1969-1976 Cessna 150 Series Service Manual
Covers Cessna 150, Reims/Cessna F150, and Cessna A150 models from 1969-1976. Includes detailed procedures for airframe, engines, and systems. Ref: D971C3-RAND-1600-7/75
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Cessna Models Covered & Key Technical Specifications
Models: Cessna 150, Reims F150, Cessna A150
Sub-models / Variants: 150 Standard, 150 Trainer, 150 Commuter, 150 Commuter II, Reims/Cessna F150, 150 Aerobat, Reims/Cessna F150 Aerobat
Build Years: 1969–1976
Serial Numbers: 150J 15069309–15071128, 150K 15071129–15072003, 150L 15072004–15074850, 150M 15074851–15077006, F150J F15000390–F15000529, F150K F15000530–F15000658, F150L F15000659–F1501143, F150M F15001144–F15001248, A150K A1500001–A15000226, A150L A15000227–A1500609, A150M A1500524–A1500610, FA150K FA1500001–FA1500081, FA150L FA1500082–FA1500261, FA150M FA1500262–FA1500281
Technical Data:
- Gross weight: 1600 lb
- Engine model: Continental O-200 Series
- Propeller: 69" McCauley (Fixed Pitch)
- Standard fuel capacity: 26 gal total
- Long-range fuel capacity: 38 gal total
- Electrical system: 12 VDC
- Nose gear strut pressure (extended): 20 psi
- Main tire pressure: 21 psi
- Wing span: 32' 8-1/2" (Conventional), 33' 2" (Conical Camber)
Cessna Manual Features & Content Preview
1969–1976 Cessna 150 Series Service Manual
- Covers 1969–1976 Cessna 150, Reims F150, and A150 aircraft, including Aerobat, Commuter, and Trainer variants
- Official OEM publication, Change 3 dated 15 June 1975, superseding all prior manual revisions
- Contains 47 detailed system exploded-view diagrams and 16 system-specific technical specification tables
- File delivers as a direct download the moment payment clears
- Indexed PDF search covers every chapter and appendix
- This 358-page reference is the factory standard for maintenance documentation on the O-200-powered Cessna 150 light aircraft portfolio
Aircraft System Documentation
This Cessna 150 service manual covers technical maintenance and structural support for the entire 1969–1976 production range. Technical sections document standard procedures for ground handling, hoisting, leveling, and parking, alongside instructions for major airframe components like the fuselage, wings, and empennage. Coverage extends to landing gear inspection and troubleshooting, including specific wheel removal and brake assembly sequences. Electrical systems and wiring diagrams are provided, along with specialized procedures for managing structural repairs and aircraft finishing.
Specification and Servicing Highlights
The 1969–1976 Cessna 150 aircraft fuel capacity is documented at 26 gallons for standard wing configurations. Landing gear strut pressure for the nose wheel is specified at 20 psi in the aircraft specification table. Detailed torque values for steel nuts on oil-free cadmium plated threads are provided for fine and coarse thread series. Lubrication requirements are categorized by frequency, including daily, 50-hour, 100-hour, and 200-hour inspection intervals for flight-critical components. Users should consult what an OEM service publication covers to understand the scope of the maintenance program, which includes detailed troubleshooting guides for landing gear shimmy, tire wear, and control wheel resistance. Reference only — always consult a certified technician before performing service on this equipment.
An official 358-page Cessna OEM service manual covering the 1969–1976 Cessna 150, Reims F150, and A150 series, documenting airframe, landing gear, engine, and electrical specifications for the entire production range of these aircraft.
Document Reference: D971C3-13-RAND-1600-7/75, Change 3 dated 15 June 1975
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