Commonwealth legislation

AD/BEA 121/25 - Control Rod End Fittings

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This AD requires owners/operators and maintenance organisations of Beagle B121 (Pup) series aeroplanes to carry out inspections and/or modifications as specified in British Aerospace Service Bulletin B121/91. It responds to an incident where a forward elevator control tube fork end detached, risking loss of elevator control. Work must be completed within 100 hours TIS after 30 June 1987 or before the next Maintenance Release; costs and scheduling are the responsibility of the owner/operator.

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AD/BEA 121/25 - Control Rod End Fittings

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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 Beagle B121 (Pup) Series Aeroplanes

AD/BEA 121/25 Control Rod End Fittings 7/87

Applicability: All models.

Requirement: Action in accordance with British Aerospace SB B121/91.

Compliance: Within 100 hours time in service after 30 June 1987 or prior to the issue of the next Maintenance Release after 30 June 1987 whichever is later.

Background: There has been an incident where the forward elevator control tube fork end became detached from the control tube assembly with consequent loss of elevator control.

Source text

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