Document ID: chunk:federal_register_of_legislation:F2016L01762:front:0:p10
Version: federal_register_of_legislation:F2016L01762
Segment Type: other
Provision Reference: 
Character Range: 24903–28014

flights in its unmodified condition — the aircraft may not be operated for an adventure flight unless the modification is demonstrated to have improved the safety of the aircraft to an adequate level for adventure flights;
(d) an individual who has been authorised by the limited category organisation to grant certificates under regulation 132.105 of CASR 1998 must assess the modification or repair;
(e) the certificate must be provided to the applicant in writing;
(f) the certificate must include the following:
           (i) the make, model and registration of the aircraft;
           (ii) a description or identification of the modification or repair;
           (iii) the approval to carry out adventure flights;
           (iv) any limitations associated with the approval;
           (v) the name of the individual who issued the certificate;
           (vi) the signature of the individual who issued the certificate;
           (vii) the name of the limited category organisation under whose authority the individual issued the certificate;
           (viii) the provision under which the certificate was issued;
           (ix) the date on which the certificate was issued.
       (2)For paragraph (1) (a), the procedures must include consideration of the following:
(a) whether the modification or repair approval permits the aircraft to be used to carry out adventure flights;
(b) for an aircraft that is to be used to carry out adventure flights — whether the approval was issued by any of the following:
           (i) the aircraft's manufacturer;
           (ii) an approved design organisation;
           (iii) CASA;
           (iv) the national aviation authority of a foreign country under a law of the foreign country;
(c) whether the unmodified aircraft is permitted to carry out adventure flights;
(d) whether the modification or repair has an adverse effect on the balance, structural strength, reliability, operational characteristics, or other characteristics affecting the airworthiness of the aircraft.
       (3)For paragraph (1) (b), an adverse effect is assessed in relation to:
(a) the airworthiness standards (if any) that applied in relation to the issue of the aircraft's limited category certificate, and the airworthiness standards (if any) that applied in relation to the approval of any associated modifications or repairs; or
(b) a system safety assessment carried out in accordance with a standard for assessing systems safety that is published by a recognised civil or military standards authority.
       (4)For paragraph (1) (c), the demonstration must include:
(a) documented engineering and system safety analysis of the design of the modification; and
(b) documented quantitative flight test data from the engineering inspection associated with the flight test.
       (5) For paragraphs (1) (d) and (e), the limited category organisation must keep a copy of the certificate and the associated assessment.

20 Procedures for giving advice about modifications or repairs under regulation 132.175 of CASR 1998
       (1)For paragraph 132.190 (2) (b) of CASR 1998,