Piper PA-32R-301 Saratoga II HP & PA-32R-301T Saratoga II TC 1995-2004 Airplane Maintenance Manual

• Covers the 1995–2004 Piper PA-32R-301 Saratoga II HP and PA-32R-301T Saratoga II TC models, providing descriptive repair references and maintenance procedures for naturally aspirated and turbocharged variants
• Official 1,236-page Piper publication (P/N 761-879) for the 46 and 57 series airframes, featuring revisions from the 1996 first edition through February 2004
• Contains 64 detailed illustration plates and over 40 technical charts mapping system capacities, torque specifications, and inspection schedules
• Highlights current inspection requirements for the model line, including specialized intervals for TC-series turbocharged components

Manual Content Summary

Organized according to GAMA Specification No. 2, this aviation manual drastically cuts down the time spent searching for technical specs on the hangar floor. Aviation technicians get streamlined access to structural data for the fuselage, power plant servicing routines, and electrical systems. Need to evaluate the landing gear? The document details oleo strut pressure settings alongside comprehensive layouts for environmental, fuel, and flight control components. It also outlines strict inspection criteria for airframes subjected to severe turbulence, hard landings, or lightning strikes. Mechanics operating in high-dust or extreme-cold environments will find the specific operational requirements needed to maintain airworthiness under harsh conditions.

Specification and Reference Data

Relying on exact tolerances prevents critical errors during daily workshop routines. The publication lists precise oil pressure limits, spark plug gap dimensions, and magneto timing requirements set at 20 degrees BTC. Mechanics use the provided reference charts to verify specific torque values, from standard nut torques to ignition harness coupling specs. Fluid capacities are clearly logged, detailing the exact 12 U.S. quart requirement for the engine sump. By following the standard system-chapter arrangement, shop personnel can quickly isolate the specific repair data required for any given component. Because aviation maintenance inherently involves significant risk, always cross-reference these technical specifications with the most current OEM bulletins and ensure all work is performed by certified professionals before clearing an aircraft for flight.