Commonwealth legislation

AD/DHC-6/11 - Flap Elevator Trim Cables - 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This Act has been repealed and is no longer in force. It is retained for historical reference.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 DHC‑6 Twin Otter aircraft (serial numbers 1–95) must, as a legal requirement, modify the flap elevator trim cables per De Havilland of Canada Modification Bulletin No. 6/1127. The work must be completed within 300 flight hours in service measured from 21 March 1968. Compliance is mandatory for continued airworthiness and legal operation in Australia.

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Current sections

Direct links to the current provisions in AD/DHC-6/11 - Flap Elevator Trim Cables - Modification.

AD/DHC-6/11 - Flap Elevator Trim Cables - 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-6/11 Flap Elevator Trim Cables - Modification 2/68

Applicability: All models with S/Nos. 1 to 95.

Document: De Havilland of Canada Mod. Bulletin No. 6/1127. Compliance: Within 300 hours time in service after 21 March 1968.

Source text

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