1971-1975 Cessna Cardinal RG Series Service Manual
Troubleshooting, parts diagrams, and service data for the Cessna Cardinal RG Series aircraft. Documents procedures, specifications, and maintenance. PN D991-3-13-RPC-200-7/79
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Models Covered & Key Technical Specifications
Cessna Cardinal RG Series (D991-3-13-RPC-200-7/79) - 1971-1975 Service & Maintenance Manual | Series Aircraft. Suite
- Factory Speed Rating: 1200 lbs establishes the maximum aircraft weight. Mapping.
- Certified Travel Rate: For optimal operation, 10 inches per minute defines the landing gear cycle. Configuration.
- Engineered Net Mass: 2800 lb -- signifies the gross aircraft weight. Benchmarks.
- Verified Assembly Torques: The critical components require 70-100 lb-in for proper installation. Range.
- Designated Adjustment Range: Control surfaces move 45 degrees maximum Parameters.
- Integral Cold Start Limits: The engine operates within -65°F to 100°F. Baseline.
Manual Description & Preview
Expert Reference Factory Manual: Aircraft Cessna 177RG Cardinal RG - Comprehensive Service & Maintenance Manual (1971-1975) Resource-Library
Machine-Range: 1971-1975 Cessna Cardinal RG Series // Model-Portfolio: Aircraft / Aviation Logic // Machine-Range: Technical Documentation.
| Performance-Element | Operational-Logic | Calibration-Data |
|---|---|---|
| Gross Weight | 2800 lb | Airframe |
| Fuel Capacity | 61 gal (Usable) | Fuel System |
| Oil Capacity | 8 qt (With External Filter) | Engine Systems |
| Engine Model | Lycoming IO-360 Series | Engine Data |
| Landing Gear | Pneumatic Hydraulic | Landing Gear System |
Technical units are distributed across the following sections: General Description, Ground Handling, Servicing, Lubrication, Inspection, and Aircraft Systems including Fuselage, Wings, Empennage, Landing Gear, Engines, Propellers, Fuel Systems, Instruments, Electrical Systems, and Structural Repair. Detailed procedures for maintenance and troubleshooting are provided throughout the manual.
Removal procedures are documented for control columns, trim tabs, and actuators. Detailed specifications are provided for critical components.
Factory specifications are documented for critical torque values and adjustments, ensuring proper assembly and function.
Engine rebuild procedures are documented for the Lycoming IO-360 series engine, covering disassembly, inspection, and reassembly.
Drivetrain specifications are addressed in various sections, detailing procedures for the landing gear and propeller systems. The manual documents torque specifications for critical components to ensure proper gasket seal integrity.
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