Commonwealth legislation

AD/DHC-6/18 Amdt 1 - Rudder and Elevator Pulley Bracket Assembly Stn 106 - Inspection

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Commonwealth

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legislative instrument

Plain English Summary

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This CASA airworthiness directive for DHC‑6 (Twin Otter) aircraft mandates a visual inspection of the elevator/rudder pulley bracket at fuselage station 106 for cracking or deformation, to be done forthwith and repeated every 25 TIS after 1 September 1971. It applies to all DHC‑6s except those incorporating Mod. No. 6/1262. Operators must carry out and fund the inspections, creating an incentive to fit the exempting modification.

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AD/DHC-6/18 Amdt 1 - Rudder and Elevator Pulley Bracket Assembly Stn 106 - Inspection

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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-6/18

Amdt 1

Rudder and Elevator Pulley Bracket Assembly Stn 106 - Inspection

6/69

Applicability: All models not incorporating Mod. No. 6/1262.

Requirement: Visually inspect the elevator rudder pulley bracket assembly at Fuselage Station 106 with particular attention to the forward flange of the top and bottom beams outboard of the outboard lightening holes for cracking or deformation.

Compliance: Forthwith, then at intervals not exceeding 25 TIS after 1 September 1971.

Source text

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