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b) a hangar when needed for the physical survey. The support of personnel appropriately qualified in accordance with Rule 61 is necessary when DGCA’s airworthiness review staff is not appropriately qualified.
Rev 0, dated 2nd March, 2010
AMC M.A.903 (a) - 1 Transfer of aircraft registration within India.
The applicant should notify to DGCA so as to allow the proper transfer of information during the aircraft transfer process.
AMC M.A.903 (b) Transfer of aircraft registration within India:  
In case of transfer of aircraft registration within India, the aircraft owner/ operator should verify that DGCA has entered the new aircraft registration, if any, on the existing airworthiness review certificate and validated the change.
AMC M.A.904 (a)-1 Airworthiness reviews of aircraft imported into India
In order to allow for possible participation, the applicant should inform DGCA at least 10 working days in advance of the time and location of the airworthiness review.
AMC M.A.904 (a)-2 Airworthiness reviews of aircraft imported into India 
1.  
When performing an airworthiness review of aircraft imported into the country 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 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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