26.332 Identification of changes affecting fatigue critical
structure
(a) A holder of a change approval shall:
(i) review the changes and shall identify those changes that affect fatigue-critical baseline structure;
(ii) for each change identified in accordance with paragraph (a)(i), identify any associated FCMS;
(iii) identify the published repairs affecting each change identified in accordance with paragraph (a)(i).
(b) The holder of a change approval that was issued on or after 1 September 2003, shall develop and submit a list of the changes and FCMS identified in accordance with paragraphs (a)(i) and (a)(ii) to the Agency before 26 February 2022, for approval, and, upon approval by the Agency, make the list available to persons and operators required to comply with paragraph (b)(ii) of point 26.370.
(c) The holder of a change approval that was issued before 1 September 2003 shall:
(i) develop and submit a list of the changes identified in accordance with paragraph (a)(i)to the Agency before 26 February 2022, for approval;
(ii) upon request of an operator required to comply with point 26.370(a)(ii) for a change, identify and list any FCMS associated with the change and submit this data to the Agency within 12 months from the operators request, for approval;
(iii) upon approval of any data submitted according to paragraphs (c)(i) and
(c)(ii), make that data available to persons and operators required to comply
with paragraph (b)(ii) of point 26.370.
EASA Airworthiness: Fatigue Critical Structure Changes Change approval holders must identify modifications impacting aircraft's fatigue-critical structures and associated fatigue control measures. Lists of these changes, including repairs, must be submitted to EASA for approval and made available to relevant parties, ensuring continued airworthiness and safety.
* Summary by Aviation.Bot - Always consult the original document for the most accurate information.
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