AD/BELL 205/65 - Vertical Fin Spar Cap

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Legislation au F2006B04402 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 205/65 Vertical Fin Spar Cap  12/99 DM

Applicability: Model 205A-1 helicopters with Vertical Fin Spar Cap PNo 212-030-447-001 or -101 fitted.

Model 205B helicopters with Vertical Fin Spar Cap PNo 212-030-447-101. Requirement:              Action in accordance with the technical requirements of FAA AD 99-18-02

Amendment 39-11268.

 

Note: The FAA calls out Bell Helicopter Textron Inc. Alert Service Bulletin 205-98- 70 Revision A dated 21 Sept 1998. However, the FAA AD requires inspections and maintenance beyond that of the Bell ASB.

 

Compliance: In accordance with the requirement document, but with a revised with effect date of 6 October 1999.

 

This Airworthiness Directive becomes effective on 6 October 1999.

 

Background: The FAA have issued an AD that inspects the vertical fin spar cap for corrosion, cracking and disbonding. The FAA justification cites 5 accidents involving helicopters of a similar design.

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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.