GM1 21.B.225(b) Findings and corrective actions

• ED Decision 2023/014/R found in: Initial Airworthiness and Environmental Protection (748/2012) Part-21 Part-21L (Jul 2024)

GM1 21.B.225(b) Findings and corrective actions; observations ED Decision 2023/014/R EXAMPLE OF A LEVEL 1 FINDING The production organisation cannot demonstrate compliance with [21.A.139](#_DxCrossRefBm1649096881)(d)2.(xii) and [21.A.163](#_DxCrossRefBm1649096916)(c), as evidenced by: The POA holder released the ‘critical’ Part No XXX, Serial Number YYY with  EASA Form 1 No ZZZZ having ticked the box *‘Certifies that the items identified above were manufactured in conformity to: approved design data and are in a condition for safe operation’;* while: (a)     the released part is not included in the organisation’s capability list/scope of work; and/or (b)     the POA holder could not demonstrate that the released part is covered by an EASA approved/accepted type design. Consequently, the released part is not eligible for installation on in-service type-certificated aircraft. ##### GM1 21.B.225(b) Findings and corrective actions; observations *ED Decision 2023/014/R* **EXAMPLE OF A LEVEL 1 FINDING** The production organisation cannot demonstrate compliance with [21.A.139](#_DxCrossRefBm485230371)(d)2.(xii) and [21.A.163](#_DxCrossRefBm485230407)(c), as evidenced by: The POA holder released the ‘critical’ Part No XXX, Serial Number YYY with  EASA Form 1 No ZZZZ having ticked the box *‘Certifies that the items identified above were manufactured in conformity to: approved design data and are in a condition for safe operation’;* while: (a) the released part is not included in the organisation’s capability list/scope of work; and/or (b) the POA holder could not demonstrate that the released part is covered by an EASA approved/accepted type design. Consequently, the released part is not eligible for installation on in-service type-certificated aircraft.