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2. The continuing airworthiness management organisation shall not use the indirect approval procedure when this organisation is not under the oversight of the  State of Registry, unless an agreement exists in accordance with point M.1, paragraph 4(ii) or 4(iii), as applicable, transferring the responsibility for the approval of the aircraft maintenance programme to DGCA.
(d) The aircraft maintenance  programme  must  establish compliance  with :
1.  
instructions issued by DGCA.

2.  
instructions for continuing airworthiness issued by the holders of the type certificate, restricted type-certificate, supplemental type-certificate, major repair design approval, TSO authorisation or any other relevant approval issued under CAR 21/ EASA 21/ FAR 21.

3.  
additional or alternative instructions proposed by the owner or the continuing airworthiness management organisation once approved in accordance with point M.A.302, except for intervals of safety related tasks referred in paragraph (e), which may be escalated, subject to sufficient reviews carried out in accordance with paragraph (g) and only when subject to direct approval in accordance with point M.A.302(b).

(e)  
The aircraft maintenance programme shall contain details, including frequency, of all maintenance to be carried out, including any specific tasks linked to the type and the specificity of operations.

(f)  
For large aircraft, when the maintenance programme is based on maintenance steering group logic or on condition monitoring, the aircraft maintenance programme shall include a reliability programme. 

(g)  
The aircraft maintenance programme shall be subject to periodic reviews and amended accordingly when necessary. These reviews shall ensure that the programme continues to be valid in light of the operating experience and instructions from DGCA whilst taking into account new and/or modified maintenance instructions promulgated by the type certificate and supplementary type certificate holders and any other organisation that publishes such data in accordance with CAR 21/EASA 21/FAR 21.

M.A.303 Airworthiness directives
Any applicable airworthiness directive must be carried out within the requirements of that airworthiness directive, unless otherwise specified by DGCA.
M.A.304 Data for modifications and repairs
Damage shall be assessed and modifications and repairs carried out using data approved by DGCA or by an approved CAR -21/ EASA Part 21/ FAA Part 21 design organization, as appropriate.
M.A.305 Aircraft continuing airworthiness record system
(a)  
At the completion of any maintenance, the associated M.A.801 certificate of release to service shall be entered in the aircraft continuing airworthiness records. Each entry shall be made as soon as practicable but in no event more than 30 days after the day of maintenance action.

(b)  
The aircraft continuing airworthiness records shall consist of:

Rev 0, dated 2nd March, 2010
1.  
an aircraft logbook, engine logbook(s) or engine module log cards, propeller logbook(s) and log cards for any service life limited component as appropriate, and,

2.  
when required in point M.A.306 for commercial air transport or by DGCA for commercial operations other than commercial air transport, the operator’s technical log.’

(c)  
The aircraft type and registration mark, the date, together with total flight time and/or flight cycles and/or landings, as appropriate, shall be entered in the aircraft logbooks.

(d)  
The aircraft continuing airworthiness records shall contain the current:

1.  
status of airworthiness directives and measures mandated by the DGCA in immediate reaction to a safety problem;

2.  
status of modifications and repairs;
　
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