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This document is an Emergency Airworthiness Directive issued by EASA regarding specific checks and inspections required for EC 225 helicopters to ensure their airworthiness related to the epicyclic
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How to fill out easa ad no 2012-0144-e

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How to fill out EASA AD No.: 2012-0144-E

01
Begin by reading the full text of EASA AD No.: 2012-0144-E to understand its scope.
02
Identify the specific aircraft and engine models that are affected by the AD.
03
Gather the documentation required to demonstrate compliance, such as maintenance records and inspection checklists.
04
Perform the required inspections or modifications as specified in the AD.
05
Document all actions taken to comply with the AD, including dates, findings, and any corrective actions.
06
Ensure that the compliance documentation is maintained in the aircraft's records.
07
Report compliance status to the relevant authorities if required.

Who needs EASA AD No.: 2012-0144-E?

01
All operators of the aircraft and engine models listed in the AD.
02
Maintenance organizations responsible for performing inspections and repairs on the affected aircraft.
03
Regulatory authorities overseeing aviation safety and compliance.
04
Aircraft owners who are responsible for ensuring their aircraft meet safety regulations.
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People Also Ask about

Definition. Airworthiness Directive (AD). A regulatory document which identifies aeronautical products in which an unsafe condition exists, and where the unsafe condition is likely to exist or develop in other aeronautical products of the same type design.
The working language in EASA is English.
European Union Aviation Safety Agency (EASA)
An AD is published by an airworthiness authority and requires mandatory actions within prescribed periods. EASA ADs are defined in Regulation (EU) 748/2012, Part 21. A. 3B. Whether anyone must comply with an AD, see our related AD FAQ.
Airworthiness Directive (AD) - Content & Format. Airworthiness Directives (ADs) consist of two parts, the preamble and the rule. The preamble provides the basis and purpose of the AD. The rule portion provides regulatory requirements for correcting the unsafe condition.
The FAA issues Airworthiness Directives (ADs) and aircraft manufacturers issue Service Bulletins (SBs). ADs are legally enforceable regulations, in accordance with 14 CFR part 39, to correct an unsafe condition that exists in a product. Compliance with an AD is mandatory for continued airworthiness.
The EASA Form 1 is the Authorised Release Certificate that declares the airworthiness of products, parts, and appliances. It states that a product, a part, or a component was manufactured in accordance with approved design data. This is an important aspect of the airworthiness regulations.
Airworthiness Directive (AD) A document issued or adopted by the Agency which mandates actions to be performed on an aircraft to restore an acceptable level of safety, when evidence shows that the safety level of this aircraft may otherwise be compromised.

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EASA AD No.: 2012-0144-E is an Airworthiness Directive issued by the European Union Aviation Safety Agency (EASA) aimed at addressing safety concerns related to specific aircraft or components. It outlines necessary inspections, modifications, or limitations to ensure continued airworthiness.
Operators and owners of the affected aircraft are required to comply with EASA AD No.: 2012-0144-E. This includes airlines, charter companies, and private operators that are using the specified aircraft or components outlined in the directive.
To fill out EASA AD No.: 2012-0144-E, operators should gather the required information concerning the affected aircraft or components, complete the compliance actions described in the directive, and document the actions taken in a maintenance log or appropriate report as specified by EASA.
The purpose of EASA AD No.: 2012-0144-E is to mitigate risks associated with specific safety deficiencies identified in certain aircraft or components, thereby ensuring the safety of operations and protecting against potential incidents.
Operators must report compliance status, details of any inspections or modifications performed, and any discrepancies noted during compliance actions. This documentation should be submitted to the relevant aviation authority as per the instructions outlined in the AD.
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