(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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