1995–2004 Piper PA-32R-301/301T Saratoga II HP/TC Parts Catalog (P/N 761-880)
414 Pages • 5.33 MB • Instant, Printable PDF
Piper Models Covered & Key Technical Specifications
Models: PA-32R-301 Saratoga II HP, PA-32R-301T Saratoga II TC
Sub-models / Variants: HP (High Performance), TC (Turbocharged)
Model Years: 1995–2004 (1995, 1996, 1997, 1998, 1999, 2000, 2001, 2002, 2003, 2004)
Serial Numbers: PA-32R-301: 3246001 and up. PA-32R-301T: 3257001 and up.
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Electrical system voltage: 14 V (PA-32R-301 serial numbers 3246001–3246017); 28 V (PA-32R-301 serial numbers 3246018 and up; PA-32R-301T serial numbers 3257001 and up)
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Alternator capacity: 90 A
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Maximum rated horsepower: 300 hp
Piper Manual Features & Content Preview
This Piper OEM illustrated parts catalog, P/N 761-880, reissued July 10, 2004, covers the 1995–2004 PA-32R-301 Saratoga II HP and PA-32R-301T Saratoga II TC. It identifies replacement components by figure, part number and aircraft serial-number effectivity.
Text search and drawing detail: Text and parts tables are searchable, with PDF bookmarks for sections, figures and the numerical index. Labels within illustrations are outside text search. Small callouts benefit from zooming; some tiny panel legends remain difficult to read.
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Airframe and tail surfaces: Illustrated parts breakdowns for wings, fuselage assemblies, cabin doors, the stabilator, fin and rudder.
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Landing gear and hydraulics: Nose and main gear assemblies, wheel and brake components, master cylinders, hydraulic pumps, actuators and lines.
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Powerplant and fuel system: Separate HP and TC installation breakdowns, engine controls, exhaust components, Hartzell propeller parts, fuel pumps and tank assemblies.
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Control system: Aileron, flap, stabilator and rudder controls, trim mechanisms, control wheels and rudder pedals, with associated cables and hardware.
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Instruments: Serial-specific instrument panels, Vacuum System Installation, Standby Vacuum System Installation and Pitot Static System Installation illustrations and parts lists.
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Cabin equipment and environmental systems: Seating configurations, interior panels, heating, ventilation, air-conditioning assemblies and the TC oxygen system.
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Electrical and electronics: Switch, annunciator and circuit-breaker panels, battery installations, external power, strobe lights, ELT components and avionics drawing references.
The illustrated listings suit aircraft mechanics and parts personnel familiar with serial-number effectivity who need component identification for parts purchasing and repair planning.
Parts Documentation Overview
Exploded-view diagrams and itemized parts lists connect each illustrated assembly to its component numbers and quantities. The table of contents and numerical index retain the GAMA-standardized Aerofiche grid references for component lookup.
Instrument-panel changes: The HP panel breakdowns distinguish serial numbers 3246001–3246017, 3246018–3246087 and 3246088 and up; the TC has its own breakdown. These divisions help identify the applicable panel components before ordering, rather than relying on the Saratoga name alone.
Landing Gear, Fuel and Powerplant Parts
The Nose Gear Assembly and Hydraulic System Installation illustrations identify strut components, seals, hydraulic cylinders and connecting lines. Separate Cleveland 10-30 and Gar-Kenyon 17000 toe-brake master-cylinder listings identify the components for each assembly.
Fuel-cap identification: Fuel Tank Assemblies includes locking and non-locking caps. Gaskets, O-rings and lock components are tied to particular cap assemblies or kits, so matching the existing cap matters when selecting replacement seals.
The powerplant listings cover engine mounts, induction and alternate-air components, oil-cooler connections, engine exhaust and propeller hardware. Engine assemblies and certain alternator items are referred to Textron Lycoming; this is not an internal engine-overhaul catalog.
Electrical, Instruments and Avionics
Early HP aircraft use 14-volt components; later HP aircraft and the TC use 28-volt components. The differences extend to electric fuel pumps, flap actuators, lighting and standby-vacuum equipment.
Electrical System Installation provides component-location illustrations and parts lists, not circuit wiring diagrams. The Avionics Installation Drawings page lists references 79643 and 85495; the referenced drawings themselves are not included.
Cabin Equipment, Finishes and Service References
Cabin listings distinguish five-seat and six-seat installations. The Environmental Group separates compressor, refrigerant-line, evaporator and condenser components, with oxygen-system parts listed for the TC.
The standard paint chart lists DuPont Imron finishes and instrument-panel colors, with a Service Spares Letter 407 reference for thermoplastic interior-panel paint. Placards Installation and the service/optional-kit list include identification markings and repair kits, including hydraulic seal replacement kit 652-363.
Service Bulletins and Letters are cross-referenced to affected figures and kits. These references are not the full service documents or a current compliance record.
Parts Catalog Scope
This publication does not contain diagnostic instructions, maintenance procedures or step-by-step repair guidelines. Piper specifically excludes its use for rigging and installation; flight-control and landing-gear illustrations must not be treated as assembly instructions.
PDF Contents and Page Count
One printable English PDF contains 414 pages: 246 for Aerofiche Card 1 and 168 for Card 2. The totals include both 14-page opening sections, each with its original cover, and all 68 pages marked intentionally blank, four of which fall within those opening sections. No separate supplement is included.
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