1968-1975 Cessna Model 177, Cardinal, and Cardinal II Illustrated Parts Catalog Aircraft • P532-12-RAND-1500-7/75, issued June 15, 1975
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
Model 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
- Built for owners, operators, and aviation mechanics of the 1968–1975 Cessna 177, Cardinal, and Cardinal II
- Documents components for serial numbers 17700001 through 17702313
- Official Cessna publication PN 17702123 (P532-12-RAND-1500-7/75, issued June 15, 1975)
- Contains 498 pages of detailed parts lists, airframe breakdowns, and interior configurations
- Available as an instant download directly to your device the moment payment clears
- Accelerate your next repair with a fully indexed, searchable PDF covering every chapter and appendix
- Supersedes all previous 177 parts catalogs dated July 1967 through July 1974
Component and Assembly Documentation
Finding the correct fastener or trim piece shouldn't halt workshop productivity. This catalog delivers a complete breakdown of structural assemblies, including the wing structure, flap installations, and empennage components. Exploded-view diagrams map out the exact relationships between airframe parts, hardware, and interior trim elements. You get immediate visual reference for the correct identification of items ranging from auxiliary seat frames to wing leading-edge assemblies.
Additional sections break down interior painted and plastic parts. Clear coding for finish and trim plate identification removes the guesswork when sourcing replacements. The manual ensures accurate identification of trim assemblies, headliners, and moldings tailored to specific aircraft model years. Extensive placard and nameplate listings verify correct labeling for instrument panels and cockpit controls. Identifying the right component confidently speeds up the overall repair process.
Technical Specification Preview
The documentation highlights essential specifications for routine workshop operations. The service data dictates Cessna 177 shock strut inflation at 50 PSI. Firewall sealant application requires specific thermal protection thresholds of 2000 degrees for 5 minutes. Engine oil viscosity standards are clearly mapped by ambient temperature ranges. To guarantee operational safety, these figures serve strictly as a component reference guide; qualified aviation technicians must always consult the full technical documentation before executing hands-on work.
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