AD/AC/69 - Main Landing Gear Torque Link Pin Retaining Bolt - Inspection
1AD/AC/69 - Main Landing Gear Torque Link Pin Retaining Bolt - Inspection
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/AC/69 - Main Landing Gear Torque Link Pin Retaining Bolt - Inspection.
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 9/1978,Aircraft below 5700 kg,Twin Commander (Gulfstream/Rockwell/ Aerocommander 500, 600 and 700) Series Aeroplanes,Main Landing Gear Torque Link Pin Retaining Bolt - Inspection,69 title: Airworthiness Directive - AD/AC/69 - Main Landing Gear Torque Link Pin Retaining Bolt - Inspection
?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 Twin Commander (Gulfstream/Rockwell/ Aerocommander 500, 600 and 700) Series Aeroplanes
AD/AC/69 Main Landing Gear Torque Link Pin Retaining Bolt - Inspection
9/78
Applicability: All models 500A, 500B, 500U, 500S, 560F, 680F(P), 680FL, 680FL(P), 680T, 680V
and 680W with S/Nos. 871 to 1876, and Model 500S with S/Nos. 3050 and subsequent; All model 681 with S/Nos. 6001 to 6072;
All model 685 with S/Nos. 1200 to 12066;
All models 690, 690A and 690B with S/Nos. 11001 and subsequent.
Document: Rockwell International SL No. 319.
Compliance: Within 25 hours’ time in service after 22 August 1978.