1970-1976 Cessna Model 210 & T210 Centurion Aircraft Service Manual (P/N D2004-13-RAND-350-2/76)

• Details the 1970–1976 Cessna 210 and T210 Centurion, including Turbo Centurion II models and serial ranges 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, complete electrical schematics, and accurate repair reference data for shop environments.
• Outlines final factory-authorized specifications for the K and L-series builds, superseding previous maintenance documentation.

Structural and Maintenance Coverage

This 646-page OEM service manual documents factory procedures for ground handling, cleaning, lubrication, and structural inspection. The chapters break down fuselage architecture. This includes cabin doors, interior upholstery, and seat installations, alongside precise wing and empennage designs. Detailed sections map out the landing gear, brakes, and hydraulic networks. You get straightforward guidance on gear retraction cycles, nose gear shimmy dampeners, and wheel alignment. The documentation also provides engine specifications for both naturally aspirated and turbocharged powerplants, plus fuel system components and propeller governors. Mechanics rely on these precise component descriptions to streamline their repair workflows on the hangar floor.

Specification and Reference Data

Technical information leaves no room for guesswork. It includes strict tolerance charts, wear limits, and hydraulic pressure settings. The comprehensive torque table categorizes values for various steel nuts by thread type and size. Hydraulic system breakdowns offer targeted troubleshooting for the landing gear power pack and actuator assemblies. To ensure flight control rigging accuracy, control surface travel limits for the ailerons, elevators, and rudder are strictly defined.

Cross-reference tables and clear part identification diagrams simplify complex component tracking. Critical operational specifications include the main landing gear strut pressure at 90 psi (extended) and a Cessna 210 main wheel tire pressure of 55 psi. Furthermore, ground tests require the hydraulic power pack system to maintain a minimum of 25 psi.

Aviation safety relies on strict protocol. Always consult a certified aviation mechanic before servicing this equipment, as this documentation serves purely as an informational reference.