AD/DHC-2/21 - Flight Controls, Elevator Root Rib - Inspection
1AD/DHC-2/21 - Flight Controls, Elevator Root Rib - 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 DHC-2 (Beaver) Series Aeroplanes
AD/DHC-2/21 Flight Controls, Elevator Root Rib - Inspection 10/80
Applicability: All Model DHC-2 Mk. I, Mk. II and Mk. III. Document: De Havilland Aircraft of Canada SB No. 2/30.
Compliance: Within 100 hours time in service after 31 December 1980 and thereafter at intervals not exceeding 400 hours time in service.
Background: Cracking of the elevator root rib at the torque tube attachment and cracking of the reinforcing doubler in the same area has been reported to the manufacturer.