Commonwealth legislation

AD/BEECH 60/9 - Inboard Elevator Hinge Bracket

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This directive requires owners/operators of Beechcraft Model 60/A60 aircraft (S/N P-3 to P-151 with >150 hours) to carry out the work specified in Beech Service Instruction No. 0342‑132 on the inboard elevator hinge bracket to maintain airworthiness. Compliance is mandatory within 100 flight hours after 31 December 1970, and costs/implementation are the operators’ responsibility under the Civil Aviation Safety Authority order.

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Current sections

Direct links to the current provisions in AD/BEECH 60/9 - Inboard Elevator Hinge Bracket.

AD/BEECH 60/9 - Inboard Elevator Hinge Bracket

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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 60 (Duke) Series Aeroplanes

AD/BEECH 60/9 Inboard Elevator Hinge Bracket 12/70

Applicability: Models 60 and A60 with S/Nos. P-3 to P-151 which have more than 150 hours’ time in service.

Requirement: Action in accordance with Beech SI No. 0342-132.

Note: FAA AD 70-22-3 refers.

Compliance: Within 100 hours’ time in service after 31 December 1970.

Source text

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