3.
status of compliance with maintenance programme;
4.
status of service life limited components;
5.
mass and balance report;
6.
list of deferred maintenance.
(e) In addition to the authorised release document, CA Form 1/ EASA Form1/ FAA 8130 or equivalent, the following information relevant to any component installed shall be entered in the appropriate engine or propeller logbook, engine module or service life limited component log card:
1.
identification of the component, and;
2.
the type, serial number and registration of the aircraft to which the particular component has been fitted, along with the reference to the installation and removal of the component, and;
3.
the particular component accumulated total flight time and/or flight cycles and/or landings and/or calendar time, as appropriate, and;
4.
the current paragraph (d) information applicable to the component.
(f)
The person responsible for the management of continuing airworthiness tasks pursuant to M.A. Subpart B, shall control the records as detailed in this paragraph and present the records to DGCA upon request.
(g)
All entries made in the aircraft continuing airworthiness records shall be clear and accurate. When it is necessary to correct an entry, the correction shall be made in a manner that clearly shows the original entry.
(h)
An owner or operator shall ensure that a system has been established to keep the following records for the periods specified:
1.
all detailed maintenance records in respect of the aircraft and any life-limited component fitted thereto, at least 24 months after the aircraft or component was permanently withdrawn from service, and;
2.
the total time and flight cycles as appropriate, of the aircraft and all life-limited components, at least 12 months after the aircraft or component has been permanently withdrawn from service, and;
Rev 0, dated 2nd March, 2010
3.
the time and flight cycles as appropriate, since last scheduled maintenance of the component subjected to a service life limit, at least until the component scheduled maintenance has been superseded by another scheduled maintenance of equivalent work scope and detail, and;
4.
the current status of compliance with maintenance programme such that compliance with the approved aircraft maintenance programme can be established, at least until the aircraft or component scheduled maintenance has been superseded by other scheduled maintenance of equivalent work scope and detail, and;
5.
the current status of airworthiness directives applicable to the aircraft and components, at least 12 months after the aircraft or component has been permanently withdrawn from service, and;
6.
details of current modifications and repairs to the aircraft, engine(s), propeller(s) and any other component vital to flight safety, at least 12 months after they have been permanently withdrawn from service.
M.A.306 Operator's technical log system
(a) In the case of commercial air transport, in addition to the requirements of M.A.305, an operator shall use an aircraft technical log system containing the following information for each aircraft:
1.
information about each flight, necessary to ensure continued flight safety, and;
2.
the current aircraft certificate of release to service, and;
3.
the current maintenance statement giving the aircraft maintenance status of what scheduled and out of phase maintenance is next due. The maintenance statement may be kept at the operators engineering office: and;
4.
all outstanding deferred defects rectifications that affect the operation of the aircraft, and;
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