2.
In the case of components in storage prior to CAR145, CAR M and CAR 21 and not released on a CA Form 1 or equivalent in accordance with M.A.501(a) or removed serviceable from active aircraft which have been withdrawn from service, this paragraph
provides additional guidance regarding the conditions under which a CA Form 1 may be issued .
2.1 A CA Form 1 may be issued for an aircraft component which has been:
.
released without a CA Form 1 or equivalent
.
Used on an aircraft and removed in a serviceable condition. Examples include leased and loaned aircraft components.
.
Removed from aircraft which have been withdrawn from service, or from aircraft which have been involved in abnormal occurrences such as accidents, incidents, heavy landings or lightning strikes.
.
Components maintained by an unapproved organisation.
2.2. An appropriately rated M.A. Subpart F maintenance organisation may issue a CA Form 1 as detailed in this AMC sub-paragraph 2.5 to 2.9, as appropriate, in accordance with procedures detailed in the manual as approved by DGCA. The appropriately rated M.A. Subpart F maintenance organisation is responsible for ensuring that all reasonable measures have been taken to ensure that only approved and serviceable aircraft components are issued a CA Form 1 under this paragraph.
2.3. For the purposes of this paragraph 2 only, appropriately rated means an organization with an approval class rating for the type of component or for the product in which it may be installed.
2.4. A CA Form 1 issued in accordance with this paragraph 2 should be issued by
Rev 0, dated 2nd March, 2010
Section-2 CAR M signing in block 20 and stating "Inspected" in block 12. In addition, block 13 should specify:
2.4.1. when the last maintenance was carried out and by whom;
2.4.2. if the component is unused, when the component was manufactured and by whom with a cross reference to any original documentation which should be included with the Form;
2.4.3. a list of all airworthiness directives, repairs and modifications known to have been incorporated. If no airworthiness directives or repairs or modifications are known to be incorporated then this should be so stated.
2.4.4. detail of life used for service life limited parts being any combination of fatigue, overhaul or storage life;
2.4.5. for any aircraft component having its own maintenance history record, reference to the particular maintenance history record as long as the record contains the details that would otherwise be required in block 13. The maintenance history record and acceptance test report or statement, if applicable, should be attached to the CA Form 1.
2.5. New / unused aircraft components
2.5.1 Any unused aircraft component in storage without a CA Form 1 up to the effective date(s) for CAR 21 that was manufactured by an organisation acceptable to DGCA at the time may be issued a CA Form 1 by an appropriately rated maintenance organisation approved under M.A. Subpart
F. The CA Form1 should be issued in accordance with the following subparagraphs which should be included in a procedure within the maintenance organisation manual.
Note 1: It should be understood that the release of a stored but unused aircraft component in accordance with this paragraph represents a maintenance release under M.A. Subpart F and not a production release under CAR
21. It is not intended to bypass the production release procedure agreed by DGCA for parts and subassemblies intended for fitment on the manufacturers own production line.
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