Commonwealth legislation

AD/BELL 205/15 - Tail Rotor Hub Assembly - Inspection

RepealedCTH

This Act has been repealed and is no longer in force. It is retained for historical reference.

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

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This directive requires owners and operators of specific Bell 205A-1 helicopters to inspect the tail rotor hub assembly (part number 212-010-701) every 25 flight hours. The inspections must follow Bell Helicopter's Service Bulletin No. 205-05-73-5 and began on 31 October 1973. This safety measure helps prevent mechanical failure in the tail rotor system, which is critical for helicopter control.

Who it affects: Operators of Bell 205A-1 helicopters with a specific tail rotor hub part.

What you must do: Inspect the tail rotor hub assembly according to the manufacturer's service bulletin at least every 25 hours of flight time.

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AD/BELL 205/15 - Tail Rotor Hub Assembly - Inspection

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

View image in the official source Bell Helicopter Textron 205 Series Helicopters

AD/BELL 205/15 Tail Rotor Hub Assembly - Inspection 10/73

Applicability: All model 205A-1 equipped with Tail Rotor Hub Assy P/N 212-010-701 (SI 205-38 refers).

Document: Bell SB No. 205-05-73-5.

Compliance: At intervals not exceeding 25 hours time in service after 31 October 1973.

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.