AD/BELL 206/39 - Nut P/N 1022A14 Main Rotor Hub Latch Bolt and Blade Retention Bolt - Inspection

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

Legislation au F2006B04494 Not in force Legislative Instrument

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Bell Helicopter Textron Canada (BHTC) 206 and Agusta Bell 206 Series Helicopters

 

AD/BELL 206/39 Nut P/N 1022A14 Main Rotor Hub Latch Bolt

and Blade Retention Bolt - Inspection

Applicability: All models delivered prior to 20 November 1972. Document: Bell SB No. 206-24, or Agusta SB No. BT206-56.


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Compliance: 1. Visual Inspection - At each daily or overnight inspection after 15 December 1972 until the magnetic particle inspection is performed.

 

2. Magnetic Particle Inspection - within 25 hours time in service after 15 December 1972.

 

Background: AD/Agusta 206/28 equivalent.

 

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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.