Commonwealth legislation

AD/DHC-6/42 - Inboard Trailing Flap - Inspection and 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This Act has been repealed and is no longer in force. It is retained for historical reference.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

3/10 complexity

This mandatory Airworthiness Directive requires owners/operators of De Havilland Canada DHC-6 Twin Otter aircraft (serials 1–510) to inspect and modify the inboard trailing flaps per De Havilland Service Bulletin No. 6/345. Issued by the Civil Aviation Safety Authority, compliance is compulsory for legal flight because it addresses a specific flap-system safety issue that could affect the aircraft’s airworthiness.

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Current sections

Direct links to the current provisions in AD/DHC-6/42 - Inboard Trailing Flap - Inspection and Modification.

AD/DHC-6/42 - Inboard Trailing Flap - 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 DHC-6 (Twin Otter) Series Aeroplanes

AD/DHC-6/42 Inboard Trailing Flap - Inspection and Modification 6/76

Applicability: All models with S/Nos. 1 to 510. Document: De Havilland of Canada SB No. 6/345. Compliance: As detailed in the requirement document.

Source text

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