马尔代夫民航法规 MCAR-M Continuing Airworthiness(51)

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An assessment of both the cause and any potentially hazardous effect of any defect or combination of defects that could affect flight safety should be made in order to initiate any necessary further investigation and analysis necessary to identify the root cause of the defect.
AMC M.403 (d) Aircraft defects
All deferred defects should be made known to the pilot/flight crew, whenever possible, prior to their arrival at the aircraft.
Deferred defects should be transferred on to worksheets at the next appropriate maintenance check, and any deferred defect which is not rectified during the maintenance check, should be re-entered on to a new deferred defect record sheet. The original date of the defect should be retained.
The necessary components or parts needed for the rectification of defects should be made available or ordered on a priority basis, and fitted at the earliest opportunity.
Subpart E COMPONENTS
AMC M.501 (a) - Installation
1.  
To ensure a component is in a satisfactory condition, the person referred to under MCAR-M.801 or the approved maintenance  organisation should perform checks and verifications.

2.  
Performance of above checks and verifications  should take place before the component is installed on the aircraft.

3.  
The following list, though not exhaustive, contains typical checks to be performed:

(a)
verify  the general condition of components  and their packaging in relation to damages that could affect the integrity of the components;

(b)
verify that the shelf life of the component has not expired;

(c)
verify that items are received in the appropriate package in respect of the type of

component:  e.g. correct ATA 300 or electrostatic  sensitive devices packaging, when necessary;

(d)
verify that component has all plugs and caps appropriately installed to prevent damage or internal contamination. Tape should not be used to cover electrical connections or fluid fittings/openings because adhesive residues can insulate electrical connections and contaminate hydraulic or fuel units.

4.  
The purpose of CAD Form 1 (see also MCAR-M Appendix II) is to release components after manufacture  and to release  maintenance  work carried  out on such components  under the approval of CAD and to allow components removed from one aircraft/component to be fitted to another aircraft/ component.

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

(a)  
an EASA Form 1, a  release document  issued  by an organisation under the terms  of a bilateral agreement signed by the European Community; (such as release forms issued under FAA and Transport Canada approval) or a release document issued under the approval of a competent authority acceptable to CAD

It should be noted that the release document should be issued by MCAR-145 or MCAR-M subpart F organisation.

(b)
 to (i) reserved

6.  Any item in storage without a CAD Form 1 or equivalent cannot be installed on aircraft registered in the Maldives unless a CAD Form 1 is issued for such item by an appropriately approved maintenance organisation in accordance with AMC MCAR-
M.613 (a)
AMC M.501 (b) – Installation
1.  
CAD Form 1 identifies the airworthiness and eligibility status of an aircraft component. Block 13 "Remarks"  on the CAD Form 1  in  some  cases  contains  vital airworthiness  related  information  (see also MCAR-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 MCAR-M.801 or the MCAR-M. Subpart F maintenance organisation is satisfied that such components/material meet required standards in respect of manufacture or maintenance, as appropriate.
　
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