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 exporting 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
Rev 0, dated 2nd March, 2010 owner/operator designed modifications and repairs, STCs, and parts needing approval; 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 DGCA type certificate, bridging check to comply with the new maintenance programme; and,
h) 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,
i) the compass compensation; and,
j) special operating rules such as extended twin-engine operations (ETOPS)/ long range operations (LROPS), reduced vertical separation minima (RVSM), MNPS, all weather operations (AWOPS), RNAV; and,
k) the aircraft survey including verification of conformity with the flight manual and the datasheet, presence of fire proof identification plates, conformity of markings including registration, presence and serviceability of emergency equipment, internal and external lighting systems,and,
l) check flight including check of control system / cockpit ground check / engine run up
3. If there is no M.A. Subpart G organisation approved for specific aircraft type available, DGCA may carry out the airworthiness review in accordance with this paragraph and the provisions
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