AD/ROBIN/20 - Main Gear Torque Link Attachment
1AD/ROBIN/20 - Main Gear Torque Link Attachment
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text Robin Aviation Series Aeroplanes
AD/ROBIN/20 Main Gear Torque Link Attachment 13/94
Applicability: Model HR100/250TR and HR100/285TR.
Requirement: Action in accordance with Avions Pierre Robin Service Bulletin 134.
Note: DGAC AD 94-129(A) refers.
Compliance: Unless already accomplished, within 25 hours time in service after 8 December 1994, and thereafter at intervals as specified in the Requirement Document.
Background: The DGAC requires an inspection in response to field reports of cracks on the strut torque link welded attachment points.