AMC M.901(g) Aircraft airworthiness review
The words “certifying staff” mean that the personnel meet at the time of the airworthiness review all the MCAR-66 requirements to be certifying staff for the aircraft subject to review(including also continuing experience requirements), which in some cases may refer toMCAR-66 Subpart B and C.The formal acceptance of the certifying staff by CAD should only be granted after verification of the qualifications and after the satisfactory performance of an airworthiness review under supervision of CAD. The sentence “shall not be issued for more than two consecutive years” means that everythree years the airworthiness review has to be performed by the CAD or by an appropriately approved MCAR-M. Subpart G organisation.
AMC M.901 (j) Aircraft airworthiness review
Suitable accommodation should include:
(a)
an office with normal office equipment such as desks, telephones, photocopying machines etc. whereby the continuing airworthiness records can be reviewed.
(b)
a hangar when needed for the physical survey.
The support of personnel appropriately qualified in accordance with MCAR-66 is necessary when CAD’s airworthiness review staff is not appropriately qualified.
AMC M.904 (a)-1 Airworthiness reviews of aircraft imported into Maldives
In order to allow for possible participation of CAD personnel, the applicant should inform the CAD at least 10 working days in advance of the time and location of the airworthiness review.
AMC M.904 (a)-2 Airworthiness reviews of aircraft imported into Maldives
1.
When performing an airworthiness review of aircraft imported into Maldives the aircraft and the relevant records should be reviewed to determine the work to be undertaken to establish the airworthiness of the aircraft.
2.
In determining the work to be undertaken during the airworthiness review on the aircraft, the following should be taken into consideration:
(a)
the information from importing country authorities such as export certificates, primary authority information; and,
(b)
the information on aircraft maintenance history such as continuing airworthiness records, aircraft, engine, propeller, rotor and life limited part log books or cards as appropriate, tech log / flight log / cabin log, list of deferred defects, total flight times and cycles, times and cycles since last maintenance, accident history, former maintenance schedule, former AD compliance status; and,
(c)
the information on aircraft such as aircraft, engine and propeller type certificate datasheets, noise and emission certificate data sheets, flight manual and supplements; and,
(d)
the aircraft continuing airworthiness status such as the aircraft and component AD status, the SB status, the maintenance status, the status of all service life limited components, weight and centre of gravity schedule including equipment list; and,
(e)
the modification and repair status of the aircraft detailing elements such as owner/operator designed modifications and repairs, STCs, and parts needing European parts approval (EPA) or equivalent approval acceptable to CAD; and,
(f)
the aircraft cabin configuration such as emergency equipment fitted, cockpit configuration, placards, instrument limitations, cabin layout; and,
(g)
the maintenance needed for import, such as embodiment of modifications needed to comply with the EASA type certificate (or equivalent if EASA type certificate is not available), bridging check to comply with the new maintenance programme; and,
(h)
the avionics such as, but not limited to, radio and navigation equipment, instrument flight rules (IFR) equipment, digital flight data recorder (DFDR) / cockpit voice recorder (CVR) test, ELT 406 MHz code and identification; and,
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