Commonwealth legislation

AD/BEECH 36/37 - 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This Act has been repealed and is no longer in force. It is retained for historical reference.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 Airworthiness Directive requires owners of specified Beechcraft Bonanza models/serial ranges to inspect the wing forward spar carry-through structure for cracks, following the procedures in FAA AD 91-14-13 (with Beechcraft Service Bulletin 2360 as guidance). Repeated inspections and immediate repair or reinforcement if cracks are found are mandated to prevent potential in-flight structural failure.

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Current sections

Direct links to the current provisions in AD/BEECH 36/37 - Wing Forward Spar Carry-Through Structure.

AD/BEECH 36/37 - 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 36 (Bonanza) Series Aeroplanes

AD/BEECH 36/37 Wing Forward Spar Carry-Through Structure 10/91

Applicability: Model 36 and A36 with serial numbers E-1 through E-2397.

Model A36TC and B36TC with serial numbers EA-1 through EA-471.

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.