AD/HU 369/8 - Tail Rotor Blades - Inspection
1AD/HU 369/8 - Tail Rotor Blades - 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 369/8 Tail Rotor Blades - Inspection 2/71 Applicability: All models with tail rotor blades with S/Nos. as listed in Hughes SIN No. HN-19.1. Document: Hughes SIN No. HN-19.1.
Compliance: 1. At each pre-flight inspection for tail rotor assemblies with less than 100 hours time in service as at 10 February 1971.
- Within 10 hours time in service after 10 February 1971 for tail rotor assemblies with more than 100 hours time in service at 10 February 1971.
Note: These inspections may be performed and certified for by the pilot.