Commonwealth legislation

AD/BN-2/34 - Rudder Bar Lower Mounting - Inspection and Modification

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

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This Airworthiness Directive requires inspection and modification of the rudder bar lower mounting on Pilatus Britten‑Norman BN‑2A aeroplanes that have exceeded 1,000 hours service (except those with Mod. No. NB/M/463 Part A). Operators must inspect within 25 hours after 24 May 1976 and every 200 hours until the modification is done, with the modification completed by 31 August 1976. It imposes compliance, cost and downtime on aircraft owners/operators.

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AD/BN-2/34 - Rudder Bar Lower Mounting - 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

View image in the official source Pilatus Britten-Norman BN-2 Series Aeroplanes

AD/BN-2/34 Rudder Bar Lower Mounting - Inspection NK

and Modification

Applicability: All model BN-2A which have exceeded 1000 hours total time in service, except those which have incorporated Mod. No. NB/M/463 Part A.

Document: Britten Norman SB No. BN-2/SB.74, Issue 2.

Compliance: Within 25 hours time in service after 24 May 1976 and thereafter at intervals not exceeding 200 hours time in service until modified. Modify not later than 31 August 1976.

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.