Commonwealth legislation

AD/BEECH 35/63 - Wing Forward Spar Carry-Through Structure

RepealedCTH

This Act has been repealed and is no longer in force. It is retained for historical reference.

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This directive requires owners/operators of specified Beechcraft Model 35 Bonanza aircraft (serials D-4866 to D-10403) to inspect the wing forward spar carry-through structure for cracks, perform recurring inspections, and repair or reinforce any defects.

It adopts FAA AD 91-14-13 (refer to Beechcraft Service Bulletin 2360) to address discovered load-bearing spar cracks that could cause structural failure; Australian compliance effective 3 October 1991.

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Current sections

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AD/BEECH 35/63 - Wing Forward Spar Carry-Through Structure

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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 35 (Bonanza) Series Aeroplanes

AD/BEECH 35/63 Wing Forward Spar Carry-Through Structure 10/91

Applicability: Model H35, J35, K35, M35, N35, P35, S35, V35, V35A and V35B with serial numbers D-4866 through D-10403.

Requirement: Action in accordance with the Technical Requirements of FAA AD 91-14-13 Amdt 39-7054.

Note: Beech SB 2360 refers.

Compliance: As specified in Requirement Document with a revised effective date of 3 October 1991, for Australian registered aircraft.

Background: The FAA has received reports of cracks in the wing front carry-through frame structure. This Directive requires initial and repetitive inspections and repair or reinforcement if found cracked.

Source text

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