(e)
issuance of a Form 1 in compliance with paragraphs 2.2, 2.3 and 2.4.
These alleviated requirements are based on the fact that credit can be taken for
their technical capabilities and their competent authority oversight, as attested
by the following documents:
· BASA/MIP-G Maintenance Implementation Procedures Guidance (USA),
· AAM-G Administrative Arrangement on Maintenance Guidance (Canada).
2.9. Used aircraft components removed from an aircraft involved in an accident or incident. Such components should only be issued with an EASA Form 1 when processed in accordance with paragraph 2.7 and a specific work order including all additional necessary tests and inspections made necessary by the accident or incident. Such a work order may require input from the TC holder or original manufacturer as appropriate. This work order should be referenced in block 12.
3.
A certificate should not be issued for any component when it is known that the component is unserviceable except in the case of a component undergoing a series of maintenance processes at several approved maintenance organisations and the component needs a certificate for the previous maintenance process carried out for the next approved maintenance organisation to accept the component for subse-quent maintenance processes. In such a case, a clear statement of limitation should be endorsed in block 12.
4.
The certificate is to be used for export/import purposes, as well as for domestic purposes, and serves as an official certificate for components from the manufac-turer/maintenance organisation to users. It should only be issued by organisations approved by a competent authority or the Agency as applicable within the scope of the approval.
AMC M.A.614 (a) Maintenance records
1.
Properly executed and retained records provide owners, operators and maintenance personnel with information essential in controlling unscheduled and scheduled maintenance, and trouble shooting to eliminate the need for re-inspection and rework to establish airworthiness.
The prime objective is to have secure and easily retrievable records with compre-hensive and legible contents. The aircraft record should contain basic details of all serialised aircraft components and all other significant aircraft components installed, to ensure traceability to such installed aircraft component documentation and associ-ated M.A.304 maintenance data.
2.
The maintenance record can be either a paper or computer system or any combina-tion of both. The records should remain legible throughout the required retention period.
3.
Paper systems should use robust material which can withstand normal handling and filing.
4.
Computer systems may be used to control maintenance and/or record details of maintenance work carried out. Computer systems used for maintenance should have at least one backup system which should be updated at least within 24 hours of any maintenance. Each terminal is required to contain programme safeguards against the ability of unauthorised personnel to alter the database.
AMC M.A.614 (c) Maintenance records
Associated maintenance data is specific information such as repair and modification data. This does not necessarily require the retention of all aircraft maintenance manual, component maintenance manual, parts catalogues etc issued by the TC holder or STC holder. Maintenance records should refer to the revision status of the data used.
ED 2008/013/R
AMC M.A.615 (b) Privileges of the organisation
M.A.615(b) refers to work carried out by another organisation which is not appropriately approved under M.A. Subpart F or Part-145 to carry out such tasks.
The intent is to permit the acceptance of specialised maintenance services, such as, but not limited to, non-destructive testing, surface treatment, heat-treatment, welding, fab-rication of specified parts for minor repairs and modifications, etc., without the need of Subpart F approval for those tasks.
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：CONTINUING AIRWORTHINESS REQUIREMENTS – PART M 1(48)
