Commonwealth legislation

AD/DHC-3/1 - Rudder Quadrant, Rudder Pedal Linkage, Tail Wheel Assembly and Rear Fuselage

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This instrument orders owners/operators of DHC‑3 (Otter) aeroplanes within the Requirement Document’s applicability to carry out specified work on the rudder quadrant, pedal linkage, NK tail wheel assembly and rear fuselage by following De H Canada TNS Otter Nos 3 or 4, 6 and 9. Compliance is required forthwith, imposing immediate maintenance, parts and downtime costs on operators; the directive cross‑references Canadian AD 53‑16.

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Current sections

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AD/DHC-3/1 - Rudder Quadrant, Rudder Pedal Linkage, Tail Wheel Assembly and Rear Fuselage

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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-3/1 Rudder Quadrant, Rudder Pedal Linkage, NK Tail Wheel Assembly and Rear Fuselage

Applicability: As detailed in Requirement Document.

Requirement: Action in accordance with De H Canada TNS Otter Nos 3 or 4, 6 and 9.

Note: Canadian AD 53-16 refers.

Compliance: Forthwith.

Source text

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