Document ID: chunk:federal_register_of_legislation:F2006B04797:body:0
Version: federal_register_of_legislation:F2006B04797
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Pilatus Britten-Norman BN-2 Series Aeroplanes

 AD/BN-2/9
 Amdt 4

 Empennage - Inspection and Modification NK

 Applicability: All models.

             Requirement: 1. Modify the elevator trim tab installation in accordance with Britten Norman Modification Leaflet No. BN-2/NB/M/507.

2.    Perform the inspections detailed in Britten Norman SB No. BN-2/SB49.

3.    Perform the additional torque inspections detailed in Britten Norman SB No. BN- 2/SB49A.

            Note: The inspection detailed in para. 2 may be performed and certified by the pilot in command.

 Compliance: For para. 1 - Before 30 September 1971.

                    For para. 2 - At intervals not exceeding 50 hours time in service after 28 November 1975. For para. 3 - Within 5 hours time in service after 9 May 1974.