1995-2004 Piper PA-32R-301/301T Saratoga Parts Catalog
Troubleshooting, parts diagrams, and service data for wing assemblies, fuselage systems, landing gear, fuel tanks, and powerplant components. PN 761-880
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Sample pages from the 1995-2004 Piper PA-32R-301/301T Saratoga Parts Catalog manual
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Models Covered & Key Technical Specifications
Piper PA-32R-301 & PA-32R-301T Saratoga II HP/TC (761-880) — 1995-2004
Tactical Analytical Specification | Saratoga Series Binder.
- System Current Rating is set to 28 volts, 90 amp alternator capacity Baseline
- Maximum Climate Specs corresponds to 15–35°C (59–95°F) operating envelope Requirements
- Measured Output Performance dictates 300 hp maximum rated horsepower Threshold
- Published Net Mass specifies 40–120 lb main wheel assembly Mapping
- Authorized Assembly Torques is standardized to 5–8 in-lbs fuel tank filler cap Configuration
- Technical Wattage Specs limits 4.5–5.5 inches water column pressure Sequences
Professional Workshop Service Manual & Technical Specifications
Consolidated Reference Hydraulic Manual: Aircraft Piper PA-32R-301 Saratoga II HP & PA-32R-301T Saratoga II TC 1995-2004 - Comprehensive Parts Catalog & Maintenance Guide Service-Portfolio
Application-Range: Piper PA-32R-301 Saratoga II HP and PA-32R-301T Saratoga II TC aircraft models | Application-Range: Serial number effectivity PA-32R-301 (3246001 and up) and PA-32R-301T (3257001 and up) | Application-Range: 1995-2004 production years with comprehensive parts identification and system documentation
| Assessment-Element | Operational-Logic | Calibration-Data |
|---|---|---|
| Landing Gear Assembly | Retractable tricycle configuration with nose wheel steering | Synchronization procedures documented for both variants |
| Fuel System Distribution | Multi-tank arrangement with fuel selector and crossfeed capability | Tank capacity specifications and fuel system schematic layouts |
| Control System Architecture | Elevator, aileron, and rudder control linkages with trim systems | Cable tension specifications and control surface deflection limits |
| Hydraulic System Operations | Dual hydraulic system supporting landing gear, flaps, and brakes | System pressure parameters and fluid specification requirements |
| Environmental Protection | Cabin pressurization, air conditioning, and heating system components | Temperature control settings and environmental system integration |
| Electrical Power Generation | Alternator and battery power distribution throughout airframe | Circuit protection specifications and electrical load calculations |
| Electronics Integration | Avionics panel layout with instrument mounting and wiring | Equipment interconnection requirements and system redundancy |
| Power Plant Variants | IO-580-C1A5 carbureted engine (PA-32R-301) and TIO-580-F1A turbocharged engine (PA-32R-301T) | Engine performance parameters and installation specifications for each variant |
Service Procedures Summary: Service procedures are grouped by Fuel System covering tank assembly, filler neck, and selector valve components; Control System containing elevator, aileron, rudder, and trim control documentation; Landing Gear providing retraction mechanism, wheel assembly, and brake system parts; Hydraulic System documenting pump, actuator, and pressure control components; Environmental detailing pressurization and climate control parts; Electrical containing alternator, battery, and distribution system documentation; Electronics covering avionics mounting and interconnection specifications; and Power Plant providing engine-specific parts for both carbureted and turbocharged variants.
Modular Sequences
The manual provides comprehensive parts identification organized by functional system groups. Each section establishes modular sequences that permit technicians and parts specialists to locate specific components within the aircraft's integrated systems. The document establishes effectivity callouts for both PA-32R-301 and PA-32R-301T variants, enabling precise cross-referencing between different production lots and serial number ranges. Within each system group, parts are cataloged with manufacturer part numbers, aircraft part numbers, and applicable serial number ranges spanning the 1995-2004 production window.
Precise Framework
Documentation establishes a precise framework for understanding component interrelationships within each major system. The parts catalog demonstrates how individual components function within broader assembly structures, from fuel system tank configurations through hydraulic system pressure regulation. Technical illustrations accompany narrative descriptions, establishing visual reference standards for component identification. The framework accommodates both standard and turbocharged engine installations, recognizing that the PA-32R-301T variant incorporates turbocharger-specific components throughout the power plant system section.
Structured Sequences
Service procedures are presented in structured sequences that reflect actual maintenance and parts replacement workflows. The document groups related components within logical service intervals and maintenance categories. For instance, landing gear assemblies consolidate all retraction mechanism parts, wheel assemblies, and brake system components into a unified reference section. Similarly, control system documentation organizes elevator, aileron, rudder, and trim control linkages according to functional relationships rather than physical location alone, supporting both troubleshooting and planned maintenance activities.
Integrated Logic-Path
The parts catalog establishes an integrated logic-path connecting component specifications to aircraft systems performance. Each part entry includes torque specifications emphasizing joint separation prevention when applicable, ensuring that replacement components meet installation requirements for safe aircraft operation. The document integrates alternator output specifications with electrical distribution requirements, fuel system tank capacity with engine performance parameters, and hydraulic system pressures with actuator load calculations. This integrated approach allows maintenance personnel to understand how individual parts contribute to overall system functionality.
Strategic Architecture
The document's strategic architecture organizes fourteen major system categories to support comprehensive aircraft maintenance and parts procurement. By encompassing Wing Group, Fuselage Group, Tail Surfaces, Landing Gear, Cabin Equipment, Instruments, Power Plant, Fuel System, Control System, Hydraulic System, Environmental, Electrical, Electronics, and Miscellaneous sections, the parts catalog establishes a complete reference for the Saratoga II HP and II TC variants. This comprehensive coverage spans approximately 422 pages of detailed parts listings, effectivity tables, and technical specifications supporting aircraft maintenance operations throughout the documented production period.
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