Document ID: chunk:federal_register_of_legislation:F2024C01027:reg:15:p49
Version: federal_register_of_legislation:F2024C01027
Segment Type: reg
Provision Reference: reg 15 (pt 49/182)
Character Range: 265985–268854

or thrust, including, for engines having a rated take‑off power or thrust higher than rated maximum continuous power or thrust, 30 minutes at rated take‑off power or thrust.
Penalty: 25 penalty units.
 (2) The test runs required by subregulation (1) may be made with the engine appropriately mounted and using current types of power and thrust measuring equipment.
 (3) A person manufacturing rocket engines under a type certificate only must establish a sampling technique for testing the engines.
Penalty: 25 penalty units.
 (4) An offence against subregulation (1) or (3) is an offence of strict liability.
Note: For strict liability, see section 6.1 of the Criminal Code.
Source FARs section 21.128 modified.

21.129  Tests: variable pitch propellers
 (1) Each person manufacturing variable pitch propellers under a type certificate only must give each propeller an acceptable functional test to determine if it operates properly throughout the normal range of operation.
Penalty: 25 penalty units.
 (2) An offence against subregulation (1) is an offence of strict liability.
Note: For strict liability, see section 6.1 of the Criminal Code.
Source FARs section 21.129 modified.

21.130  Statement of conformity
 (1) Each holder or licensee of a type certificate for a type of aircraft, aircraft engine or propeller must give CASA a statement of conformity, in a form acceptable to CASA, for each aircraft, aircraft engine or propeller manufactured under the type certificate only:
 (a) when the holder or licensee applies for the original issue of an aircraft certificate of airworthiness or an aircraft engine or propeller authorised release certificate for the aircraft, aircraft engine or propeller; or
 (b) if the holder or licensee transfers the ownership of the aircraft, aircraft engine or propeller without applying for an authorised release certificate for it—when the ownership of the aircraft, aircraft engine or propeller is transferred.
 (2) The statement of conformity must be signed by a person who holds a responsible position in the manufacturing organisation and has been authorised by the manufacturer to sign the statement, and must include:
 (a) for each aircraft, aircraft engine or propeller, a statement that it conforms to its type certificate and is in a condition for safe operation; and
 (b) for each aircraft, a statement that the aircraft has been flight checked; and
 (c) for each aircraft engine or variable pitch propeller, a statement that the engine or propeller has been subjected by the manufacturer to a final operational check.
 (3) However, in the case of an aircraft, aircraft engine or propeller manufactured for the Defence Force, or for an armed force of Canada, the United Kingdom or the United States of America, a statement of conformity is not required if the aircraft, aircraft engine or propeller has been accepted