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b)  are installed in accordance with the Type Certificate holder’s requirements or other
applicable data acceptable to the State of Registry by a competent and appropriately
approved individual or maintenance organization.
3.2.7.2 In the case of a repair following an accident or at any time when significant structural replacement becomes necessary, the AID of the State of Registry may wish to have a more direct role in the aircraft’s return to service, perhaps completing an inspection of the aircraft or requiring the submission of a report by an individual or organization prior to the restoration of the Certificate of Airworthiness.
3.2.7.3  The crucial role played in such circumstances by the related airworthiness records, i.e. log books, worksheets, etc. is self-evident and these will require considerable attention in order to ensure the aircraft is properly configured and conforms to its type design.
3.2.8 Airworthiness flight test
Note.— This paragraph is not intended to specify any particular necessity to carry out airworthiness flight tests additional to test flights for normal production/initial Certificate of Airworthiness issue, or maintenance/modification approval flight tests. Such flight tests are expected to be part of regular production procedures or be specified in the aircraft manufacturers maintenance data or in the requirements pertaining specifically to the approval of a particular modification and be under the control of an organization, or person, approved to do such test flying.
This paragraph is intended to ensure that, when a CAA does require airworthiness flight tests in support of continuing airworthiness assurance, the flight tests are carried out with due care and attention to safety, and under appropriate management by the CAA and the organization conducting the flight tests. The principles for safe flight test control and operation are expected to be applied to all test flights for whatever purpose.
3.2.8.1 A State may require airworthiness flight tests to be performed in support of continuing airworthiness assurance. Such flight tests should be carried out by pilots and crew approved for the purpose by the CAA/AID. The crew should be appropriately licensed for the specific aircraft type and competent to conduct the tests defined in the flight test schedule. Except when additional crew are required to be carried for a specific flight test purpose, the number of persons conducting the flight test should be restricted to the minimum crew specified in the Certificate of Airworthiness (Flight Manual).
3.2.8.2 A flight test schedule, specific to the aircraft involved, will be prepared and agreed with the CAA, before the test flight. The flight test schedule should define the purpose of the test(s), the requirements and/or the conditions to be met and any particular limitations for the test(s), which may apply, in addition to the normal limitations of the Certificate of Airworthiness and the Flight Manual.
3.2.8.3 A flight test report, in a format acceptable to the CAA, should be prepared and presented, as soon as possible after the test flight, for acceptance/approval by the CAA.
3.3 Approvals for special flights
3.3.1 When an aircraft is not fully in compliance with its airworthiness requirements, the CAA airworthiness regulations may, nevertheless, make provisions for the AID to issue a special flight permit, providing the aircraft is capable of safe flight. Such occasions might include:
a)  relocating the aircraft to a base where maintenance is to be performed, or to a point of storage;
b)  delivering the aircraft; or
c)  evacuating the aircraft from an area of impending danger, or in cases of force majeure.
3.3.2 Application for a special flight permit should be submitted in a manner prescribed by the AID, indicating at least the following: a) the make, model, serial number and registration marks of the aircraft; b) the purpose of the flight; c)  the proposed itinerary; d) the crew required to operate the aircraft; e) details of non-compliance with applicable airworthiness requirements; f) any restriction the applicant considers necessary for safe operation of the aircraft; and
　
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