Group 21 1D15 Turbocharger Group 23 1D17 Cabin And Cockpit Group 23 1D17 Fuselage And empennage Group 24 1D18 Wing Group 26 1D20 Landing Gear Group 27 1D21 Special Inspections 27 1D21 operational Inspection 27 1D21 General 28 1D22 notes 28 1D22 Service Publications List - Saratoga II TC 31 1e1 CHAPTER 5 - TIME LIMITS / MAINTENANCE CHECKS TABLE OF CONTENTS SUBJECT SECTION PAGE GRID NO. INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL PAGE 2 Jul 31/13 1C145 - CONTENTS SPeCIAL InSPeCTIonS 5-30-00 1 1e5 Per Flight hour 1 1e5 each 200 hours 1 1e5 each 400 hours 1 1e5 each 500 hours 1 1e5 each 1000 hours 2 1e6 each 1500 hours 2 1e6 each 2000 hours 2 1e6 each 2400 hours 3 1e7 each 2700 hours 3 1e7 Per Calendar year 3 1e7 each Thirty (30) Days 3 1e7 each ninety (90) Days 4 1e8 each Four (4) Months 4 1e8 each Six (6) Months 4 1e8 each Twelve (12) Months 4 1e8 each Two (2) years 5 1e9 each Three (3) years 5 1e9 each Five (5) years 5 1e9 each Six (6) years 6 1e10 each Seven (7) years 6 1e10 each eight (8) years 6 1e10 each Ten (10) years 7 1e11 each Twelve (12) years 7 1e11 each Fifteen (15) years 7 1e11 each Twenty (20) years 7 1e11 Specific operation / operating environment 8 1e12 high Dust or Industrial Pollution 8 1e12 high Salt or high humidity 9 1e13 operation in extreme Cold 9 1e13 operation from Soft or Unusual Terrain 10 1e14 At engine overhaul 10 1e14 UnSCheDULeD MAInTenAnCe CheCKS 5-50-00 1 1e15 Lightning Strike 1 1e15 overspeed, overtemp, Loss of oil, or Sudden Stoppage 2 1e16 Severe Turbulence, hard or overweight Landing 2 1e16 Flaps extended Above Maximum Flap extension Speed (Vfe) 3 1e17 Flood Damage, Immersion in Water 4 1e18 CHAPTER 5 - TIME LIMITS / MAINTENANCE CHECKS TABLE OF CONTENTS (continued) SUBJECT SECTION PAGE GRID NO. INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL PAGE 1 Jul 31/13 1C15 5-00-00 GeneRAL 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 schedule for the PA-32R-301/301T Saratoga II hP / TC is provided in 5-20-00. B. Piper Service Bulletins are of special importance and Piper considers compliance mandatory. C. Service Letters deal with product improvements and service hints pertaining to the affected aircraft. owners should give careful attention to service letter information so they can ensure their airplane is properly serviced and kept up to date with the latest changes. D. Service Spares Letters offer improved parts, kits and optional equipment which were not originally available. These may be of interest to the owner. e. Service Bulletins, Service Letters and Service Spares Letters are emailed to Piper Dealers/Service Centers. owners are encouraged to download these service publications from http://www.piper.com/. noTe: Piper mails flight manual (AFM / Poh) 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 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 flight manual revisions during this interim period through their Piper Dealer/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 their 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 www.faa.gov. owners should periodically check with a Piper Dealer/Service Center to find out the latest information to keep his aircraft up to date. Service Bulletins, Service Letters, and Service Spares Letters are also available by subscription. See the availability statement in Revision Status. INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL PAGE 2 Jun 30/07 1C165-00-00 THIS PAGE INTENTIONALLY BLANK INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL PAGE 1 Jul 31/13 1C17 5-10-00 TIMe LIMITS 1. General A. 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. B. Refer to 5-20-00 for Piper’s recommended Inspection Programs. They include the frequency and extent of the inspections required for the continued airworthiness of these airplanes. C. 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. 2. 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. As stated in 4-00-00, there are no life limited parts defined by Type Certificate (TC). other parts which are replaced or rebuilt after having accumulated cycles, hours, or other replacement limit are specified in 5-20-00 or 5-30-00. A. Parts that are removed prior to accumulating their life limit, are to be marked with indelible ink or marker with the part number, serial number and accumulated life status as defined in 14 CFR Part 43.10 in a manner that does not affect part structural integrity, i.e. - no surface deformation such as vibration/etching allowed. B. Parts that have accumulated the life limit shall be disposed of in accordance with the applicable FARs. Piper recommends life limited parts with no time and/or cycles remaining be completely destroyed. INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL PAGE 2 Jun 30/07 1C185-10-00 THIS PAGE INTENTIONALLY BLANK INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL 1C195-20-00 PAGE 1 Mar 21/12 SCheDULeD MAInTenAnCe This section provides instructions for conducting inspections. Repair or replacement instructions for those components found to be unserviceable during inspections will be found in the applicable airplane system chapter. (See Chapter/Section Index Guide, Introduction.) WARnInG: GRoUnD The MAGneTo PRIMARy CIRCUIT (P LeAD), BeFoRe PeRFoRMInG Any MAInTenAnCe oPeRATIon on The 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 the PA-32R-301T Saratoga II TC are provided herein as Annual / 100 hour Inspections. Progressive Inspection Programs are available in a separate manual form. See the availability statement in Revision Status. Piper inspection programs comply with the F.A.A. 