4.  
Subject to compliance with the conditions 1 to 3 above, this approval shall remain valid for an unlimited duration unless the approval has previously been surrendered, superseded, suspended or revoked. 

If this form is also used for AOC holders, the AOC number shall be added to the reference, in addition to the standard number, and the condition 4 shall be replaced by the following extra conditions:

5.  
This approval does not constitute an authorisation to operate the types of aircraft referred in paragraph 1. The authorisation to operate the aircraft is the Air Operator Certificate (AOC).

6.  
Where the continuing airworthiness management organisation contracts under its Quality System the service of an/several organisation(s), this approval remains valid subject to such organisation(s) fulfilling applicable contractual obligations

7.  
Termination, suspension or revocation of the AOC automatically invalidates the present approval in relations to the aircraft registrations specified in the AOC, unless otherwise explicitly stated by the CAD.

8.  
Subject to compliance with the previous conditions, this approval shall remain valid for an unlimited duration unless the approval has previously been surrendered, superseded, suspended or revoked.

Date of original issue …………………………… Signed ……………………………………………..
Date of this revision ……………………….. Revision No: ............................................................

For the Civil Aviation Department:......................................................

Page ..... of .......

CONTINUING AIRWORTHINESS MANAGEMENT ORGANISATION
APPROVAL CERTIFICATE

REFERENCE: MV.MG.XXXX (ref. AOC MV.XXXX)
ORGANISATION:[COMPANY NAME AND ADDRESS]

Aircraft type/series/group  Airworthiness review authorised  Organisation(s) working under the quality system 
[YES/NO] 

This approval Schedule is limited to that specified in the scope of approval contained in MCAR-M subpart G
approved continuing airworthiness management exposition section .................................................
Continuing Airworthiness Management Exposition reference: ............................................
Date of original issue …………………………… Signed ……………………………………………..

Date of this revision ……………………….. Revision No: ............................................................

For the Civil Aviation Department:......................................................

Page ..... of .......
CAD Form 14

Appendix VII
Complex Maintenance Tasks
The following constitutes the complex maintenance tasks referred to in points MCAR-M.502(d)3, MCAR-M.801(b)2 and MCAR-M.801(c):
1.  The modification, repair or replacement by riveting, bonding, laminating, or welding of any of the following airframe parts:
(a)
a box beam;

(b)
a wing stringer or chord member;

(c)
a spar;

(d)
a spar flange;

(e)
a member of a truss-type beam;

(f)
the web of a beam;

(g)
a keel or chine member of a flying boat hull or a float;

(h)
a corrugated sheet compression member in a wing or tail surface;

(i)
a wing main rib;

(j)
a wing or tail surface brace strut;

(k)
an engine mount;
　
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