Commonwealth legislation

AD/DHC-6/39 - Electric Power Cable Below Cockpit - Modification

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This airworthiness directive (AD/DHC-6/39) mandates a modification to the electric power cable below the cockpit on De Havilland DHC‑6 (Twin Otter) aeroplanes serial numbers 1–135, carried out per De Havilland SB No. 6/304 Revision B within 100 hours TIS after 30 August 1974.

It affects registered owners/operators, who must arrange and pay for the maintenance and record compliance so the aircraft meet continuing airworthiness requirements.

JSON API

Deep dive

Want the full deep dive?

Zoe can write the in-depth analysis on top of the summary above: how it works, who it affects and what each part actually does.

Current sections

Direct links to the current provisions in AD/DHC-6/39 - Electric Power Cable Below Cockpit - Modification.

AD/DHC-6/39 - Electric Power Cable Below Cockpit - Modification

meta-content-style-type: text/css meta-content-type: application/xhtml+xml; charset=utf-8 meta-generator: Aspose.Words for .NET 22.10.0

?xml version="1.0" encoding="utf-8" standalone="no"?>

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-6/39 Electric Power Cable Below Cockpit - Modification

Applicability: All models with S/Nos. 1 to 135.

Document: De Havilland of Canada SB No. 6/304 Rev. B.

Compliance: Within the next 100 hours time in service after 30 August 1974.

7/74

Source text

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