Commonwealth legislation

AD/BELL 206/5 - Cyclic Pitch Control System Lever - Inspection and Modification

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This Act has been repealed and is no longer in force. It is retained for historical reference.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

2/10 complexity

This mandatory CASA airworthiness directive requires owners/operators of certain Bell 206A helicopters (specific serial numbers) to inspect the cyclic pitch control lever within 10 flying hours and complete the required repair or replacement within 100 flying hours after 6 June 1968, following Bell SB No. 206A-2. It targets a defect that could cause loss of pilot control, posing a serious safety risk.

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Current sections

Direct links to the current provisions in AD/BELL 206/5 - Cyclic Pitch Control System Lever - Inspection and Modification.

AD/BELL 206/5 - Cyclic Pitch Control System Lever - Inspection and Modification

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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 Canada (BHTC) 206 and Agusta Bell 206 Series Helicopters

AD/BELL 206/5 Cyclic Pitch Control System Lever - Inspection and Modification

7/68

Applicability: All model 206A with S/Nos. 6 to 10, 12 to 79, 81 to 83 85 to 91, 93 to 97 and 99 to

Document: Bell SB No. 206A-2.

Compliance: Inspect within 10 hours time in service and modify within 100 hours time in service after 6 June 1968.

Source text

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