AD/HU 369/63 - Landing Gear Struts and Feet - Inspection

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

Legislation au F2006B10727 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 369/63 Landing Gear Struts and Feet - Inspection 2/85

Applicability: All 500C model 369HS Series. Requirement: Hughes S.I.N. HN-196.

Compliance: Within 300 hours time in service after 28 February 1985.

 

Background: Cracking of certain P/N landing gear struts and feet is suspected. Revised corrosion prevention and sealing techniques and torque load values for the landing gear feet/strut attach bolts are also introduced.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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.