Piper PA-28-140, PA-28-150, PA-28-160, PA-28-180, PA-28-235, PA-28R-180, PA-28R-200 Cherokee Aircraft Service Manual - Comprehensive Maintenance & Repair Procedures 1961-1971
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Sample pages from the Piper PA-28-140, PA-28-150, PA-28-160, PA-28-180, PA-28-235, PA-28R-180, PA-28R-200 Cherokee Aircraft Service Manual - Comprehensive Maintenance & Repair Procedures 1961-1971 manual
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Models Covered & Key Technical Specifications
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Piper Cherokee PA-28 Series (753-586) — 1968–2004 Technical Repository PA-28-140, PA-28-150, PA-28-160, PA-28-180, PA-28-235, PA-28R-180, PA-28R-200 Aircraft Library (Service-Logic).
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Specific Measurement: 1/32 inch is required for the cable-to-pulley clearance to prevent structural binding within the flight control architecture.
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Essential Rating: 12V / 25Ah must be maintained for the primary battery system to ensure reliable engine cranking under cold-weather conditions.
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Advanced Parameter: 50 PSI establishes the standard inflation threshold for the nose gear oleo strut to facilitate optimal impact absorption.
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Core Limit: 2000 RPM signifies the maximum allowable engine speed during the magneto ground check sequence to verify ignition integrity.
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Technical Data-Point: 0.012 - 0.015 inches defines the spark plug electrode gap specification for the Lycoming powerplant assembly.
Professional Workshop Service Manual & Technical Specifications
Piper Cherokee PA-28 Series — Service Manual (Contents Overview)
This listing provides a manual contents and scope preview for the Piper Cherokee PA-28 series, covering early production years from 1961 through the early 1970s (coverage can vary by model, serial range, and edition). The manual is presented as a technical reference organized by major aircraft systems and serial-number-specific sections.
Included content (typical sections)
- Manual structure and aircraft identification references (model/serial-based grouping)
- Model coverage index for PA-28 variants (as listed in the manual)
- Serial number range breakdowns to match specific airframes and editions
- Structures & airframe coverage with diagrams and reference tables
- Powerplant-related sections referencing Lycoming engine families (e.g., O-320, O-360, O-540)
- Landing gear and hydraulics system coverage (including PA-28R Arrow sections where applicable)
- Fuel system coverage with variant-specific notes (edition-dependent)
- Electrical/avionics references with wiring diagrams and component indexing (edition-dependent)
- Flight control system sections with configuration notes by variant
- Inspection form references by interval (where included in the manual)
- Specification appendices (e.g., tightening data, lubrication/fluid reference tables)
- Table of contents and index/navigation tools
Note: This page is a contents overview for the manual. It does not provide step-by-step repair, inspection, or diagnostic instructions.
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