General

Where can I obtain information about Alternative Methods of Compliance (AMOC) to ADs?

Information related to AMOCs can be found on the EASA website, Airworthiness Directives page. 
In addition, please consult the AMOC FAQ page.

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Can EASA provide the service information referenced in an AD?

In principle, EASA does not provide service information as it contains proprietary information owned by the approval holder of the product, part or appliance to which the AD applies. Please contact the appropriate owner of such information, e.g. the Design Approval Holder, whose contact details can be found in the relevant AD. In exceptional cases, with the consent of the approval holder, EASA may make service information available as an attachment to the record of the AD.

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How can I identify an AD as being a State of Design AD?

In principle, an AD is a State of Design AD when the authority that issues the AD is, on the date of issuance of that AD, the State of Design authority for the products, parts or appliances (or STC modification) to which the AD applies. The Type Certificates of some products have been known to move from one  State of Design to another in the recent past, e.g. the Bell 206 and 222 helicopter types moving to Bell Helicopter Textron Canada, from the USA to Canada; the British Aerospace 125 business jet type design was sold to Raytheon (now Hawker Beechcraft Corp.), moving from the UK to the USA; and APEX sold the R 2000 type design to Alpha Aviation, moving the State of Design (responsibilities) from France to New Zealand.

Some examples:

When operating a product for which France is the State of Design, e.g. an Airbus aeroplane, or a CFM56 engine, the applicable ADs are those issued (or approved) by EASA and, previously, ADs issued by DGAC France.

When operating a product for which the USA is the State of Design, e.g. a Boeing aeroplane, or a General Electric engine, the applicable ADs are those issued by the Federal Aviation Administration (FAA).

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Am I required to comply with ADs published on the EASA website?

The answer to this question depends on where (in which country)  the aircraft is registered, or on the specific agreement existing between the Authority of the State of Registry and the State of the affected operator. In principle, the regulations of the State of Registry of an aircraft determine which ADs apply to that aircraft (including the engine, propeller, parts and appliances). In nearly all cases, ICAO Annex 8, Chapter 4 guidelines are applied, which means that the State of Design ADs (see definition above) apply.

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Where can I find a State of Design AD issued before 28 September 2003 (start date of EASA) if it is not in the Safety Publications Tool?

All ADs issued by the State of Design (SoD) Authorities before 28 September 2003 should be retrieved from the relevant SoD websites.  Please consult the list of Useful links on the EASA Airworthiness Directives page.

SoD ADs issued before 28 September 2003 are progressively uploaded to the EASA Safety Publications Tool by the Safety Information Section. Once this upload is finished, an announcement will be made on the  EASA Airworthiness Directives webpage.

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What are the applicable ADs in EASA Member States (European Union and some associated countries) for a specific product, part or appliance?

ADs applicable to an EASA approved design (products, parts or appliances) are those ADs which have been issued or adopted by the Agency by way of:

  • ADs issued by the Agency through Agency decisions,
  • ADs issued by Foreign State of Design Authorities (Non-EASA Member States) and adopted by the Agency by way of: 
    • for ADs issued before 28 September 2003 (start date of EASA):
      Commission Regulation (EU) No 748/2012, Article 3, Paragraph 1 (a) (iii) 
      (ADs issued by the State of Design for products, parts and appliances);
    • for ADs issued after 28 September 2003 (start date of EASA): 
      ED Decision 02/2003 on the implementation of airworthiness directives for products, parts and appliances designed in third countries.

Note: One-time actions (inspection, repair, modification, etc.) accomplished before 28 September 2003, based on (i.e. required by) an AD issued by an EASA State of Registry authority, in deviation from a State of Design AD, remain ‘valid’ in the sense that such actions constitute compliance with the State of Design AD for the same subject. Repetitive actions, previously required by an AD issued by an EASA State of Registry authority, must be continued after 28 September 2003 as required by the State of Design AD for the same subject. Each AD issued before 28 September 2003 by an EASA State of Registry authority, in the absence of a State of Design AD (also identified as ‘additional’ AD), is no longer valid from 28 September 2003 (i.e. cannot be enforced anymore).

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Are Foreign State of Design (non-EASA Member States) ADs that are not available in the Safety Publishing Tool applicable in Europe?

Commission Regulation (EU) No 748/2012, Article 3, paragraph 1 (a) (iii) specifies that “the applicable airworthiness directives were those of the State of design”. 
This means that all ADs issued by the State of Design before 28 September 2003 (start date of EASA), either applicable to European or non-European products (i.e. aircraft, engines, propellers), parts or appliances (or STC modifications),  have been adopted by EASA under that Regulation.

As a result, all ADs issued by the State of Design authority for the affected product(s), part(s) or appliance(s) are valid in Europe, unless EASA has issued a different decision. 
Commission Regulation (EU) No 1321/2014, M.A.301, paragraph 5 (i) requires that the “aircraft continuing airworthiness […] shall be ensured by […] the accomplishment of any applicable airworthiness directive”, as identified by Regulation (EU) 748/2012.
All Foreign State of Design ADs issued after 28 September 2003 have been (and still are) ‘automatically’ adopted by EASA under the provisions of EASA Executive Director’s ED Decision 02/2003. This decision implies that any AD issued by the State of Design authority for the products, parts or appliances (or STC modification) to which that AD applies, becomes valid in Europe upon the day that AD becomes effective, unless the Agency issues a different decision (e.g. deviating AD, or statement of non-adoption) before that AD becomes effective. This decision applies to all State of Design ADs, not only those issued by the FAA.

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Can the information provided on EASA's FAQ be considered as legally binding?

EASA is not the competent authority to interpret EU Law. The responsibility to interpret EU Law rests with the judicial system, and ultimately with the European Court of Justice. EASA cannot even provide an 'authentic interpretation' (which is an official interpretation of a statute issued by the statute's legislator). Therefore any information included in these FAQs shall only be considered as EASA's understanding on a specific matter, and cannot be considered in any way as legally binding.

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