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AD/BEECH 50/15 - Elevator Trim Tab Hinge Beam
1AD/BEECH 50/15 - Elevator Trim Tab Hinge Beam
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meta-content-style-type: text/css meta-content-type: application/xhtml+xml; charset=utf-8 meta-description: CASA Airworthiness Directive meta-generator: Aspose.Words for .NET 22.10.0 meta-keywords: Issue 12/1965,Aircraft below 5700 kg,Beechcraft 50 (Twin Bonanza) Series Aeroplanes,Elevator Trim Tab Hinge Beam,15 title: Airworthiness Directive - AD/BEECH 50/15 - Elevator Trim Tab Hinge Beam
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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 50 (Twin Bonanza) Series Aeroplanes
AD/BEECH 50/15 Elevator Trim Tab Hinge Beam 12/65
Applicability: All models.
Requirement: Visually inspect the elevator trim tab hinge beam (P/N 50/610000/94) for cracking in the flange and web.
Compliance: At intervals not exceeding 250 hours’ time in service.