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AMC1 21.A.139(d)(2) Production management system
Available versions for ERULES-1963177438-3810
ED Decision 2022/021/R
found in: Initial Airworthiness and Environmental Protection (748/2012) Part-21 Part-21L (Jul 2024)
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AMC1 21.A.139(d)(2) Production management system ED Decision 2022/021/R QUALITY SYSTEM — ELEMENTS OF THE QUALITY SYSTEM (1) The control procedures covering the elements of point [21.A.139](#_DxCrossRefBm1649096881)(d)(2) should document the standards to which the production organisation intends to work. (2) An organisation having a quality system designed to meet a recognised Standard such as ISO 9001 (relevant to the scope of approval being requested) should expand it to include at least the following additional topics, as appropriate, in order to demonstrate compliance with the requirements of Part 21: — mandatory and voluntary occurrence reporting, as required by points [21.A.3A](#_DxCrossRefBm1649096889) and [21.A.139](#_DxCrossRefBm1649096881)(c) and continued airworthiness as required by point [21.A.165](#_DxCrossRefBm1649096910)(e); — control of work occasionally performed (outside the POA facility by POA personnel); — coordination with the applicant for, or holder of, an approved design, as required by points [21.A.133](#_DxCrossRefBm1649096911)(b) and (c) and [21.A.165](#_DxCrossRefBm1649096910)(g); — issue of certifications within the scope of approval for the privileges of point [21.A.163](#_DxCrossRefBm1649096916); — incorporation of airworthiness data in production and inspection data, as required in points [21.A.133](#_DxCrossRefBm1649096911)(b) and (c) and [21.A.145](#_DxCrossRefBm1649096920)(b) — when applicable, ground test and/or production flight test of products in accordance with procedures defined by the applicant for, or holder of, the design approval; — procedures for traceability including a definition of clear criteria of which items need such traceability; traceability is defined as a means of establishing the origin of an article by reference to historical records for the purpose of providing evidence of conformity; and — personnel training and qualification procedures especially for certifying staff as required in [21.A.145](#_DxCrossRefBm1649096920)(d). (3) An organisation having a quality system designed to meet a recognised aerospace quality standard will still need to ensure compliance with all the requirements of Part 21. In all cases, the competent authority will still need to be satisfied that compliance with Part 21 is established.
##### AMC1 21.A.139(d)(2) Production management system *ED Decision 2022/021/R* **QUALITY SYSTEM — ELEMENTS OF THE QUALITY SYSTEM** (1) The control procedures covering the elements of point [21.A.139](#_DxCrossRefBm485230371)(d)(2) should document the standards to which the production organisation intends to work. (2) An organisation having a quality system designed to meet a recognised Standard such as ISO 9001 (relevant to the scope of approval being requested) should expand it to include at least the following additional topics, as appropriate, in order to demonstrate compliance with the requirements of Part 21: — mandatory and voluntary occurrence reporting, as required by points [21.A.3A](#_DxCrossRefBm485230380) and [21.A.139](#_DxCrossRefBm485230371)(c) and continued airworthiness as required by point [21.A.165](#_DxCrossRefBm485230401)(e); — control of work occasionally performed (outside the POA facility by POA personnel); — coordination with the applicant for, or holder of, an approved design, as required by points [21.A.133](#_DxCrossRefBm485230402)(b) and (c) and [21.A.165](#_DxCrossRefBm485230401)(g); — issue of certifications within the scope of approval for the privileges of point [21.A.163](#_DxCrossRefBm485230407); — incorporation of airworthiness data in production and inspection data, as required in points [21.A.133](#_DxCrossRefBm485230402)(b) and (c) and [21.A.145](#_DxCrossRefBm485230411)(b) — when applicable, ground test and/or production flight test of products in accordance with procedures defined by the applicant for, or holder of, the design approval; — procedures for traceability including a definition of clear criteria of which items need such traceability; traceability is defined as a means of establishing the origin of an article by reference to historical records for the purpose of providing evidence of conformity; and — personnel training and qualification procedures especially for certifying staff as required in [21.A.145](#_DxCrossRefBm485230411)(d). (3) An organisation having a quality system designed to meet a recognised aerospace quality standard will still need to ensure compliance with all the requirements of Part 21. In all cases, the competent authority will still need to be satisfied that compliance with Part 21 is established.