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 accomplished only by persons authorized by the FAA or appropriate national Aviation Authority who are qualified on these 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. (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. INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL PAGE Mar 21/12 1C205-20-00 PAGE 2 Dec 31/09 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 test 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.) 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.” INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL 1C215-20-00 PAGE 3 Mar 21/12 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. Inspections must be accomplished by persons authorized by the FAA or appropriate national Aviation Authority. 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. B. Progressive Inspection. The Progressive Inspection program is designed to permit the best utilization of the aircraft through the use of a planned inspection schedule. These schedules: P/n 767-016 for the Saratoga II hP (S/n’s 3246001 & up), and P/n 767-015 for the Saratoga II TC (S/n’s 3257001 & up). are prepared in manual form. See the availability statement in Revision Status. Refer to Piper’s Customer Service Information File P/n 1761-755 for a checklist to ensure obtaining latest issue. noTe: The 50 hour Progressive Inspection Manuals (P/n 767-015 and 767-016) referenced above are not stand-alone documents. They constitute a snapshot of the Airworthiness Limitations and Inspection sections of the Instructions for Continued Airworthiness (ICA) and are 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 and applicable vendor publications. INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL 1C225-20-00 PAGE 4 Mar 21/12 4. Annual / 100 hour Inspection Procedure A. Scheduled Maintenance (i.e. - paragraphs 5 and 6). 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. (1) The required periodic inspection procedures are listed in paragraph 5 (PA-32R-301), and 6 (PA-32R-301T). These inspection procedures are broken down into major groups which include Propeller, engine, Turbocharger (where applicable), Cabin and Cockpit, Fuselage and empennage, Wing, Landing Gear, Special Inspections, 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 interval of 50 hours or 100 hours. each inspection or operation is required at each of the inspection intervals indicated by a circle (o). When a vendor publication specifies a time outside the 50 / 100 hour cycle, it will be listed as a special inspection in 5-30-00. (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: 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). are available. See the availability statement in Revision Status. noTe: Service centers conducting Part 91 Annual / 100 hour Inspections can use the appropriate Inspection Report Form (above), as a working check-off list, provided they verify its 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. - paragraph 5 or 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.) INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL PAGE Mar 21/12 1C235-20-00 PAGE 5 Jun 30/07 THIS PAGE INTENTIONALLY BLANK INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL PAGE Mar 21/12 1C245-20-00 PAGE 6 Jun 30/07 THIS PAGE INTENTIONALLY BLANK INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL 1D15-20-00 5. Scheduled Maintenance - Saratoga II HP (S/N’s 3246001 & up) (continued) Inspection NATURE OF INSPECTION Interval (Hrs) 50 100 PAGE 7 Mar 21/12 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 NATURE OF INSPECTION Interval (Hrs) 50 100 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, 12-20-00 . . . . . . . . . . . . . . . . . . . . . . . o 5. Inspect spinner mounting brackets for cracks and security. . . . . . . . . . . . . . . . . . o 6. Inspect propeller mounting bolts for condition and security. If safety is broken, re-torque and safety . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 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 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 cowling and inspect for internal and external damage . . . . . . . . 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 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 fittings 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 cowling or in Lubrication Chart, 12-20-00 . o o CAUTIon: USe CAUTIon noT To ConTAMInATe VACUUM PUMP WITh CLeAnInG FLUID. 10. Clean engine with approved solvents . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL 5. Scheduled Maintenance - Saratoga II HP (S/N’s 3246001 & up) (continued) 1D25-20-00 Inspection NATURE OF INSPECTION Interval (Hrs) 50 100 PAGE 8 Jul 31/13 B. ENGINE GROUP (CONT.) 11. Inspect condition of spark plugs. Clean and adjust gap as required; adjust per latest revision 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 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. Inspect magnetos for oil seal leakage . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 18. Inspect magnetos to engine timing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 19. Remove air filter and clean per 12-20-00. Replace as required . . . . . . . . . . . . . . o o 20. Clean fuel injector inlet line screen . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o o 21. Inspect condition of alternate air valve and housing . . . . . . . . . . . . . . . . . . . . . . . o o 22. Inspect intake seals for leaks and clamps for tightness. (Torque clamps 40–50 in.