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This Airworthiness Directive addresses issues with the alternator fail indication system in DA 42 NG and DA 42 M-NG aeroplanes, highlighting necessary modifications to ensure electrical system safety.
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How to fill out EASA AD No.: 2013-0224

01
Review the EASA AD No.: 2013-0224 document to understand its content and requirements.
02
Identify the affected aircraft and components as specified in the AD.
03
Gather all necessary tools and materials required for compliance with the AD.
04
Follow the step-by-step instructions outlined in the AD for performing inspections or repairs.
05
Document all actions taken to comply with the AD, including any findings or corrective actions.
06
Submit the required reports and notifications to the relevant authorities if specified in the AD.

Who needs EASA AD No.: 2013-0224?

01
Operators and maintenance organizations of the affected aircraft models.
02
Aircraft owners who have the specified components installed.
03
Aviation regulatory bodies that oversee compliance with airworthiness directives.
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EASA AD No.: 2013-0224 is an Airworthiness Directive issued by the European Union Aviation Safety Agency (EASA) to address safety concerns related to specific aircraft models or components.
Operators, owners, and maintenance organizations of the affected aircraft or components are required to comply with and file EASA AD No.: 2013-0224.
To fill out EASA AD No.: 2013-0224, the reporting entity must provide specific details regarding the aircraft or component, compliance status, and any corrective actions taken.
The purpose of EASA AD No.: 2013-0224 is to mitigate safety risks by ensuring that necessary inspections or modifications are conducted to enhance the operational safety of affected aircraft.
The information that must be reported includes detailed identification of the aircraft or component, findings of any inspections, actions taken to address issues, and compliance with the directive.
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