Document ID: chunk:federal_register_of_legislation:F2006B04730:body:0
Version: federal_register_of_legislation:F2006B04730
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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-2/19 Engine Mounting Bracket Jo-Bolts - Inspection NK

       and Modification

            Applicability: All models which have exceeded 1000 hours total time in service not incorporating Modification NB/M/455.

             Requirement: 1. Inspect the engine mounting frames for loose jo-bolts in accordance with Britten Norman SB BN-2/SB.44.

             2. If on inspection it is found possible to move or partially rotate Jo-Bolts in both brackets on any one engine mounting, Modification NB/M/455 must be carried out before further flight.

            Compliance: Within 100 hours time in service after 31 March 1971 and there- after as detailed in SB No. BN-2/SB.44.