(c)
The area in which maintenance is carried out shall be well organised and clean in respect of dirt and contamination.
(d)
All maintenance shall be performed within any environmental limitations specified in the MCAR-M.401 maintenance data.
(e)
In case of inclement weather or lengthy maintenance, proper facilities shall be used.
(f)
After completion of all maintenance a general verification must be carried out to ensure the aircraft or component is clear of all tools, equipment and any other extraneous parts and material, and that all access panels removed have been refitted.
MCAR-M.403 Aircraft defects
(a)
Any aircraft defect that hazards seriously the flight safety shall be rectified before further flight.
(b)
Only the authorised certifying staff, according to points MCAR-M.801(b)1, MCAR-M.801(b)2, MCAR-M.801(c), MCARM.801(d) or MCAR-145 can decide, using MCAR-M.401 maintenance data, whether an aircraft defect hazards seriously the flight safety and therefore decide when and which rectification action shall be taken before further flight and which defect rectification can be deferred. However, this does not apply when:
1.
the approved minimum equipment list as mandated by CAD is used by the pilot; or,
2.
aircraft defects are defined as being acceptable by CAD.
(c)
Any aircraft defect that would not hazard seriously the flight safety shall be rectified as soon as practicable, after the date the aircraft defect was first identified and within any limits specified in the maintenance data.
(d)
Any defect not rectified before flight shall be recorded in the MCAR-M.305 aircraft maintenance record system or MCAR-M.306 operator's technical log system as applicable.
SUBPART E
COMPONENTS
MCAR-M.501 Installation
(a)
No component may be fitted unless it is in a satisfactory condition, has been appropriately released to service on a CAD Form 1 or equivalent and is marked in accordance with MCAR-21 Subpart Q, unless otherwise specified in MCAR-21, MCAR-145 and MCAR-M Subpart F.
(b)
Prior to installation of a component on an aircraft the person or approved maintenance organisation shall ensure that the particular component is eligible to be fitted when different modification and/or airworthiness directive configurations may be applicable.
(c)
Standard parts shall only be fitted to an aircraft or a component when the maintenance data specifies the particular standard part. Standard parts shall only be fitted when accompanied by evidence of conformity traceable to the applicable standard.
(d)
Material being either raw material or consumable material shall only be used on an aircraft or a component when the aircraft or component manufacturer states so in relevant maintenance data or as specified in MCAR-145. Such material shall only be used when the material meets the required specification and has appropriate traceability. All material must be accompanied by documentation clearly relating to the particular material and containing conformity to specification statement plus both the manufacturing and supplier source.
MCAR-M.502 Component maintenance
(a)
The maintenance of components shall be performed by maintenance organisations appropriately approved in accordance with MCAR-M Subpart F or MCAR-145.
(b)
By derogation from paragraph (a), maintenance of a component in accordance with aircraft maintenance data or, if agreed by the CAD, in accordance with component maintenance data, may be performed by an A rated organisation approved in accordance with MCAR-M Subpart F or MCAR-145 as well as by certifying staff referred to in point MCAR-M.801(b)2 only whilst such components are fitted to the aircraft. Nevertheless, such organisation or certifying staff may temporarily remove this
component for maintenance, in order to improve access to the component, except when such removal generates the need for additional maintenance not eligible for the provisions of this paragraph. Component maintenance performed in accordance with this paragraph is not eligible for the issuance of a CAD Form 1 and shall be subject to the aircraft release requirements provided for in point MCAR-M.801. 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：马尔代夫民航法规 MCAR-M Continuing Airworthiness(11)