-lbs.) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o o 23. Inspect all air inlet duct hoses. Replace as required . . . . . . . . . . . . . . . . . . . . . . . o o 24. Inspect condition of flexible fuel lines . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 25. Inspect fuel system for leaks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 26. Inspect engine-driven and electric fuel pumps for condition and operation. Replace as required . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 27. If installed, inspect and operationally test engine driven and auxiliary vacuum pumps and lines. (See notes 10, 11, and 20.). . . . . . . . . . . . . . . . . . . . . o 28. Inspect throttle, alternate air, mixture, and propeller governor controls for security, travel, and operation condition . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 29. Inspect exhaust stacks, connections and gaskets. Replace gaskets as required. (See 100 hour Inspection, 78-00-00.). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o o 30. Inspect muffler, heat exchange, and baffles. (See 100 hour Inspection, 78-00-00.). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o o 31. Inspect breather tube for obstructions and security . . . . . . . . . . . . . . . . . . . . . . . o 32. Inspect crankcase for cracks, leaks, and security of seam bolts. . . . . . . . . . . . . . o 33. Inspect engine mounts for cracks and loose mounting. (See note 22.) . . . . . . . . o 34. Inspect all engine baffles. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 35. Inspect rubber engine mount bushings for deterioration. (Replace as required.) . o 36. Inspect firewall seals . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 37. Inspect condition and tension of alternator drive belt. (Refer to 24-30-00; or 21-50-00, if air conditioning is installed.) . . . . . . . . . . . . . . o o 38. 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 39. Inspect condition of alternator and starter. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 40. Inspect security of alternator and mounting . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 41. If installed, inspect Standby Alternator per 100 hour Standby Alternator Inspection, 24-30-00 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 42. If installed, inspect air conditioning compressor oil level. (See note 12.) . . . . . . . o INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL 1D35-20-00 5. Scheduled Maintenance - Saratoga II HP (S/N’s 3246001 & up) (continued) Inspection NATURE OF INSPECTION Interval (Hrs) 50 100 PAGE 9 Jul 31/13 B. ENGINE GROUP (CONT.) 43. If installed, inspect condition of compressor belt and tension. (Refer to 21-50-00.). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o o 44. If installed, inspect compressor clutch security and wiring. (See note 13.) . . . . . o 45. If installed, inspect compressor mounting for cracks, corrosion, and security . . . o 46. Check fluid in brake reservoir. Fill as required. . . . . . . . . . . . . . . . . . . . . . . . . . . . o o 47. If installed, perform Inadvertent Ice Protection System (TKS) 50 hour Inspection, 30-10-00 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o o 48. Inspect condition and security of all controls. . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 49. Lubricate per Lubrication Chart, 12-20-00 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o o 50. Install engine cowling . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o o C. CABIN AND COCKPIT GROUP 1. Inspect cabin doors and windows for damage, operation and security. . . . . . . . . o 2. Inspect windows for scratches, crazing and condition. . . . . . . . . . . . . . . . . . . . . . o 3. Inspect window and door seals for deterioration, cracks and voids. (Refer to Chapter 56.) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 4. Inspect upholstery for tears. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 5. Inspect seats and attaching brackets and hardware for condition, security and operation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 6. Inspect seat belts and shoulder harnesses per 25-10-00, Restraint System . . . . o 7. Inspect trim operation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 8. Inspect rudder pedals . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 9. Inspect parking brake valve and brake handle for operation and cylinder leaks . . o 10. Inspect control wheels, column, pulleys, cables, turnbuckles, and fittings for condition, security, and full travel. Inspect cables per Control Cable Inspection, 27-00-00. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 11. Cycle each circuit breaker with airplane power off . . . . . . . . . . . . . . . . . . . . . . . . o o 12. Check landing, navigation, strobe, cabin, and instrument lights . . . . . . . . . . . . . . o o 13. Inspect instruments, lines, and attachments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 14. Inspect gyro operated instruments (if installed), and electric turn and bank. (overhaul or replace as required.) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 15. If installed, replace vacuum regulator filter element . . . . . . . . . . . . . . . . . . . . . . . o 16. Inspect static system, altimeter (and ADAhRS (in Avidyne PFD), if installed) and transponder for installation/certification per latest revision of AC43.13-1 and current test/inspection per FAR’s 91.411 and 91.413, respectively . