1975-1986 Cessna Aircraft Model 172 Illustrated Parts Catalog
Diagnostic procedures and component service for Cessna 172 models, including airframe, engine, and interior components. Part numbers like 0500010-44 are listed.
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Models Covered & Key Technical Specifications
Cessna 172M / 172N / 172P / 172Q / 172RG / R172K / F172 (Reims) (0500001-134) - 1975-1986 Illustrated Parts Catalog | Aircraft File
- Reference Fluid Capacity: 20 GAL is calibrated to meet the requirements for the fuel system.
- Approved System Fill: For the integral fuel cell, 10 GAL governs the minimum volume Baseline.
- Designated Assembly Gap: For the wing assembly, 0.062 inches is specified as the standard dimension Requirements.
- Certified Dimensional Limits: The main landing gear requires 65.33 inches for proper alignment Mapping.
- Factory Locking Torques: The wing spar assemblies provide the necessary support Configuration.
- Fundamental Ambient Limits: -57 degrees C to 57 degrees C is rated at the maximum environmental Threshold.
Professional Workshop Service Manual & Technical Specifications
Illustrated Parts Catalog Manual: Cessna 172 Skyhawk, Cutlass, Hawk XP, F172 - Comprehensive Illustrated Parts Catalog 1975-1986 Logic-Archive
Design-Core: 1975-1986 // Machine-Range: Aircraft / Airframe Logic // Engineering-Metrics: Illustrated Parts Catalog.
| Integrated-Framework | Value | Calibration-Data |
|---|---|---|
| Part Number | Figure/Index | Description |
Maintenance hierarchies are structured into:
- Fuselage Assembly
- Wing Assembly
- Engine Components
- Landing Gear
- Control Surfaces
This document provides an exhaustive listing of all parts and components for the Cessna 172 series aircraft, covering models from 1975 through 1986. It includes detailed diagrams, part numbers, and serial number applicability to ensure accurate identification and ordering.
Brake system specifications are included for locating and identifying brake components.
Safety procedures are documented for information on ordering and general use of the catalog.
Fluid capacities are listed for specific parts of the aircraft, such as fuel tanks.
Tool requirements are listed for the proper assembly and disassembly of components.
Installation guidelines are provided for various parts to assist in their correct placement.
...documents torque specifications for wing spars to ensure proper structural misalignment prevention.
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