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

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B03892 Not in force Legislative Instrument

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


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.

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.