Commonwealth legislation

AD/DHC-2/18 - Tailplane Rear Spar - Inspection and Modification

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

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This airworthiness directive requires every De Havilland DHC‑2 (Beaver) operator to inspect the tailplane rear spar within 25 hours TIS after 8 July 1977 and to carry out any required modification and ongoing inspections per De Havilland Service Bulletin No. 2/19. Compliance is the owner/operator’s legal responsibility, enforced by CASA under the Civil Aviation Regulations, and may cause near‑term downtime, inspection and modification costs charged by maintenance providers.

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AD/DHC-2/18 - Tailplane Rear Spar - Inspection and 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-2 (Beaver) Series Aeroplanes

AD/DHC-2/18 Tailplane Rear Spar - Inspection and Modification 7/77

Applicability: All models.

Document: De Havilland Aircraft of Canada SB No. 2/19.

Compliance: Initially inspect within 25 hours time in service after 8 July 1977 and thereafter as per requirement document.

Source text

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