Federal Register of Legislation
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES
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.
We try to embed the page this law was scraped from. If the site blocks framing, you still get the link and a local excerpt.
Last checked with source on —
Checking whether the official page can be embedded…
Plain-English simplify of this law: a short summary, key points, and both sides of the argument. Generated on first view via Replicate, then cached. Vote on what helps your study.
No study brief is cached for this law yet. Sign up to generate a plain-English brief.
Sign up to generate