1977 Cessna 172 Skyhawk Series Factory Service Manual (OEM)
298 Pages • 12.67 MB • Instant, Printable PDF
Cessna Models Covered & Key Technical Specifications
Models: Cessna 172 Skyhawk Series, Reims/Cessna F172 Skyhawk, Skyhawk II
Sub-models / Variants: 172N, F172N
Model Years: 1977
Serial Numbers: 17267585, F17201515
Technical Data:
- Engine model: Lycoming O-320 Series
- Gross weight: 2300 lb
- Wing span: 36 ft
- Fuel capacity (standard): 43 gal total / 40 gal usable
- Oil capacity (with filter): 7 qt
- Propeller: 75 in McCauley (fixed pitch)
- Main tire pressure: 29 psi
- Nose tire pressure: 31 psi
- Nose gear strut pressure: 45 psi
- Battery location: Firewall
Cessna Manual Features & Content Preview
- Covers 1977 Cessna 172 Skyhawk Series aircraft, including the 172N and F172N variants powered by Lycoming O-320 engines
- Official 298-page Cessna OEM publication, first edition dated 1 July 1976
- Remains the primary reference source for launch build specifications, documenting engine, airframe, electrical, and control systems
- Contains 40 detailed system diagrams and 3 major torque specification tables
Manual Content Summary
This publication provides detailed maintenance procedures for the 1977 Cessna 172 Skyhawk series. Content spans ground handling, lubrication, and rigorous inspection routines. It also includes dedicated sections for the fuselage, wings, empennage, and landing gear. Aviation mechanics will find specific guidance on control system rigging, engine oil servicing, and structural repair protocols designed to keep the airframe in a verified configuration. Procedures for temporary and indefinite storage are detailed to help maintain airworthiness during long-term non-operational status. Because aviation maintenance inherently requires strict adherence to safety standards, users must always cross-reference these archival specifications with current FAA directives and utilize calibrated equipment prior to evaluating or servicing aircraft components.
Technical Data Preview
Technical specifications are centralized in Section 1. Here, professionals will find essential airframe dimensions, control surface travel limits, and fluid capacities. Key operational data includes main wheel tire pressure set at 29 psi, alongside nose gear strut inflation at 45 psi. The documentation lists precise torque values for steel nuts on oil-free cadmium-plated threads in both fine and coarse series. Additionally, cylinder head specification tables define the intake valve clearance at 0.11–0.20 mm.
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