AD/HU 369/23 - Main Rotor Hub Lead Lag Link - Inspection
1AD/HU 369/23 - Main Rotor Hub Lead Lag Link - 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 369/23 Main Rotor Hub Lead Lag Link - Inspection 3/77
Applicability: All 500 model 369H with lead lag links P/Nos. 369A1234, 369A1234-7, 80-369H1234 and lead lag link assembly P/No. 369H1203.
Document: Hughes SIN No. HN-109.
Compliance: Within 100 hours time in service after 31 March 1977 and thereafter at intervals not exceeding 100 hours time in service.