Document ID: chunk:federal_register_of_legislation:F2024C01027:reg:15:p155
Version: federal_register_of_legislation:F2024C01027
Segment Type: reg
Provision Reference: reg 15 (pt 155/182)
Character Range: 548188–551153

issued by a Part 145 organisation—the authorisation reference number allocated to the authorisation by the organisation in accordance with the Part 145 Manual of Standards.
competent, to carry out maintenance on an aircraft or aeronautical product, has the meaning given by subregulation 42.315(1).
configuration deviation list, for an aircraft, means a document that:
 (a) is prepared by the aircraft's type certificate holder or foreign type certificate holder; and
 (b) is approved by the State of Design for the aircraft; and
 (c) lists each external part of the aircraft that is permitted to be missing from the aircraft, under conditions specified in the document, at the commencement of a flight by the aircraft.
continuing airworthiness management service has the meaning given by subregulation 42.575(1).
continuing airworthiness manager, for a continuing airworthiness management organisation, has the meaning given by subregulation 42.575(1).
continuing airworthiness record, for an aircraft, has the meaning given by subregulation (3).
continuing airworthiness records system, for an aircraft, means the system required by regulation 42.170 for the aircraft.
continuing airworthiness responsibility, for a continuing airworthiness management organisation, has the meaning given by subregulation 42.575(1).
creation date has the meaning given by subregulation 42.260(2).
critical control system maintenance, for an aircraft:
 (a) means maintenance carried out on the aircraft control system for the aircraft that, if not carried out correctly, may result in a failure, malfunction or defect of the system that will endanger the safe operation of the aircraft; and
 (b) does not include optional dual flight control maintenance.
eligible to be fitted, for a part, has the meaning given by subregulation (4).
eligible to be used, for a material, has the meaning given by subregulation (5).
exposition:
 (a) for a Subpart 42.F organisation—has the meaning given by subregulation 42.500(1); and
 (b) for a continuing airworthiness management organisation—has the meaning given by subregulation 42.575(1); and
 (c) for a Part 145 organisation—has the meaning given by subregulation 145.010(1).
independent individual, for critical control system maintenance for an aircraft, has the meaning given by regulation 42.335.
independent maintainer means an individual mentioned in item 1, 3, 4 or 5 of table 42.300.
life limit, for an aeronautical product that is fitted, or is to be fitted, to an aircraft or another aeronautical product (the second aeronautical product), means:
 (a) if an airworthiness directive specifies an amount of use, or an age, after which the product must not be used—that amount of use, or age; or
 (b) if paragraph (a) does not apply, and the approved design for the aircraft specifies an amount of use, or an age, after which the product must not be used—that amount of use, or age; or
 (c) if paragraphs (a) and (b) do not apply, and