1961-1971 Piper PA-28 Cherokee Series Aircraft Service Manual

Technical Scope for the 1961–1971 Piper PA-28 Cherokee

• Covers the 1961–1971 Piper PA-28 Cherokee series, including PA-28-140, PA-28-150, PA-28-160, PA-28-180, PA-28-235, PA-28R-180, and PA-28R-200
• Official Piper Aircraft Corporation publication, P/N 753-586, interim revision dated February 27, 2004
• Features over 150 detailed illustrations of access panels, station reference lines, fuel systems, and engine installations
• Stored against your account so you can retrieve it after a hard-drive loss
• Full-text search finds any part number in seconds
• This 916-page publication serves as the primary technical record for the airframe, documenting all configurations including fixed and retractable landing gear variants

Manual Content and Structural Overview

This official Piper PA-28 Cherokee service documentation provides comprehensive maintenance guidance for the entire Cherokee family. The content is organized by system, starting with an introduction to the aircraft design, followed by exhaustive sections on ground handling, servicing procedures, and airframe structures. Technicians find detailed information regarding inspection schedules, landing gear maintenance for both fixed and retractable types, and specific rigging instructions for flight controls, including ailerons, stabilators, and rudders.

The document also covers the extensive fuel and electrical systems, documenting fuel pump configurations, transmitter calibration, and wiring diagrams for various sub-models. Heating, ventilation, and air conditioning systems are explored with component installation and testing details. Additionally, the manual provides data for engine installation and cooling, ensuring that the necessary procedures are available for Avco-Lycoming powerplant maintenance and propeller governance.

Specification Highlights and Data Preview

This publication includes detailed technical data for identifying aircraft configuration and service limits. Torque values for nuts and bolts are categorized by thread series, and fluid capacities are provided for various fuel and hydraulic setups. The manual covers how factory workshop documentation is structured to facilitate accurate maintenance performance across the entire 1961–1971 production range.

Key technical metrics include: Nose gear oleo strut exposure is specified at 3.25 ±.25 inches for PA-28 models. Main gear oleo strut exposure is documented as 4.5 ±.50 inches for the fixed-gear Cherokee 235. The fuel system capacity for the PA-28-235 is 84 U.S. gallons, documented within the principal dimensions table. An official 916-page Piper OEM service manual covering the 1961–1971 PA-28 Cherokee, documenting structural, landing gear, and systems maintenance data for all primary airframe variants.