AD/ECUREUIL/5 - Tail Rotor Control Fixed Plate - Inspection of Self Aligning Bearing

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

Legislation au F2006B09355 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

 


Eurocopter AS 350 (Ecureuil) Series Helicopters

 

AD/ECUREUIL/5 Tail Rotor Control Fixed Plate - Inspection

of Self Aligning Bearing


8/79

 

Applicability: All model AS.350 not modified in accordance with AMS 350A.07.6513 and AMS 350A.07.8515.

 

Document: AS.350 SB 05.01.

 

Compliance: At periods not exceeding 50 hours time in service.

 

Background:  Regular inspections are required to ensure that the tail rotor control self aligning bearing is correctly located in the bore of the fixed plate.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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.