(d)
A new airworthiness certificate will be issued by the Member State of registry when it is satisfied the aircraft complies with the prescriptions of Part-21.

(e)
The Member State shall also issue the airworthiness review certificate valid normally for one year unless the Member State has safety reason to limit the validity.

AMC M.A.904 (a)(1) Airworthiness reviews of aircraft imported into the EU
In order to allow for possible participation of authority personnel, the applicant should inform the competent authority at least 10 working days in advance of the time and loca-tion of the airworthiness review.
AMC M.A.904 (a)(2) Airworthiness reviews of aircraft imported into the EU
1.  
When performing an airworthiness review of aircraft imported into the EU 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 third country authorities such as export certificates, pri-mary authority information;

(b)
the information on aircraft maintenance history such as continuing airworthi-ness 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;

(c)  
the information on aircraft such as aircraft, engine and propeller type certificate datasheets, noise and emission certificate data sheets, flight manual and supple-ments;

(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;

(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);

(f)  
the aircraft cabin configuration such as emergency equipment fitted, cockpit configuration, placards, instrument limitations, cabin layout;

(g)
the maintenance needed for import, such  as embodiment of modifications needed to comply with the EASA type certificate, bridging check to comply with the new maintenance programme;

(h)
the avionics such as, but not limited to, radio and navigation equipment, instru-ment flight rules (IFR) equipment, digital flight data recorder (DFDR)/cockpit voice recorder (CVR) test, emergency locator transmitter (ELT) 406 MHz code and identification;

(i)  
the compass compensation;

(j)  
special operating rules such as extended twin-engine operations (ETOPS)/long range operations (LROPS), reduced vertical separation minima (RVSM), minimum navigation performance specifications (MNPS), all weather operations (AWOPS), area navigation (RNAV);

ED 2010/002/R
Section A
PART-M
Subpart I

ED 2008/013/R ED 2010/002/R
(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 the specific aircraft type available, the competent authority may carry out the airworthiness review in accordance with this paragraph and the provisions M.A.901(h) and M.B.902. In this case, the airworthiness review should be requested to the competent authority with a 30-day notice.
　
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