Piper PA-28-140, PA-28-150, PA-28-160, PA-28-180, PA-28-235, PA-28R-180, and PA-28R-200 1961-1971 Service Manual (P/N 753-586)
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Piper Models Covered & Key Technical Specifications
Models: PA-28-140, PA-28-150, PA-28-160, PA-28-180, PA-28-235, PA-28R-180, PA-28R-200
Sub-models / Variants: Flite Liner
Model Years: 1961–1971
Serial Numbers: PA-28-140: 28-1 to 28-1760, 28-7125174 and up, 28-7225001 and up, 28-7425001 and up, 28-25000 to 28-26956, 28-7125001 to 28-7325684, 28-7425001 and up; PA-28-150/160/180: 28-1761 to 28-4377, 28-4378 to 28-7105244, 28-7205001 to 28-7205328, 28-7305001 and up; PA-28-235: 28-10000 to 28-11039, 28-11040 to 28-7110042, 28-7210001 to 28-7210033, 28-7310001 and up; PA-28R-180: 28-30005 to 28-7130019; PA-28R-200: 28-30482, 28-35001 to 28-35830, 28-7135001 to 28-7135238, 28-7235001 to 28-7335455
Technical Data:
- Engine models: Avco-Lycoming O-320, O-360, O-540, IO-360 series
- Fuel system: 50 U.S. gallons (standard), 84 U.S. gallons (PA-28-235)
- Hydraulic fluid: MIL-H-5606
- Propeller types: Sensenich fixed pitch, Hartzell/McCauley constant speed
- Main gear tire pressure: 24 psi (PA-28 models) up to 35-40 psi (PA-28R-200)
Piper Manual Features & Content Preview
- Covers the 1961–1971 Piper PA-28 Cherokee series, including the 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.
- 916-page primary technical record documenting all configurations, including fixed and retractable landing gear variants.
- Features over 150 detailed technical illustrations mapping out access panels, station reference lines, fuel systems, and engine installations.
Manual Content and Structural Overview
Having exact factory reference data on the hangar floor takes the guesswork out of maintenance. This official Piper service document breaks down the Cherokee family system by system, giving mechanics a structured baseline for daily operations. It skips the filler. You dive straight into ground handling procedures, scheduled servicing, and structural airframe inspections.
Working on active aircraft naturally demands strict adherence to approved tolerances to ensure flight safety. Always cross-reference current baseline data before turning a wrench.
Inside, technicians will find exhaustive reference material for landing gear maintenance on both fixed and retractable setups. Flight control rigging is covered in high detail. The manual lays out the required tolerances needed for ailerons, stabilators, and rudders. Beyond the structural components, the text maps out the electrical and fuel systems. You can quickly reference wiring diagrams for different sub-models. Need to trace a fuel issue? It details pump configurations and transmitter calibration steps. HVAC component installation and testing procedures are fully outlined. Finally, the document delivers essential engine installation and cooling baselines to support Avco-Lycoming powerplant maintenance and propeller governors.
Specification Highlights and Data Preview
Accurate technical data speeds up diagnostic time in the workshop. This manual categorizes torque values for nuts and bolts by thread series, keeping workflow highly efficient. It also lists fluid capacities for all standard fuel and hydraulic setups used across the 1961–1971 production run.
Hard technical metrics are clearly defined. For example, nose gear oleo strut exposure is set at 3.25 ±.25 inches for standard PA-28 models. If you are servicing the fixed-gear Cherokee 235, the main gear oleo strut exposure is documented at 4.5 ±.50 inches. The principal dimensions table also logs the PA-28-235 fuel system capacity at exactly 84 U.S. gallons.
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