Document ID: chunk:federal_register_of_legislation:F2024C01027:reg:15:p8
Version: federal_register_of_legislation:F2024C01027
Segment Type: reg
Provision Reference: reg 15 (pt 8/182)
Character Range: 153037–155984

(2) and (2A):
 (a) fires caused by a system or equipment failure, malfunction, or defect;
 (b) an engine exhaust system failure, malfunction, or defect which causes damage to the engine, adjacent aircraft structure, equipment, or components;
 (c) the accumulation or circulation of toxic or noxious gases in the crew compartment or passenger cabin;
 (d) a malfunction, failure, or defect of a propeller control system;
 (e) a propeller or rotorcraft hub or blade structural failure;
 (f) flammable fluid leakage in areas where an ignition source normally exists;
 (g) a brake system failure caused by structural or material failure during operation;
 (h) a significant aircraft primary structural defect or failure caused by any self‑generating condition (for example, fatigue or corrosion);
 (i) any abnormal vibration or buffeting caused by a structural or system malfunction, defect, or failure;
 (j) an engine failure;
 (k) any structural or flight control system malfunction, defect, or failure which causes an interference with normal control of the aircraft or which derogates from the flying qualities;
 (l) a complete loss of more than one electrical power generating system or hydraulic power system during a given operation of the aircraft;
 (m) a failure or malfunction of more than one attitude, airspeed, or altitude instrument during a given operation of the aircraft.
 (6) For subregulations (1), (2) and (2A), a report must:
 (a) be given to CASA, in writing, within 3 working days after the person required to make the report becomes aware, or could reasonably be expected to have become aware, that the failure, malfunction, or defect required to be reported has occurred; and
 (b) include as much of the following information as is available and applicable:
 (i) the aircraft's serial number;
 (ii) the aircraft's registration mark;
 (iii) when the failure, malfunction, or defect is associated with an article approved under an ATSO authorisation—the article serial number and model designation, as appropriate;
 (iv) when the failure, malfunction, or defect is associated with an aircraft engine or propeller—the aircraft engine or propeller serial number, as appropriate;
 (v) identification of the product model;
 (vi) identification of the part, component, or system involved (including the part number);
 (vii) the nature of the failure, malfunction, or defect.
 (7) Whenever the investigation of an accident or service difficulty report shows that an article manufactured under an ATSO authorisation is unsafe because of a manufacturing or design defect, the manufacturer must, upon request of CASA, investigate the defect and report to CASA the results of its investigation and any action taken or proposed by the manufacturer to correct that defect.
Penalty: 25 penalty units.
 (8) If action is required to correct the defect in an article manufactured under an ATSO authorisation, the manufacturer must submit to CASA