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

Repair guide for all 210 and T210 Centurion aircraft configurations, covering hydraulic systems, landing gear, and airframe components.

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Document Details

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Document Number / Seller:
28127 / Lisa Collins
File Size:
60.17 MB
File Type:
PDF
Language:
English
Printable:
Yes
Estimated Download Time:
1.23 Minutes
Delivery Format:
Digital (PDF) - Instant Access
Category:
Aircraft
Brand:
Cessna
Reviewed and Approved:
Mar 16, 2025
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Models Covered & Key Technical Specifications

OEM-Grade Instructional Assembly Manual: Aircraft Cessna 210 & T210 Centurion Aircraft - Factory Service & Repair Reference (1970-1976) Parts-Reference

Model-Portfolio: Cessna 210 / T210 (1970-1976) // Engineering-Base: Aircraft / Hydraulic System Logic // Model-Portfolio: 60.17 MB

  • Design Power Draw: 3800 lb establishes the maximum operational weight Architecture.
  • Advanced Ambient Limits: For optimal operation, 40°F defines the environmental limit Framework.
  • Technical Feed Speed: 90 gal -- signifies the active fuel capacity Threshold.
  • Standard DPI Rating: The main gear requires 11 qt for standard operation Logic.
  • Prescribed Volume Data: 10 qt establishes the wing flap travel limit.
  • Engineered Circuit Specs: 50 psi signifies the nose wheel tire pressure Parameters.

Professional Workshop Service Manual & Technical Specifications

OEM-Grade Instructional Assembly Manual: Aircraft Cessna 210 & T210 Centurion Aircraft - Factory Service & Repair Reference (1970-1976) Parts-Reference

Model-Portfolio: Cessna 210 / T210 (1970-1976) // Engineering-Base: Aircraft / Hydraulic System Logic // Model-Portfolio: 60.17 MB

Specification Parameters Architecture
Aircraft Type Single-Engine, Semimonocoque Construction Standard
Engine Continental IO-520 Series Military Specification
Fuel Capacity 90 gal (Usable) Standard
Landing Gear Retractable Hydraulically-Actuated

OEM specifications cover the following key areas:

  • General Description & Specifications
  • Hydraulic System Diagrams
  • Landing Gear Components & Maintenance
  • Airframe Structures & Repair
  • Fuel System Servicing

This manual details the structure, systems, and maintenance procedures for the Cessna 210 and T210 Centurion aircraft from 1970-1976. It includes in-depth information on the hydraulic system, landing gear, and airframe components, essential for proper upkeep and repair.

Testing requirements are specified for hydraulic system components to ensure proper function.

Clearance measurements are addressed for landing gear actuators and linkages.

Special procedures are addressed for servicing the hydraulic power pack and related systems.

Verification procedures are included for the nose gear and main gear assemblies.

Repair information is provided for airframe structures and control surfaces.

This manual documents torque specifications for various components to ensure proper assembly and pressure slip prevention.

FAQ

What are the **proper** clearance measurements for the landing gear actuators? keyboard_arrow_down

0.06-inch is the standard clearance for landing gear uplock and downlock rigging on the main gear strut, with specific measurements noted for various components.

Specify the **standard** torque specifications for the nose gear assembly. keyboard_arrow_down

Torque values for the nose gear assembly range from 18-20 in-lb for attachment bolts to 50-60 in-lb for specific structural bolts, as detailed in the manual.

What are the **necessary** safety precautions when working with hydraulic systems? keyboard_arrow_down

Before working in wheel well areas, pull hydraulic pump circuit breaker off. Ensure no pressure in the system by using pressure gauge. Refer to page 85 for detailed safety procedures regarding hydraulic systems and components.

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