Commonwealth legislation

AD/BEECH 200/7 - Rudder Push Rod Assembly

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This airworthiness directive requires owners/operators of Beechcraft 200 (Super King Air) aeroplanes S/N BB-2 through BB-58 to have the rudder push rod assembly serviced per Beechcraft Service Instruction No. 0778‑153. Work must be completed within 100 hours time‑in‑service after 31 May 1976. The CASA enforces the mandate; owners bear the costs and maintenance organisations must perform and document the work.

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Current sections

Direct links to the current provisions in AD/BEECH 200/7 - Rudder Push Rod Assembly.

AD/BEECH 200/7 - Rudder Push Rod Assembly

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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 Beechcraft 200 (Super King Air) Series Aeroplanes

AD/BEECH 200/7 Rudder Push Rod Assembly 5/76

Applicability: All models with S/Nos BB-2 to BB-58.

Requirement: Action in accordance with Beechcraft SI No 0778-153.

Note: FAA AD 76-03-07 refers.

Compliance: Within 100 hours time in service after 31 May 1976.

Source text

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