CTHRepealedLegislation
AD/HU 369/30 - Main Rotor Pitch Control Rod - Replacement
1AD/HU 369/30 - Main Rotor Pitch Control Rod - Replacement
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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 McDonnell Douglas (Hughes) and Kawasaki 369 Series Helicopters
AD/HU 369/30 Main Rotor Pitch Control Rod - Replacement 11/77
Applicability: All model 369D with S/Nos. 0001D to 0043D. Document: Hughes SIN No. DN-6.
Compliance: Within 100 hours time in service after 30 November 1977.