1968–1975 Cessna Model 177, Cardinal, and Cardinal II Illustrated Parts Catalog Aircraft (P/N P532-12-RAND-1500-7/75)
498 Pages • 26.30 MB • Instant, Printable PDF
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
- 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
- Accelerate your next repair with a fully indexed PDF covering every chapter and appendix
- Supersedes all previous 177 parts catalogs dated July 1967 through July 1974
- Features stabilators, shimmy dampeners, vacuum systems, alternators, and turn coordinators
- Details nose gears, main landing gears, fuel systems, and exterior placards
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. Accurate part identification is the first step in successful troubleshooting.
A notorious repair trap when servicing the 1968–1975 Cardinal series involves the all-moving stabilator and the nose gear. Technicians familiar with other Cessna models sometimes assume interchangeable hardware, leading to improper rigging or using incorrect AN and NAS fasteners on the critical pivot points. Utilizing the specific usable-on codes and component assembly drawings in this catalog ensures you procure the exact linkages, preventing severe in-flight vibrations or landing gear shimmy.
Additional sections break down interior painted and plastic parts. Instead of paying high shop rates for a specialized facility to identify matching upholstery, the manual provides step-by-step instructions on decoding the finish and trim plate to properly order interior elements yourself. Clear coding ensures accurate matching when sourcing replacements. Beyond structural components, the documentation features paint code charts, bulk item diagrams, and placard layout views. The manual ensures precise 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, while detailing the exact step-by-step filling instructions for the nose gear shock strut. 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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