7.  
all service life limited components installed on the aircraft are properly identified, registered and have not exceeded their approved service life limit, and;

8.  
all maintenance has been released in accordance with this Part of CAR , and;

9.  
the current mass and balance statement reflects the configuration of the aircraft and is valid, and;

10.  
the aircraft complies with the latest revision of its type design approved/ accepted by the DGCA.

(b)  The approved continuing airworthiness management organisation's airworthiness review staff shall carry out a physical survey of the aircraft. For this survey, airworthiness review
Rev 0, dated 2nd March, 2010
staff not appropriately qualified to the licensing requirements shall be assisted by such qualified personnel.
(c)  Through the physical survey of the aircraft, the airworthiness review staff shall ensure that:
1.  
all required markings and placards are properly installed, and;

2.  
the aircraft complies with its approved flight manual, and;

3.  
the aircraft configuration complies with the approved documentation, and;

4.  
no evident defect can be found that has not been addressed according to M.A.403, and;

5.  
no inconsistencies can be found between the aircraft and the paragraph (a) documented review of records.

(d)  
By derogation to M.A.902(a) the airworthiness review can be anticipated by a maximum period of 90 days without loss of continuity of the airworthiness review pattern, to allow the physical review to take place during a maintenance check.

(e)  
An M.A.902 airworthiness review certificate (CA Form 15b – Appendix-III) or a recommendation is issued by appropriately authorised M.A.707 airworthiness  review staff on behalf of the approved continuing airworthiness management organisation when satisfied that the airworthiness review has been properly carried out.

(f)  
A copy of any airworthiness review certificate issued or extended for an aircraft shall be sent to State of Registry within 10 days.

(g)  
Airworthiness review tasks shall not be sub-contracted.

(h)  
Should the outcome of the airworthiness review be inconclusive, the DGCA shall be informed. 

M.A.711 Privileges of the organization 
(a)        A continuing airworthiness management organisation approved in accordance with Section A, Subpart G of CAR-M may: 
1.  
manage the continuing airworthiness of non-commercial air transport aircraft as listed on the approval certificate;

2.  
manage the continuing airworthiness of commercial air transport aircraft when listed both on its approval certificate and on its Air Operator Certificate (AOC);

3.  
arrange to carry out limited continuing airworthiness tasks with any contracted organisation, working under its quality system, as listed on the approval certificate; 

4.  
extend, under the conditions of point M.A.901(f), an airworthiness review certificate that has been issued by DGCA or by another continuing airworthiness management organisation approved in accordance with Section A, Subpart G of CAR-M;

M.A.712 Quality system
(a)  To ensure that the approved continuing airworthiness management organisation continues to meet the requirements of this Subpart, it shall establish a quality system and designate a quality manager to monitor compliance with, and the adequacy of,
Rev 0, dated 2nd March, 2010 procedures required to ensure airworthy aircraft. Compliance monitoring shall include a feedback system to the accountable manager to ensure corrective action as necessary.
(b)  The quality system shall monitor M.A. Subpart G activities. It shall at least include the following functions:
　
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