AD/BELL 205/2 - Tail Rotor Yoke - Inspection

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

Legislation au F2006B04361 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 205 Series Helicopters

 

AD/BELL 205/2 Tail Rotor Yoke - Inspection 9/68

Applicability: All 205A models fitted with tail rotor yoke P/N 204-010-781-5 or 204-010-781-9.

 

Requirement: Inspect yoke assembly P/N 204-010-781-5 or 204-010-781-9 by magnetic particle method with particular emphasis on the threaded portion of the yoke spindle.

Maximum amperage 1400 amps. DC or 1100 amps. AC. Do not exceed 4200 ampere turns.

 

Compliance: At intervals not exceeding 100 hours time in service, after 1 September 1971.

 

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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.