Under which regulation and annex is a declaration of design compliance made that would make the declarant the responsible design organisation for occurrence reporting?

The declaration of design compliance is made under Subpart C of Annex Ib (Part 21 Light) to Regulation (EU) No 748/2012.

Who can be considered the organisation responsible for the design of an aircraft or component in the context of occurrence reporting?

Depending on the case, the organisation responsible for the design can be (a) the 'design approval holder' (e.g., holder of a type certificate, restricted type certificate, supplemental type certificate, ETSO authorisation, major repair design approval, major change design approval, or any other relevant approval or authorisation for products, parts and appliances deemed issued under Regulation (EU) No 748/2012), or (b) the declarant of a declaration of design compliance made under Subpart C of Annex Ib (Part 21 Light) to Regulation (EU) No 748/2012.

GM1 145.A.60(b) Occurrence reporting

Q: Which specific approvals or authorisations qualify a holder as a 'design approval holder' for occurrence reporting purposes?

A 'design approval holder' may be the holder of a type certificate, a restricted type certificate, a supplemental type certificate, a European Technical Standard Order (ETSO) authorisation, a major repair design approval, a major change design approval, or any other relevant approval or authorisation for products, parts and appliances deemed to have been issued under Commission Regulation (EU) No 748/2012.

Q: Does the definition of 'design approval holder' include holders of approvals issued under regulations other than Commission Regulation (EU) No 748/2012?

No, the text specifies that the approvals or authorisations are deemed to have been issued under Commission Regulation (EU) No 748/2012. It does not mention approvals under other regulations.

Navigate / EASA

Ask question Discover more Add to collection

GM1 145.A.60(b) Occurrence reporting

ED Decision 2023/013/R

Depending on the case, the organisation responsible for the design of the aircraft or component can be:

(a) the ‘design approval holder’: it may be the holder of a type certificate, a restricted type certificate, a supplemental type certificate, a European Technical Standard Order (ETSO) authorisation, a major repair design approval, a major change design approval or any other relevant approval or authorisation for products, parts and appliances deemed to have been issued under Commission Regulation (EU) No 748/2012;

(b) the declarant of a declaration of design compliance made under Subpart C of Annex Ib (Part 21 Light) to Regulation (EU) No 748/2012.

Details

Source-Title: GM1 145.A.60(b) Occurrence reporting View latest amendments

Erulesid: ERULES-1963177438-20047 Compare versions

Domain: Continuing airworthiness

Aircraftuse: Used by licensed air carrier (LAC), Used by private operator or for limited operations

Aircraftcategory: Complex motor-powered aircraft (CMPA), Non-complex motor-powered aircraft (non-CMPA)

Applicabilitydate: 21 October, 2023

Entryintoforcedate: 21 October, 2023

Registrystate: EU-registered, Non-EU registered

Regulatorysource: ED Decision 2023/013/R Navigate

Regulatorysubject: Part-145

Typeofcontent: GM to IR (Guidance material to implementing rule)

Parentir: 145.A.60 Occurrence reporting

Origin: EASA

Category: EAR