1970-1976 Cessna Model 210 & T210 Centurion Aircraft Service Manual

Cessna 210 and T210 Service Manual 1970–1976

• Covers the 1970–1976 Cessna 210 and T210 Centurion aircraft, including Turbo Centurion II variants and specific serial ranges from 21059200 through 21061040
• Official OEM publication D2004-13-RAND-350-2/76, incorporating Change 4, dated 1 October 1975
• Contains 40 detailed exploded-view diagrams, extensive torque specifications for fine and coarse thread hardware, and comprehensive electrical/hydraulic system schematics
• Delivered as a direct download the moment payment clears
• Stored against your account so you can retrieve it after a hard-drive loss
• Print resolution preserves exploded-view detail
• Indexed PDF search covers every chapter and appendix
• This fourth-change edition provides the final factory-authorized specifications for the L-model production run, superseding all earlier 1970–1976 maintenance documentation

Structural and Maintenance Coverage

This 646-page Cessna 210 service manual documents factory-recommended procedures for ground handling, cleaning, lubrication, and inspection. Chapters describe the fuselage architecture, including interior upholstery, seats, and cabin door installation, as well as the wing and empennage design. Detailed sections outline the landing gear, brakes, and hydraulic systems, providing guidance for gear retraction systems, nose gear shimmy dampeners, and wheel alignment. The publication also details engine specifications for both normally aspirated and turbocharged powerplants, along with fuel system components and propeller governors.

Specification and Reference Data

Technical information includes precise tolerance charts, wear limits, and pressure settings for hydraulic components. The torque table lists values for various steel nuts, categorized by thread type and size. The hydraulic system documentation provides troubleshooting for the landing gear power pack and actuator assemblies. Control surface travel limits for the ailerons, elevators, and rudder are specified with precision to ensure flight control rigging accuracy. Understanding parts documentation for aircraft is simplified through the included cross-reference tables and detailed component identification diagrams. The main landing gear strut pressure is documented at 90 psi for the extended state. Main wheel tire pressure for the Cessna 210 is specified at 55 psi. The hydraulic power pack system operates with a minimum of 25 psi during ground tests.

Reference only — always consult a certified technician before performing service on this equipment. An official 646-page Cessna OEM service manual covering the 1970–1976 Cessna 210 and T210 Centurion, documenting engine, chassis, electrical, and hydraulic specifications for the K and L-series builds.