AD/DHC-2/20 - Control Column Torque Tubes - Inspection
1AD/DHC-2/20 - Control Column Torque Tubes - 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-2/20 Control Column Torque Tubes - Inspection 9/80
Applicability: All models DHC-2 and DHC-2 Mk. III. Document: De Havilland Aircraft of Canada SB No. 2/28.
Compliance: Initially inspect within 25 hours time in service after 18 September 1980 and thereafter as noted in De Havilland Aircraft of Canada SB No. 2/28.
Background: Three overseas operators have reported cracks in the horizontal torque tube at the base of the control column.