AD/HU 269/78 - Tail Rotor Pitch Control Link Assembly

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

Legislation au F2006B10637 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 269/78 Tail Rotor Pitch Control Link Assembly 6/86

DM

 

Applicability: All model 269A, 269A-1 and 269C Helicopters.

 

Requirement: Action in accordance with Schweizer Service Information Notice No. N198. Compliance:               Within 50 hours time in service after 16 May 1986.

For spares, before installation in an aircraft.

 

Background:  The inspection and rework procedure called for ensures correct clearance between tail rotor pitch links and pitch control housing assembly.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.