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Division ML.A.501 Classification and installationF1X1

United Kingdom

Original text. Later amendments are not shown.

  1. (a)

    Unless otherwise specified in Subpart F of Annex I (Part-M), Annex II (Part-145), Annex Vd (Part-CAO) to this Regulation F2or in point 21.A.307 of Annex I (Part-21) to Regulation (EU) No 748/2012, component may be fitted only if all of the following conditions are met:

    1. (i)

      it is in a satisfactory condition;

    2. (ii)

      has been appropriately released to service using F3a CAA Form 1 as set out in Appendix II of Annex I (Part-M), or equivalent;

    3. (iii)

      has been marked in accordance with Subpart Q of Annex I (Part-21) to Regulation (EU) No 748/2012.

  2. (b)

    Prior to the installation of a component on an aircraft, the person or approved maintenance organisation shall ensure that the particular component is eligible to be fitted if different modifications or AD configurations are applicable.

  3. (c)

    Standard parts shall only be fitted to an aircraft or component when the maintenance data specifies those particular standard parts. Standard parts shall only be fitted when accompanied by evidence of conformity to the applicable standard and has appropriate traceability.

  4. (d)

    Raw or consumable material shall only be used on an aircraft or component provided that:

    1. (i)

      the aircraft or component manufacturer allows for the use of raw or consumable material in relevant maintenance data or as specified in Subpart F of Annex I (Part-M), Annex II (Part-145) or Annex Vd (Part-CAO).

    2. (ii)

      such material meets the required material specification and has appropriate traceability.

    3. (iii)

      such material is accompanied by documentation clearly relating to the particular material and containing a conformity-to-specification statement as well as the manufacturing and supplier source.

  5. (e)

    In case of balloons, where different combinations of baskets, burners and fuel cylinders are possible for a particular envelope, the person installing them shall ensure that:

    1. (1)

      the basket, burner and/or fuel cylinders are eligible for installation according to the TCDS or other documents referred to in the TCDS;

    2. (2)

      the basket, burner and/or fuel cylinders are in serviceable condition and have the appropriate maintenance records.

Annotations

Textual amendments

F1

Inserted by Commission Implementing Regulation (EU) 2019/1383 of 8 July 2019 amending and correcting Regulation (EU) No 1321/2014 as regards safety management systems in continuing airworthiness management organisations and alleviations for general aviation aircraft concerning maintenance and continuing airworthiness management (Text with EEA relevance).

F2

Words in Annex 5b point ML.A.501(a) substituted (1.7.2024) by The Aviation Safety (Amendment) Regulations 2023 (S.I. 2023/588), regs. 1(3), 29(3)(a)

F3

Words in Annex 5b point ML.A.501 substituted (31.12.2020) by The Aviation Safety (Amendment) (EU Exit) Regulations 2020 (S.I. 2020/1116), regs. 1(2), 76(7)(a)

Editorial notes

X1

Inserted by Corrigendum to Commission Implementing Regulation (EU) 2019/1383 of 8 July 2019 amending and correcting Regulation (EU) No 1321/2014 as regards safety management systems in continuing airworthiness management organisations and alleviations for general aviation aircraft concerning maintenance and continuing airworthiness management (Official Journal of the European Union L 228 of 4 September 2019).

Notes on Division

Textual amendments

F2

Annex 5b point ML.1(b) omitted (31.12.2020) by virtue of The Aviation Safety (Amendment) (EU Exit) Regulations 2020 (S.I. 2020/1116), regs. 1(2), 76(3)(a)

F3

Words in Annex 5b point ML.1(c) substituted (31.12.2020) by The Aviation Safety (Amendment) (EU Exit) Regulations 2020 (S.I. 2020/1116), regs. 1(2), 76(3)(b)