Commonwealth legislation

AD/DHC-6/13 - Flap Control Push Rod Assembly - Modification

RepealedCTH

This Act has been repealed and is no longer in force. It is retained for historical reference.

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

Owners/operators of De Havilland DHC‑6 Twin Otter aircraft (serial numbers 1–105) must install a safety modification to the flap control push‑rod assembly per De Havilland Canada Modification Bulletin No. 6/1085. The modification, required before 1 January 1969, addresses a flap control failure risk that could compromise safe takeoffs and landings.

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Current sections

Direct links to the current provisions in AD/DHC-6/13 - Flap Control Push Rod Assembly - Modification.

AD/DHC-6/13 - Flap Control Push Rod Assembly - 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 DHC-6 (Twin Otter) Series Aeroplanes

AD/DHC-6/13 Flap Control Push Rod Assembly - Modification 8/68

Applicability: All models with S/Nos. 1 to 105 not modified in Mod. Bulletin No. 6/1085. Document: De Havilland Canada Mod. Bulletin No. 6/1085.

Compliance: Before 1 January 1969.

Source text

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