Installation and Disposal of Life-limited Parts
571.09 (1) No person shall install a used life-limited part on an aeronautical product unless the part meets the standards of airworthiness applicable to the installation of life-limited parts and
(a) the technical history of the part within the meaning of section 571.09 of the Airworthiness Manual is available to show that the time in service authorized for that part in the type certificate governing the installation has not been exceeded; and
(b) the history referred to in paragraph (a) is incorporated into the technical record for the aeronautical product on which the part is installed.
(2) No person shall install a used life-limited part in a place other than that from which it was removed unless the part is installed
(a) in the same or in an identical position on another aeronautical product bearing the same part number as that from which the part was removed; or
(b) in conformity with the requirements in respect of technical data that have been approved or the use of which has been approved within the meaning of section 571.09 of the Airworthiness Manual.
(3) When a life-limited part has reached the time in service authorized in its type design, the part shall be
(a) rendered unusable; or
(b) identified as not airworthy and kept segregated from airworthy parts.
- SOR/2002-112, s. 10.
571.10 (1) No person shall sign a maintenance release required pursuant to section 605.85 or permit anyone whom the person supervises to sign a maintenance release, unless the standards of airworthiness applicable to the maintenance performed and stated in Chapter 571 of the Airworthiness Manual have been complied with and the maintenance release meets the applicable requirements specified in section 571.10 of the Airworthiness Manual.
(2) Except as provided in subsection (4), a maintenance release shall include the following, or a similarly worded, statement:
“The described maintenance has been performed in accordance with the applicable airworthiness requirements.”
(3) No maintenance release is required in respect of any task designated as elementary work in the Aircraft Equipment and Maintenance Standards that is performed by
(a) in the case of a glider, a balloon or an unpressurized small aircraft that is powered by a piston engine and not operated pursuant to Part IV or VII, the pilot of the aircraft;
(b) in the case of an aircraft operated under Part IV or VII, a person who has been trained and authorized in accordance with the flight training unit’s or the air operator’s maintenance control manual (MCM), approved under Subpart 6 of Part IV or of Part VII, respectively; or
(c) in the case of an aircraft operated pursuant to Subpart 4 of Part VI, a person who has been trained in accordance with those sections of a private operator’s operations manual that contain details of the operator’s maintenance control system.
(4) Where a person signs a maintenance release in respect of maintenance performed on an aircraft, the satisfactory completion of which cannot be verified by inspection or testing of the aircraft on the ground, the maintenance release shall be made conditional on the satisfactory completion of a test flight carried out pursuant to subsections 605.85(2) and (3), by the inclusion of the phrase “subject to satisfactory test flight”.
(5) No person shall sign a maintenance release in respect of specialized maintenance unless the requirements of section 571.04 have been met.
- SOR/2000-404, s. 8;
- SOR/2003-154, s. 6(F).
- Date modified: