AD/HU 369/17 - Tail Rotor Drive System - Inspection
1AD/HU 369/17 - Tail Rotor Drive System - 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 McDonnell Douglas (Hughes) and Kawasaki 369 Series Helicopters
AD/HU 369/17 Tail Rotor Drive System - Inspection 6/75
Applicability: All models equipped with metal tail rotor blades and all models with drive shafts not previously indexed.
Document: Hughes SIN No. HN-86.
Compliance: For Part 1 - Within 100 hours time in service after 30 June 1975.
For Part 2 - At intervals not exceeding 100 hours time in service after 30 June 1975.