AD/HU 369/8 - Tail Rotor Blades - Inspection

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B10744 Not in force Legislative Instrument

Legislation content

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


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.

 

2. 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.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Interactions

Authorises

All Versions

Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.