1975-1986 Cessna Aircraft Model 172 Illustrated Parts Catalog (P/N P696-12)
Cessna Models Covered & Key Technical Specifications
Models: Cessna 172M, Cessna 172N, Cessna 172P, Cessna 172Q, Cessna 172RG, Reims F172, R172K
Sub-models / Variants: Skyhawk, Skyhawk II, Cutlass, Cutlass II, French Manufactured (Reims), Long Range Wing, Integral Fuel Cell
Model Years: 1975–1986
Serial Numbers: 172M (17263459–17276584), 172N (17272884–17275034), 172P (17275759–17276259), 172Q (17275869–17276516), F172M (F17201235–F17201514), F172N (F17201640–F17202134), F172P (F17202195–F17202238)
Technical Data:
- Fuel system capacity: 19–31 gallons depending on configuration
- Operational temperature range: -57°C to 57°C
- Standard wing assembly dimension: 0.062 inches
- Main landing gear alignment limit: 65.33 inches
Cessna Manual Features & Content Preview
- 662-page official Cessna Aircraft Company publication P696-12, revised August 1, 1996
- Built for owners and workshops servicing the 1975–1986 Cessna 172 series, including 172M, 172N, 172P, 172Q, 172RG, and Reims F172 models
- Contains dozens of detailed exploded-view assembly diagrams for wing structures, fuel systems, and exterior trim components
- Supersedes all previous 172 parts catalogs dated 1974 through 1985
Component Catalog Overview
Pinpointing the exact replacement part quickly keeps shop operations profitable. This parts catalog defines the structural components and replaceable hardware for multiple 172 variants, including the Skyhawk, Skyhawk II, and Cutlass. Detailed lists break down wing assemblies, fuel tank installations, and interior trim configurations. Mechanics get a granular view of every sub-component and its attaching hardware, eliminating guesswork during the ordering process.
Specification and Identification Data
Beyond basic part numbers, the publication documents exact structural clearances. You will find specifics like the 0.062-inch wing assembly gap alongside the 65.33-inch main landing gear alignment. Fuel system data specifies capacity volumes ranging from 19 to 31 gallons, ensuring accurate part matching for both standard and long-range wing setups. It also lists environmental thresholds rated for maximum limits between -57°C and 57°C. Since aviation maintenance carries inherent risks, any structural work or component installation guided by these specifications must be performed and verified by a certified airframe and powerplant mechanic to ensure airworthiness.
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