1965-1986 Piper Cherokee Six PA-32-260/PA-32-300/PA-32R-300 Service Manual (P/N 753 690)
721 Pages • 20.93 MB • Instant, Printable PDF
Piper Models Covered & Key Technical Specifications
Models: Piper Cherokee Six PA-32-260, PA-32-300, PA-32R-300
Sub-models / Variants: PA-32-260, PA-32-300, PA-32R-300
Model Years: 1965–1986
Serial Numbers: 32-1 to 32-7140086, 32-7200001 to 32-7840222, 32-7940001 and up, 32R-7680001 to 32R-7880068
Technical Data:
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Engine displacement: 540 cubic inches
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Engine power: 260 hp at 2700 rpm (PA-32-260), 300 hp at 2700 rpm (PA-32-300 / PA-32R-300)
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Oil sump capacity: 12 U.S. quarts
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Fuel capacity (total/usable): 84/83.5 gallons (PA-32-260/300), 98/94 gallons (PA-32-300 S/N 32-7940001 and up, PA-32R-300)
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Main landing gear strut extension: 4.50 inches (PA-32-260/300), 4.00 inches (PA-32R-300)
Piper Manual Features & Content Preview
- Official 721-page Piper Aircraft Corporation OEM service manual (publication 753 690), incorporating revisions through May 6, 1987.
- Covers the 1965–1986 Piper Cherokee Six PA-32-260, PA-32-300, and PA-32R-300 aircraft, documenting airframe, engine, landing gear, and electrical systems.
- Contains 80+ maintenance-related illustrations, exploded-view diagrams, system schematics, and comprehensive nut-torque tables.
Manual Contents & System Coverage
This comprehensive Piper Cherokee Six service publication provides the factory-authorized maintenance data required for thorough airframe inspections and component adjustments. Delivered as an instant download, the manual is organized into thirteen distinct sections across three aerofiche cards to streamline troubleshooting. The content covers everything from initial setup to specific subsystem maintenance, including detailed inspection protocols for the structure, flight controls, landing gear, and electrical systems. It features descriptive breakdowns of the wing, fuselage, and cabin heater systems, acting as a definitive reference for A&P mechanics and owner-operators working on the PA-32 aircraft family.
Technical Specifications & Workshop Data
Beyond general handling and servicing procedures, this documentation delivers critical data to eliminate guesswork in the shop. It details essential specifications like oil sump capacities (12 quarts) and specific fuel system storage for the 260 and 300 variants. You will find multi-stage sequences for cylinder head bolt torque, alongside precise nut torque requirements for both fine and coarse thread series. The manual also lists exact landing gear oleo strut extension measurements, such as 4.50 inches (±.25 inches) for the PA-32-260 main gear.
Note: understanding how factory workshop documentation is structured assists owners in utilizing these technical values correctly during routine operations. Please remember that all technical data is provided for reference purposes; always ensure critical maintenance is performed or supervised by a certified aviation mechanic to maintain strict flight safety standards.
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