Cessna 210K / T210K / 210L / T210L Illustrated Parts Catalog - 1974

Diagnostic procedures and component service for Cessna 210K / T210K / 210L / T210L aircraft. This catalog includes P/N C4085-91017 and details on assembly, parts, and diagrams for efficient aircraft maintenance.

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Document Details

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Document Number / Seller:
28128 / Deborah Wilson
File Size:
31.41 MB
File Type:
PDF
Language:
English
Pages:
667
Printable:
Yes
Category:
Aircraft
Last updated / verified
Aug 25, 2025

Models Covered & Key Technical Specifications

Cessna 210K / T210K / 210L / T210L (C4085-91017) -- 1974 Documentary Applied Compendium | Package.

  • Factory Maximum Resolution: 1200 dpi is set to establish the maximum print output Architecture.
  • Essential Assembly Torques: For optimal operation, 15-30C specifies the environmental limit Framework.
  • Key Capacity Limits: 450 W -- signifies the active printing consumption Threshold.
  • Verified Energy Draw: The formatter board requires 64 MB for standard operation Logic.
  • Designated Burn-in Temperature: Maximum throughput reaches 25 ppm Parameters.
  • Approved Optical Resolution: The [component] requires 1200 dpi for sharp image reproduction Requirements.

Manual Description & Preview

Commercial Diagnostic Calibration Manual: Aircraft Official Cessna 210K, T210K, 210L und T210L Illustrated Parts List - 1974 Aircraft Maintenance Reference Assembly-Guide

Series-Validation: Cessna 210K / T210K / 210L / T210L (C4085-91017) // Documentation-Type: Illustrated Parts List / Aircraft Maintenance Logic // Series-Validation: 1974.

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Identifier Operational-Logic Calibration-Data
Serial Number Identification 21059503 & ON N/A
Document Type Illustrated Parts Catalog N/A
Applicable Models Cessna 210K, T210K, 210L, T210L N/A

The service manual covers detailed illustrations and part numbers for various aircraft components. Effectively requiring accurate part identification, this document provides a critical reference for maintenance personnel. Documentation covers various systems, including wing assemblies, fuselage structures, and landing gear components.

Timing procedures are documented for key aircraft systems and sub-assemblies.

Technical notes are provided for specific part applications and identification.

Quality checks are addressed for components to ensure proper assembly and function.

The [component] section documents detailed part breakdowns for critical aircraft sections.

The troubleshooting chapter addresses part interchangeability and identification.

This catalog documents part numbers and diagrams to ensure proper assembly and joint separation prevention.

FAQ

Check the **standard** component identification for the firewall grommets. keyboard_arrow_down

19532-3 is the part number for the firewall grommet used in Installation C.

What does the **necessary** adjustment procedures entail for the nose gear steering system? keyboard_arrow_down

1243420-1 is the part number for the boot-steering link rod, which is a key component in the nose gear steering system.

Reference the **recommended** pressure specifications for the main landing gear. keyboard_arrow_down

103 indicates the page number where main landing gear wheel and brake installation details can be found.

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