AD/BEECH 55/28 - Landing Gear Upper and Lower Torque Link Clevis Pins
1AD/BEECH 55/28 - Landing Gear Upper and Lower Torque Link Clevis Pins
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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 3/1972,Aircraft below 5700 kg,Beechcraft 55, 58 and 95-55 (Baron) Series Aeroplanes,Landing Gear Upper and Lower Torque Link Clevis Pins,28 title: Airworthiness Directive - AD/BEECH 55/28 - Landing Gear Upper and Lower Torque Link Clevis Pins
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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 55, 58 and 95-55 (Baron) Series Aeroplanes
AD/BEECH 55/28 Landing Gear Upper and Lower
Torque Link Clevis Pins
Applicability: All models which have exceeded 1000 hours’ time in service.
3/72
Requirement: Remove and inspect the AN or MS lock pins in the upper and lower torque link clevis pins on the main and nose landing gear assemblies. Any pins which exhibit wear or corrosion shall be replaced.
Compliance: Within 100 hours’ time in service after 29 March 1972 and thereafter at intervals not exceeding 3 years.