Document ID: chunk:federal_register_of_legislation:F2024C01027:reg:15:p157
Version: federal_register_of_legislation:F2024C01027
Segment Type: reg
Provision Reference: reg 15 (pt 157/182)
Character Range: 553467–556382

design of an aeronautical product other than an aircraft engine or propeller:
 (i) a modification/repair design approval; or
 (ii) an approval taken to have been given under regulation 21.465 or 21.470; or
 (iii) an approval mentioned in regulation 21.475; or
 (iv) an approval that continues in force under regulation 202.054, 202.055 or 202.056.
Note: For the definition of modification/repair design approval, see Part 1 of the Dictionary.
Part 90 Manual of Standards means the Manual of Standards issued by CASA under regulation 90.020.
person responsible for continuing airworthiness, for an aircraft, has the meaning given by regulation 42.105.
qualified individual, for a defect in an aircraft, has the meaning given by regulation 42.350.
quality manager, for a continuing airworthiness management organisation, has the meaning given by subregulation 42.575(1).
responsibility start date, for a person and an aircraft, means the day on which the person becomes the person responsible for continuing airworthiness for the aircraft.
responsible manager:
 (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).
serviceable, in relation to an aeronautical product, has the meaning given by subregulation (6).
significant change:
 (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).
unapproved, in relation to a part, has the meaning given by regulation 42.470.
unsalvageable, in relation to an aeronautical product, has the meaning given by subregulation (7).
Note: See the Dictionary for definitions of other terms used in this Part.
 (2) An aircraft is airworthy if it is in a state that conforms with its approved design and is in a condition for safe operation.
 (3) Each of the following is a continuing airworthiness record for an aircraft:
 (a) a record made under paragraph 42.130(3)(b) for the aircraft;
 (b) a record made under Subdivision 42.C.3.2 for the aircraft;
 (c) a document kept under regulation 42.215 for the aircraft;
 (d) a record made under this Part in the flight technical log for the aircraft;
 (e) a record made by a means, other than a flight technical log, approved by CASA under regulation 42.250;
 (f) a record made under regulation 42.345 for the aircraft;
 (g) a record made under regulation 42.370 for the aircraft;
 (h) a maintenance record for maintenance carried out on the aircraft;
 (i) a certificate of release to service for an aircraft in relation to maintenance carried out on the aircraft;
 (j) a copy of the design of a modification or repair that is unique to the aircraft;
 (k) if an aircraft maintenance record was kept for the aircraft in accordance with Division 10 of