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 17. Inspect operation of fuel selector valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 18. Inspect fuel valve drain lever cover for security. Check that door opens and closes freely and prevents operation of lever when closed . . . . . . . . . . . . . . . . . . o o 19. Inspect condition of heater controls and ducts . . . . . . . . . . . . . . . . . . . . . . . . . . . o 20. Inspect condition and operation of air vents . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 21. Inspect condition of air conditioning ducts . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 22. If installed, remove and clean air conditioning evaporator filter. . . . . . . . . . . . . . . o 23. If installed, inspect portable fire extinguisher minimum weight as specified on nameplate . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL 5. Scheduled Maintenance - Saratoga II HP (S/N’s 3246001 & up) (continued) 1D45-20-00 Inspection NATURE OF INSPECTION Interval (Hrs) 50 100 PAGE 10 Jul 31/13 D. FUSELAGE AND EMPENNAGE GROUP 1. Remove inspection plates and panels. (See Figure 3, 6-00-00.) . . . . . . . . . . . . . o 2. Inspect aft wing attach fittings for corrosion per Aft Wing Attach Fittings 100 hour Inspection, 53-20-00 . . . . . . . . . . . . . . . . . . . . . . . . . . . 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 24-30-00 . . . . o 5. Conduct a general visual inspection of electrical and electronic installations (mounting, wiring, harnesses, shields, connectors, etc.) for condition and security . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 6. Inspect skins, bulkheads, frames, and stringers for damage, irregularities, or structural defects (i.e. - skin cracks, distortion, dents, corrosion, and loose or missing rivets) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 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. If installed, inspect air conditioning system for refrigerant leaks. (See note 12.) . o 11. If installed, inspect refrigerant level in sight gauge of receiver-dehydrator. (Refer to 21-50-00.). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o o 12. If installed, inspect air conditioner condenser air scoop for condition and rigging. (See note 19.). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 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. Flush selector valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 15. Inspect security of all lines . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 16. Inspect electric flap screw jack and attachments for condition and lubrication . . . o 17. Inspect vertical fin for surface damage or irregularities (i.e. - skin cracks, distortion, dents, and corrosion); structural defects (i.e. - loose or missing rivets); and attachment points for missing or worn hardware . . . . . . . . . . . . . . . . o 18. Inspect vertical fin attachments for security . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 19. Inspect rudder for surface damage or irregularities (i.e. - skin cracks, distortion, dents, and corrosion); structural defects (i.e. - loose or missing rivets); misrigging; hinge damage, excessive wear, freedom of movement and proper lubrication; and attachment points for missing or worn hardware . . . . . . . . . . . . . o 20. Inspect rudder hinges, sector and attachments for damage, security and proper operation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 21. Inspect rudder hinge bolts for excessive wear. Replace as required. . . . . . . . . . . o 22. Inspect rudder control stops to ensure stops have not loosened and locknuts are tight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 23. Inspect stabilator and tab for surface damage or irregularities (i.e. - skin cracks, distortion, dents, and corrosion); structural defects (i.e. - loose or missing rivets); misrigging; hinge damage, excessive wear, freedom of movement and proper lubrication; and attachment points for missing or worn hardware . . . . . . . o 24. Inspect stabilator tab hinges, horn, and attachments for damage, security, and operation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 25. Inspect stabilator attachments and attach brackets per Stabilator Attach Brackets Corrosion Inspection, 55-20-00. . . . . . . . . . . . . . . . . . . . . . . . . . o INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL 1D55-20-00 5. Scheduled Maintenance - Saratoga II HP (S/N’s 3246001 & up) (continued) Inspection NATURE OF INSPECTION Interval (Hrs) 50 100 PAGE 11 Jul 31/13 D. FUSELAGE AND EMPENNAGE GROUP (CONT.) 26. Inspect stabilator control stops to ensure stops are not loose. ensure bolts and locknuts are tight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 27. Inspect stabilator trim mechanism for safety, damage, and operation . . . . . . . . . o 28. Inspect rudder, stabilator, and stabilator trim cable tensions per 27-00-00, Chart 2. Use a tensiometer. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 29. Inspect aileron, rudder, stabilator, and stabilator trim cables; and cable terminals, turnbuckles, guides, fittings, and pulleys for safety, condition, and operation per Control Cable Inspection, 27-00-00. