1968-1975 Cessna Model 177, Cardinal, and Cardinal II Illustrated Parts Catalog Aircraft
Full service documentation for Cessna 177, Cardinal, and Cardinal II, covering all parts for aircraft from 1968 to 1975. PN 17702123
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Sample pages from the 1968-1975 Cessna Model 177, Cardinal, and Cardinal II Illustrated Parts Catalog Aircraft manual
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Cessna Models Covered & Key Technical Specifications
Models: Cessna 177, Cardinal, Cardinal II
Sub-models / Variants: Standard, Long Range, Standard Wing, Long Range Wing, AA, B, C, D, E, F, G, H, J, K, L, M, N, P, Q, R, S, T, U, V, W, X, Y, Z, AB, AC, AD
Build Years: 1968–1975
Serial Numbers: 17700001 through 17702313
Technical Data:
- Engine oil capacity: Above 60°F use SAE 50, 0°F to 70°F use SAE 30, below 10°F use SAE 20
- Shock strut inflation: 50 PSI with no load on strut
- Hydraulic fluid type: MIL-H-5606
- Standard tire types: Various aircraft-grade pneumatic variants documented in parts listing
- Sealant temperature limits: Firewall sealant withstands 2000 degree heat for 5 minutes
Cessna Manual Features & Content Preview
Cessna 177 Cardinal Illustrated Parts Catalog Coverage
- Built for owners and operators of the 1968–1975 Cessna 177, Cardinal, and Cardinal II, documenting parts for serials 17700001 through 17702313
- Official Cessna Aircraft Company publication P532-12-RAND-1500-7/75, issued June 15, 1975
- Contains 498 pages of detailed parts lists and assembly diagrams for the airframe, interior, and paint configurations
- Accessible as a direct download the moment payment clears
- Indexed PDF search covers every chapter and appendix
- Re-download the file any time, no expiration
- This 1975 edition supersedes all previous 177 parts catalogs dated July 1967 through July 1974
Component and Assembly Documentation
This Cessna 177 parts manual provides a complete breakdown of structural assemblies, including wing structure, flap installations, and empennage components. The document features detailed exploded-view diagrams illustrating the relationships between various airframe parts, fasteners, and interior trim elements. Each section is organized to facilitate the correct identification of items ranging from auxiliary seat frames to wing leading-edge assemblies.
Additional chapters focus on interior painted or plastic parts, providing clear coding for finish and trim plate identification. This section ensures the correct identification of trim assemblies, headliners, and moldings tailored to specific aircraft model years. Extensive placard and nameplate listings verify the correct labeling for instrument panels and cockpit controls, ensuring the what an OEM service publication covers requirements for the aircraft are maintained.
Technical Specification Preview
Specification highlights include detailed oil change requirements and shock strut air pressure limits. The 1968–1975 Cessna 177 shock strut inflation is specified at 50 PSI in the service data. Firewall sealant application documents thermal protection thresholds of 2000 degrees for 5 minutes. The 1968–1975 Cessna 177 engine oil viscosity standards are listed by ambient temperature ranges to support proper maintenance. All service data shown here is for reference only — qualified technicians and the original OEM documentation remain the authoritative source for any hands-on work.
An official 498-page Cessna Aircraft Company illustrated parts catalog covering the 1968–1975 Cessna 177, Cardinal, and Cardinal II, documenting airframe, interior, and marking specifications for the specified serial number range.
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