AD/BEECH 65/52 - Landing Gear Torque Tube - Inspection and Replacement
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
View image in the official source Beechcraft 65 and 70 (Queen Air) Series Aeroplanes
AD/BEECH 65/52 Landing Gear Torque Tube - Inspection
and Replacement
Applicability: Model 65-B80 with S/Nos. LD-506 to LD-511. Document: Beechcraft SI No. 1049.
Compliance: Within 100 hours’ time in service after 31 August 1979.
8/79
Background: The landing gear torque tube is to be inspected for elongation or double drilling of the bolt hole where the nose gear drive sprocket attaches.