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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Sample pages from the Cessna 210K / T210K / 210L / T210L Illustrated Parts Catalog - 1974 manual
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Cessna Models Covered & Key Technical Specifications
Models: Cessna 210K, T210K, 210L, T210L
Sub-models / Variants: Turbo Centurion, Centurion II, Turbo Centurion II
Build Years: 1970–1975
Serial Numbers: 21059200 through 21060540 and on
Technical Data:
- Engine oil capacity: Not specified
- Maximum allowable manifold pressure: Documented per altitude tables in Placards section
- Required electrical power: 24 Volts D.C.
- Standard print output resolution: 1200 dpi
- Max throughput: 25 ppm
Cessna Manual Features & Content Preview
Cessna 210K/T210K & 210L/T210L Parts Catalog Preview
- Covers 1970–1975 Cessna 210K, T210K, 210L, and T210L variants including Turbo Centurion and Centurion II configurations
- Original OEM publication P523-12-RAND-1000-10/74, published September 1, 1974
- Contains 12 detailed exploded-view airframe diagrams and extensive parts-usage cross-reference tables
- File delivered as a direct download the moment payment clears
- Indexed PDF search covers every chapter and appendix
- what an OEM service publication covers
- Note: This page is a contents overview for the manual. It does not provide repair or diagnostic instructions.
- This 1974 first edition serves as the definitive reference for the C4085-91017 airframe series, documenting specific interior finish codes and structural sub-assemblies for the listed 1970–1975 models.
Component and Structural Walkthrough
This Cessna 210K and T210L illustrated parts catalog provides the complete structure for airframe maintenance and component procurement. The manual begins with comprehensive alphabetical and numerical indexes, allowing for rapid location of specific assemblies such as wing structures, empennage components, landing gear, and control systems. Each chapter details the individual components with their associated part numbers, units per assembly, and applicability to specific serial number ranges.
Specification and Identification Data
This documentation lists key identification data including the Finish and Trim Plate interpretation, which maps the specific year, interior color, and exterior paint combination for each aircraft. The text also includes detailed placards and markings diagrams, establishing the exact configuration for instrument panel layouts and exterior safety decals. Service limits and environmental requirements, such as the 1200 dpi resolution for print output and 24 VDC electrical architecture, are documented throughout the reference sections. A 667-page Cessna 210K, T210K, 210L, and T210L OEM illustrated parts catalog detailing serial-specific components, structural assembly breakdowns, and finish identification for 1970–1975 Centurion models.
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