CESSNA 414A — Airworthiness Directives

This document is an Airworthiness Directive (AD) issued by the Federal Aviation Administration (FAA) concerning specific safety issues related to Cessna Aircraft Company airplanes, particularly the Model 414A. The directive was prompted by reports of an asymmetrical flap condition in the Model 414A, which could lead to loss of control during flight. The AD mandates inspections and modifications to the flap control system to ensure safety and compliance. It applies to all Cessna 414A airplanes modified by a specific Supplemental Type Certificate (STC) and outlines the necessary actions to be taken by aircraft operators to mitigate the identified risks.

• Effective date of the AD is December 26, 2012.
• Inspection of the flap control system must be completed within 60 days of the effective date.
• If damage is found, repairs and modifications must be completed before further flight.
• If no damage is found, modifications must be completed within 180 days after the effective date.
• Estimated cost for compliance is $3,125 per aircraft.