(b)
removing original part number identification;

(c)
removing data plate identification;

(d)
maintaining  a tracking  or  accountability  system,  by serial  number  or other individualised data, to record transferred unsalvageable aircraft component;

(e)
including  written procedures concerning disposal of such components  in any agreement or contract transferring such components.

NOTE: Unsalvageable components should not be released to any person or organisation that is known to return unsalvageable components back into the aviation supply system, due to the potential safety threat.
Subpart F MAINTENANCE ORGANISATION
AMC M.602 Application
An application should be made on a CAD Form 2 or equivalent acceptable to CAD.
The CAD Form 2 is valid for the application for both MCAR-M. Subpart F and MCAR-145 Organisations. Organisations applying for both approvals may do it using a single EASA Form 2. CAD Form 2G is valid for the application for MCAR-M Subpart G Organisation. 
AMC M.603 (a) Extent of Approval
The following table identifies the ATA specification 100 chapter for the category C component rating.
CLASS  RATING  ATA CHAPTERS  
COMPONENTS OTHER  THAN COMPLETE ENGINES OR APUs  
C1 Air Cond & Press  21 
C2 Auto Flight  22 
C3 Comms and Nav  23 - 34 
C4 Doors - Hatches  52 
C5 Electrical Power  24 - 33 
C6 Equipment   25 - 38 - 45 
C7 Engine – APU  49 - 71 - 72 - 73 - 74 - 75 - 76 - 77 - 78 - 79 - 80 - 81 - 82 -83 
C8 Flight Controls  27 - 55 - 57.40 - 57.50 -57.60 - 57.70 
C9 Fuel - Airframe  28 
C10 Helicopters -Rotors  62 - 64 - 66 - 67 
C11 Helicopter - Trans   63 - 65 
C12 Hydraulic  29 
C13 Instruments  31 
C14 Landing Gear  32 
C15 Oxygen  35 
C16 Propellers  61 
C17 Pneumatic  36 - 37 
C18 Protection ice/rain/fire   26 - 30 
C19 Windows   56 
C20 Structural  53 - 54 - 57.10 - 57.20 - 57.30 

AMC M.603 (b) Extent of approval
1.  
The agreement  by the  CAD for the fabrication  of parts by the approved maintenance  organisation should be formalised  through the  approval of a detailed procedure in the maintenance organisation manual.  This AMC contains principles and conditions to be taken into account for the preparation of an acceptable procedure.

2.  
Fabrication, inspection, assembly and test should be clearly within the technical and procedural capability of the approved maintenance organisation.

3.  
The approved data necessary to fabricate the part are those approved either by CAD, the TC holder, MCAR-21 design organisation approval holder, or STC holder.

4.  
Items fabricated by an approved maintenance organisation may only be used by that organisation in the course of overhaul, maintenance, modifications, or repair of aircraft or components undergoing work within its own facility. The permission to fabricate does not constitute approval for manufacture, or to supply externally and the parts do not qualify for certification on CAD Form 1. This also applies to the bulk transfer or surplus

inventory, in that locally fabricated parts are physically segregated and excluded from any delivery certification.

5.  
Fabrication of parts, modification kits etc for onward supply and/or sale may not be conducted under a MCAR-M Subpart F approval.
　
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