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 30. Lubricate per Lubrication Chart, 12-20-00 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o o 31. Inspect anti-collision light for security and operation. . . . . . . . . . . . . . . . . . . . . . . o o 32. If installed, inspect security of Autopilot bridle cables and clamps. Inspect condition of cables per Control Cable Inspection, 27-00-00 . . . . . . . . . . . . . . . . . o 33. Inspect air ducts, electrical leads, lines, radio antenna leads, and attaching parts for security, routing, chafing, deterioration, wear, and correct installation. Perform 100 hour Inspection, 51-80-00 . . . . . . . . . . . . . . . . . o 34. Inspect eLT battery mount for condition and security . . . . . . . . . . . . . . . . . . . . . . o 35. Inspect eLT antenna for condition, security, and operation (check operation per Antenna Test in 25-60-00). Replace antenna if bent or damaged . . . . . . . . . . . . . o 36. Install inspection plates and panels . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 37. Inspect static wicks per Static Wicks, Inspection, 23-60-00. (Replace as required.). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o E. WING GROUP 1. Remove inspection plates and fairings. (See Figure 3, 6-00-00.) . . . . . . . . . . . . . o 2. Inspect surfaces and tips for damage, loose rivets, and condition of walkway. (See note 21.). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 3. Inspect ailerons for surface damage or irregularities (i.e. - skin cracks, distortion, dents, and corrosion); structural defects (i.e. - loose or missing rivets); misrigging; hinge damage, excessive wear, freedom of movement and proper lubrication; and attachment points for missing or worn hardware. (See note 8.) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 4. Inspect aileron hinges and attachments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 5. Inspect aileron control stops to ensure stops have not loosened and locknuts are tight. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 6. Inspect aileron cables and cable terminals, turnbuckles, fittings, guides, pulleys, and bellcranks for safety, condition, and operation per Control Cable Inspection, 27-00-00 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 7. Inspect aileron cable tension per 27-00-00, Chart 2. Use a tensiometer . . . . . . . o 8. Inspect pitot tube for damage and condition . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o CAUTIon: SeVeRe BURnS CAn ReSULT FRoM CoMInG In ConTACT WITh A heATeD PIToT TUBe. 9. Check pitot heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 10. Inspect flaps for surface damage or irregularities (i.e. - skin cracks, distortion, dents, and corrosion); structural defects (i.e. - loose or missing rivets); misrigging; hinge damage, excessive wear, freedom of movement and proper lubrication; and attachment points for missing or worn hardware . . . . . . . . . . . . . o INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL 5. Scheduled Maintenance - Saratoga II HP (S/N’s 3246001 & up) (continued) 1D65-20-00 Inspection NATURE OF INSPECTION Interval (Hrs) 50 100 PAGE 12 Mar 21/12 E. WING GROUP (CONT.) 11. Inspect condition of flap hinge bolts. Replace as required . . . . . . . . . . . . . . . . . . o 12. Lubricate per Lubrication Chart, 12-20-00 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o o 13. Inspect wing attachment bolts and brackets for security and condition. (See note 14.). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 14. Inspect fuel tanks and lines for leaks and water. (See note 15.). . . . . . . . . . . . . . o 15. Inspect fuel tanks for minimum octane markings . . . . . . . . . . . . . . . . . . . . . . . . . o 16. Inspect fuel caps, cap gaskets, fuel filler neck gaskets, sight gauge gaskets, fuel gauge transmitter gaskets, gauge transmitter access covers, and upper surface inspection covers for condition, proper sealing, security, alignment, etc. ensure to service and clean these areas, replacing parts as necessary . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 17. Inspect the interior of metal fuel tanks for signs of corrosion, which may indicate water contamination. If signs of contamination are found, alert the owner and fuel supplier of your findings for corrective action . . . . . . . . . . . . . . . . o 18. Inspect the interior of bladder tanks for wrinkles, broken or missing hangers, etc. If signs of contamination are found, alert the owner and fuel supplier of your findings for corrective action . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 19. Inspect fuel cell vents . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 20. Inspect air ducts, electrical leads, lines, and attaching parts for security, routing, chafing, deterioration, wear, and correct installation. . . . . . . o 21. Install inspection plates and fairings . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o 22. Inspect static wicks per Static Wicks, Inspection, 23-60-00. (Replace as required.). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 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 per 7-10-00 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 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 condition and 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 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 INTERNATIONAL AEROTECH ACADEMY FOR TRAINING PURPOSES ONLY PIPER AIRCRAFT, INC. PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUAL 1D75-20-00 5. Scheduled Maintenance - Saratoga II HP (S/N’s 3246001 & up) (continued) Inspection NATURE OF INSPECTION Interval (Hrs) 50 100 PAGE 13 Mar 21/12 F. LANDING GEAR GROUP (CONT.) 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. Retrac