Commonwealth legislation

AD/DHC-3/22 - Elevator Tab Control Arm

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This AD in the Commonwealth schedule requires owners/operators of all De Havilland DHC‑3 (Otter) aeroplanes to carry out the work specified in De Havilland Canada Service Bulletin No. 3/4 on the elevator tab control arm within 50 hours TIS after 2 November 1967. It matters because it mandates corrective action for that component, delegates technical detail to the manufacturer’s SB, and imposes immediate inspection/repair costs, downtime and logistical burdens on operators.

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Current sections

Direct links to the current provisions in AD/DHC-3/22 - Elevator Tab Control Arm.

AD/DHC-3/22 - Elevator Tab Control Arm

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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-3/22 Elevator Tab Control Arm 10/67

Applicability: All models.

Requirement: Action in accordance with De H Canada SB No 3/4. Compliance: Within 50 hours time in service after 2 November 1967.

Source text

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