Commonwealth legislation

AD/BELL 206/19 Amdt 1 - Tail Rotor Pedal Controls - Inspection

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This AD mandates recurring inspections (≤100 flight hours) of the tail rotor pedal spring and friction adjustment on specified Bell/Agusta 206 helicopters, with re‑adjustment as required per Section IV of the Maintenance and Overhaul Instructions. It affects owners/operators and maintenance organisations, who bear inspection and adjustment costs; the intent is to reduce tail‑rotor pedal‑control failures by enforcing regular preventive maintenance.

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Current sections

Direct links to the current provisions in AD/BELL 206/19 Amdt 1 - Tail Rotor Pedal Controls - Inspection.

AD/BELL 206/19 Amdt 1 - Tail Rotor Pedal Controls - 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 Canada (BHTC) 206 and Agusta Bell 206 Series Helicopters

AD/BELL 206/19

Amdt 1

Tail Rotor Pedal Controls - Inspection 6/70

Applicability: All model AB-206A fitted with hydraulically boosted tail rotor pitch control; and All model 206A with S/Nos. 4 to 497.

Requirement: Check the tail rotor pedal spring and friction adjustment and re- adjust as necessary in accordance with the requirements of Section IV the Maintenance and Overhaul Instructions.

Compliance: At intervals not exceeding 100 hours time in service. Background: AD/Agusta 206/10A equivalent.

Source text

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