CESSNA TURBO 210L — Airworthiness Directives

This document is an Airworthiness Directive (AD) issued by the Federal Aviation Administration (FAA) concerning the Cessna Turbo 210L. It outlines mandatory inspection and modification procedures for the turbocharger and its components to ensure safety and compliance with federal regulations. The directive is aimed at aircraft operators and maintenance personnel, providing essential guidelines to prevent potential failures that could compromise flight safety. The AD emphasizes the importance of adhering to the specified compliance dates and procedures to maintain airworthiness standards.

• Inspect turbocharger components as per Cessna Service Kit SK 210-78.
• Replace turbocharger center housing if not done according to AD 77-06-02.
• Operators may fly to a maintenance location under FAR 21.197.
• Compliance with this AD is mandatory by April 6, 1978.
• Alternative compliance methods require FAA approval.