AD/AC-CLA/3 - Main Landing Gear Attachment
1AD/AC-CLA/3 - Main Landing Gear Attachment
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/AC-CLA/3 - Main Landing Gear Attachment.
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 9/1967,Aircraft below 5700 kg,Aircraft Parts and Development (CALL AIR) A-9 Series Aeroplanes,Main Landing Gear Attachment,3 title: Airworthiness Directive - AD/AC-CLA/3 - Main Landing Gear Attachment
?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 Aircraft Parts and Development (CALL AIR) A-9 Series Aeroplanes
AD/AC-CLA/3 Main Landing Gear Attachment 9/67
Applicability: All A-9 Series.
Requirement: Inspect the main landing attachment points on the wing to fuselage struts P/N 10915- 1 and 10915-2 for cracking in the welded area.
Compliance: At intervals not exceeding 100 hours’ time in service after 1 September 1971.