AD/BEECH 35/63 - Wing Forward Spar Carry-Through Structure
1AD/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
Image unavailable in extracted text 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.