AD/S-76/43 - Tail Rotor Servo Actuator Linkage

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

Legislation au F2006B06724 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

 


Sikorsky S-76 Series Helicopters

 

AD/S-76/43 Tail Rotor Servo Actuator Linkage 10/86

Applicability: All model S-76A Helicopters.

 

Requirement: Inspect and modify in accordance with Sikorsky S76 Alert Service Bulletin No. 76- 67-24 and HR Textron Service Bulletin No. SB272.

 

Compliance: Inspect - within 25 hours time in service after 31 October 1986 and thereafter at intervals not exceeding 25 hours time in service until modification is carried out.

 

Modify - prior to 31 November 1986.

 

Background:  The Manufacturer has received reports which indicate possible bolt misalignment on the servo actuator input crank assembly, causing fretting of the bolt.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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.