AD/ROBIN/2 - Flap Control Mechanism Dented Plate - Inspection
1AD/ROBIN/2 - Flap Control Mechanism Dented Plate - Inspection
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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/2 Flap Control Mechanism Dented Plate - Inspection 8/81
Applicability: All models R1000.
Document: Avions Pierre Robin SB No. 88.
Compliance: Within 100 hours time in service after 31 August, 1981.
Background: The manufacturer advises that some cracks have been found around the axle of the flap control dented plate.