AD/AC-CLA/5 - Shock Strut Assembly
1AD/AC-CLA/5 - Shock Strut Assembly
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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 4/1975,Aircraft below 5700 kg,Aircraft Parts and Development (CALL AIR) A-9 Series Aeroplanes,Shock Strut Assembly,5 title: Airworthiness Directive - AD/AC-CLA/5 - Shock Strut Assembly
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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 Aircraft Parts and Development (CALL AIR) A-9 Series Aeroplanes
AD/AC-CLA/5 Shock Strut Assembly 4/75
Applicability: All A-9 series.
Requirement: Main landing gear shock strut assemblies P/N 12018 shall be disassembled and inspected for general condition.
Note: Particular attention should be paid to the bore of the tube for reduction of wall thickness due to contact with the inner spring.
Compliance: At next major inspection after 30 April 1975 and thereafter at each major inspection.