ML.A.501
Classification and installation
Regulation (EU) 2019/1383, Regulation (EU) 2021/700
(a) Unless otherwise specified in Subpart F of
Annex I (Part-M),
Annex II
(Part-145), Annex Vd
(Part-CAO) to this Regulation and Annex I (Part-21) to Regulation (EU) No 748/2012,
component may be fitted only if all of the following conditions are met:
(i) it
is in a satisfactory condition;
(ii) has
been appropriately released to service using an EASA Form 1 as set out in
Appendix II of Annex I (Part-M), or equivalent;
(iii) has
been marked in accordance with Subpart Q of Annex I (Part-21) to Regulation (EU) No 748/2012.
(a) Unless
otherwise specified in Subpart F of Annex I (Part-M), in Annex II (Part-145),
in Annex Vd (Part-CAO) to this Regulation
or in point 21.A.307 of Annex I (Part 21) to Regulation (EU) No 748/2012, a
component may be fitted only if
all of the following conditions are met:
(i) it is in a satisfactory condition;
(ii) it has been appropriately released to service using an EASA
Form 1 as set out in Appendix II to Annex I (Part-M), or equivalent;
(iii) it has been marked in accordance with Subpart Q of Annex I
(Part 21) to Regulation (EU) No 748/2012.
[applicable from 18 May 2022]
(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.
(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.
(d) Raw or consumable material shall only be
used on an aircraft or component provided that:
(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).
(ii) such
material meets the required material specification and has appropriate
traceability.
(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.
(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) the basket, burner and/or fuel cylinders
are eligible for installation according to the TCDS or other documents
referred to in the TCDS;
(2) the basket, burner and/or fuel cylinders
are in serviceable condition and have the appropriate maintenance records.
EASA balloon component installation requires satisfactory condition, proper release to service (EASA Form 1 or equivalent), and correct marking. Prior to installation, eligibility must be verified, especially with modifications. Standard parts require specified maintenance data and conformity evidence. Raw materials need manufacturer approval, specification compliance, and traceability documentation. Balloon basket, burner, and fuel cylinder combinations must adhere to TCDS requirements.
* Summary by Aviation.Bot - Always consult the original document for the most accurate information.
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