AD/BN-2/19 - Engine Mounting Bracket Jo-Bolts - Inspection and Modification
1AD/BN-2/19 - Engine Mounting Bracket Jo-Bolts - Inspection and Modification
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text 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.
- 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.