AD/UH-1/2 - Tail Rotor Slider

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

Legislation au F2006B07531 In force Legislative Instrument

Legislation content

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Bell UH-1 Series Helicopters

 

AD/UH-1/2 Tail Rotor Slider  4/97 DM

 

Applicability: All models.

 

Requirement: Measure the outside diameter of the splined shaft (barrel) of the slider Part Number 204-010-720-3, or Part Number 204-010-720-003 at two points that are 90 apart on the outside circumference, at ½” to 1” from either end of the slider. Replace any slider which measures less than 1.300”.

 

Note: FAA AD 97-01-06 refers.

 

Compliance: Within 5 hours time in service after 12 February 1997.

 

Background: US Army “Breakout” spares of this item have been discovered with less than the minimum wall thickness. This Directive is to prevent a possible fatigue failure of a defective slider which would result in the loss of the tail rotor.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.