Document ID: chunk:federal_register_of_legislation:F2006B03590:body:0
Version: federal_register_of_legislation:F2006B03590
Segment Type: other
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Character Range: 0–691

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 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.