AD/FU24/61 - Main Landing Gear Torque Link Brackets - Inspection/Replacement
meta-content-style-type: text/css meta-content-type: application/xhtml+xml; charset=utf-8 meta-generator: Aspose.Words for .NET 22.10.0
?xml version="1.0" encoding="utf-8" standalone="no"?>
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
View image in the official source Airparts (NZ) Ltd. FU 24 Series Aeroplanes
AD/FU24/61 Main Landing Gear Torque Link Brackets - Inspection/Replacement
Applicability: All Series FU24.
7/83
Requirement: Remove from service any torque link brackets P/N 245129L and 245129R fitted to aircraft or spare undercarriage assemblies which were supplied on release notes dated 27 March 1980 to 5 May 1983.
Compliance: Within 100 hours time in service after 31st July 1983.
Background: Failure of a bracket in service has been attributed to incorrect heat treatment.