5.
For the purpose of CAR - M, a document equivalent to a CA Form 1 may be:

-
    EASA Form ONE

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    FAA Form 8130-3

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    Any other form acceptable to DGCA.

6.  Any item in storage without a CA Form 1 or equivalent cannot be installed on aircraft registered in India unless a CA Form 1 or equivalent is issued for such item by an appropriately approved maintenance organisation in accordance with AMC M.A.613 (a)
AMC M.A.501 (b) – Installation
1.  
The CA Form 1 identifies the airworthiness and eligibility status of an aircraft component. Block 13 "Remarks" on the CA Form 1 in some cases contains vital airworthiness related information (see also CAR M Appendix II) which may need appropriate and necessary actions

2.  
The fitment of a replacement components/material should only take place when the person referred to under M.A.801 or the M.A. Subpart F maintenance organisation is satisfied that

Rev 0, dated 2nd March, 2010
 Section-2 CAR M such components/material meet required standards in respect of manufacture or maintenance, as appropriate.
3.  The person referred to under M.A.801 or the M.A. Subpart F approved maintenance organisation should be satisfied that the component in question meets the approved data/standard, such as the required design and modification standards. This may be accomplished by reference to the TC holder or manufacturer's parts catalogue or other approved data (i.e. SB). Care should also be exercised in ensuring compliance with applicable AD and the status of any service life limited parts fitted to the aircraft component.
AMC M.A.501(c) – Installation
1.  
Standard parts are parts manufactured in complete compliance with an established industry, DGCA or other Government specification which includes design, manufacturing, test and acceptance criteria, and uniform identification requirements. The specification should include all information necessary to produce and verify conformity of the part. It should be published so that any party may manufacture the part. Examples of specifications are National Aerospace Standards (NAS), Army-Navy Aeronautical Standard (AN), Society of Automotive Engineers (SAE), SAE Sematec, Joint Electron Device Engineering Council, Joint Electron Tube Engineering Council, and American National Standards Institute (ANSI), EN Specifications etc…

2.  
To designate a part as a standard part the TC holder may issue a standard parts manual accepted by competent authority of original TC holder or may make reference in the parts catalogue to a national/international specification (such as a standard diode/capacitor etc) not being an aviation only specification for the particular part.

3.  
Documentation accompanying standard parts should clearly relate to the particular parts and contain a conformity statement plus both the manufacturing and supplier source. Some material is subject to special conditions such as storage condition or life limitation etc. and this should be included on the documentation and / or material packaging.

4.  
A CA Form 1 or equivalent is not normally issued and therefore none should be expected.

AMC M.A.501 (d) – Installation
1.  
Consumable material is any material which is only used once, such as lubricants, cements, compounds, paints, chemicals dyes and sealants etc.

2.  
Raw material is any material that requires further work to make it into a component part of the aircraft such as metals, plastics, wood, fabric etc.

3.  
Material both raw and consumable should only be accepted when satisfied that it is to the required specification. To be satisfied, the material and or its packaging should be marked with the specification and where appropriate the batch number.
　
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