AD/HU 269/18 - Tail Boom - Inspection

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

Legislation au F2006B10592 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

 


Schweizer (Hughes) 269 Series Helicopters

 

AD/HU 269/18 Tail Boom - Inspection 11/67

Applicability: Models 269A and 269B.

 

Requirement:  Visually inspect the tail boom for cracks originating at the bolts attaching the tail rotor transmission housing to the boom and also the horizontal stabiliser forward mounting bolt.

 

Compliance: At intervals not exceeding 50 hours time in service after 13 May 1966.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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.