Commonwealth legislation

AD/BN-2/43 - Engine Controls Attachment Brackets - Modification

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

Requires BN‑2 series aircraft to have engine control cable attachment brackets inspected and either reinforced or replaced per Britten Norman SB BN‑2/SB.109 Issue 3 within 100 hours after 31 May 1979. Affects aircraft owners/operators and maintenance providers, who bear the costs; intended to prevent fatigue failure that could cause partial loss of engine control.

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AD/BN-2/43 - Engine Controls Attachment Brackets - 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-2/43 Engine Controls Attachment Brackets - Modification

5/79

Applicability: All models.

Document: Britten Norman SB No. BN-2/SB.109, Issue 3. Compliance: Within 100 hours time in service after 31 May 1979.

Background: To prevent partial loss of engine control due to fatigue failure of the engine control cables attachment brackets, the brackets are to be either reinforced if uncracked or replaced with improved brackets if cracked.

Source text

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