Commonwealth legislation

AD/DHC-6/41 - Wing Tip Bonding - Modification

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legislative instrument

Plain English Summary

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This airworthiness directive requires a wing‑tip bonding modification on De Havilland DHC‑6 (Twin Otter) aircraft, serial numbers 1–430, fitted with wing‑tip strobe lights, carried out to De Havilland Service Bulletin No. 6/318 and Canadian AD CF‑76‑04. The modification must be completed within 100 hours time‑in‑service after 30 June 1976; owners/operators pay the costs and must comply to avoid regulatory enforcement.

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AD/DHC-6/41 - Wing Tip Bonding - 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-6/41 Wing Tip Bonding - Modification 5/76

Applicability: All models with S/Nos. 1 to 430 incorporating wing tip strobe lighting. Document: 1. De Havilland SB No. 6/318.

Canadian AD CF-76-04.

Compliance: Within 100 hours time in service after 30 June 1976.

Source text

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