CESSNA 210 — Maintenance Manual

This document is a maintenance manual revision for the Cessna 210 series aircraft, published by Cessna Aircraft Co. on February 10, 2014. It introduces a new section titled 'Airworthiness Limitations' (ALS), which outlines mandatory inspection intervals and replacement times for critical components of the aircraft. The document emphasizes the regulatory implications of the ALS, particularly in relation to FAA regulations that govern aircraft maintenance. It is intended for aircraft owners, maintenance personnel, and aviation enthusiasts who need to understand the compliance requirements associated with the Cessna 210. The manual highlights the importance of adhering to the ALS to ensure airworthiness and safety in operations.

• Initial eddy-current inspection of wing main spar lower caps required at 8,000 hours.
• Recurring inspections for wing spars every 2,000 hours thereafter.
• For severe environments, inspections required at 3,500 hours and every 500 hours thereafter.
• P210 models have a life limit of 13,000 hours on specific components including windows and ice light lens.
• Compliance with the ALS is mandatory as per FAA regulations.