Article 1
Objective and scope
1. This Regulation establishes common technical requirements and administrative pro-cedures for ensuring the continuing airworthiness of aircraft, including any compo-nent for installation thereto, which are:
(a)
registered in a Member State; or
(b)
registered in a third country and used by an operator for which a Member State ensures oversight of operations.
2.
Paragraph 1 shall not apply to aircraft the regulatory safety oversight of which has been transferred to a third country and which are not used by a Community operator, or to aircraft referred to in Annex II to the basic Regulation.
3.
The provisions of this Regulation related to commercial air transport are applicable to licensed air carriers as defined by Community law.
Article 2
Definitions
Within the scope of the basic Regulation, the following definitions shall apply:
(a)
“aircraft” means any machine that can derive support in the atmosphere from the reactions of the air other than reactions of the air against the earth’s surface;
(b)
“certifying staff” means personnel responsible for the release of an aircraft or a com-ponent after maintenance;
(c)
“component” means any engine, propeller, part or appliance;
(d)
“continuing airworthiness” means all of the processes ensuring that, at any time in its operating life, the aircraft complies with the airworthiness requirements in force and is in a condition for safe operation;
(e)
“JAA” means “Joint Aviation Authorities”;
(f)
“JAR” means “Joint Aviation Requirements”;
(g)
“large aircraft” means an aircraft, classified as an aeroplane with a maximum take-off mass of more than 5700 kg, or a multi-engined helicopter;
(h)
“maintenance” means any one or combination of overhaul, repair, inspection, replacement, modification or defect rectification of an aircraft or component, with the exception of pre-flight inspection;
(i)
“organisation” means a natural person, a legal person or part of a legal person. Such an organisation may be established at more than one location whether or not within the territory of the Member States;
(j)
“pre-flight inspection” means the inspection carried out before flight to ensure that the aircraft is fit for the intended flight.
(k)
“ELA1 aircraft” means the following European Light Aircraft:
(i) an aeroplane, sailplane or powered sailplane with a Maximum Take-off Mass (MTOM) less than 1000 kg that is not classified as complex motor-powered air-craft;
14
Marked impostata da ragusa
EC 1056/2008
Marked impostata da ragusa
EC 1056/2008 EC 1056/2008
Article 4
Maintenance organisation approvals
1.
Organisations involved in the maintenance of large aircraft or of aircraft used for commercial air transport, and components intended for fitment thereto, shall be approved in accordance with the provisions of Annex II.
2.
Maintenance approvals issued or recognised by a Member State in accordance with the JAA requirements and procedures and valid before the entry into force of this Regulation shall be deemed to have been issued in accordance with this Regulation. For this purpose, by derogation from the provisions of 145.B.50(2) under Annex II, level 2 findings associated with the differences between JAR 145 and Annex II may be closed within one year. Certificates of release to service and authorised release certificates issued by an organisation approved under JAA requirements during that one-year period shall be deemed to have been issued under this Regulation.
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本文鏈接地址：CONTINUING AIRWORTHINESS REQUIREMENTS – PART M 1(12)
