AD/BEECH 65/52 - Landing Gear Torque Tube - Inspection and Replacement
1AD/BEECH 65/52 - Landing Gear Torque Tube - Inspection and Replacement
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/BEECH 65/52 - Landing Gear Torque Tube - Inspection and 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
Image unavailable in extracted text 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.