ANNEX IISupplementary provisions
ANNEX II Annex II (Part-145) to Commission Regulation (EU) No 1321/2014 is amended as follows: (1) point 145.A.42 is amended as follows: (i) point (a)(i) is replaced by the following: ‘(i) Components which are in a satisfactory condition, released on an EASA Form 1 or equivalent and marked in accordance with Subpart Q of Annex I (Part 21) or, as applicable, Subpart Q of Section A of Annex Ib (Part 21 Light) to Regulation (EU) No 748/2012, unless otherwise specified in point 21.A.307 of Annex I (Part 21) or point 21L.A.193 of Annex Ib (Part 21 Light) to Regulation (EU) No 748/2012, in point M.A.502 of Annex I (Part-M), in point ML.A.502 of Annex III (Part-ML), or in this Annex (Part-145).’; (ii) point (b)(iv) is replaced by the following: ‘(iv) Components which are referred to in point (b)(2) of point 21.A.307 of Annex I (Part 21) or in point (b)(2) of point 21L.A.193 of Annex Ib (Part 21 Light) to Regulation (EU) No 748/2012 shall only be installed if considered eligible for installation by the aircraft owner on their own aircraft.’; (2) point (b) of point 145.A.60 is replaced by the following: ‘(b) The organisation shall report to its competent authority and to the organisation responsible for the design of the aircraft or component: (i) any safety-related event or condition of an aircraft or component identified by the organisation which endangers or, if not corrected or addressed, could endanger an aircraft, its occupants or any other person; and (ii) in particular any accident or serious incident.’