Commonwealth legislation

AD/DHC-3/16 - Flap Control Rod Sub-Assembly

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This AD mandates that owners/operators of De Havilland DHC-3 (Otter) aircraft serial numbers 2–292 must immediately carry out the actions set out in De H Canada Engineering Bulletin "O" No 49 on the flap control rod sub‑assembly.

It affects operators and maintenance organisations (costs for parts, labour and downtime fall to owners) and matters because it reduces the risk of flap control‑rod failure to preserve airworthiness.

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Current sections

Direct links to the current provisions in AD/DHC-3/16 - Flap Control Rod Sub-Assembly.

AD/DHC-3/16 - Flap Control Rod Sub-Assembly

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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-3 (Otter) Series Aeroplanes

AD/DHC-3/16 Flap Control Rod Sub-Assembly NK

Applicability: All models with S/Nos 2 to 292.

Requirement: Action in accordance with De H Canada EB “O” No 49.

Note: Canadian AD 58-15 refers.

Compliance: Forthwith.

Source text

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