Commonwealth legislation

AD/BELL 206/122 - Tail Rotor Blade

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This airworthiness directive orders operators of listed Bell/Agusta 206-series helicopters with specified tail-rotor blade part numbers to inspect blades and remove from service any blade whose serial number appears in the manufacturer’s Alert Service Bulletin. (Requirement; Compliance: prior to further flight.) Operators bear the cost and operational disruption of inspections and any replacement; nondestructive testing may not reliably detect the defect, so removal is based on serial-number identification in the bulletin.

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Current sections

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AD/BELL 206/122 - Tail Rotor Blade

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

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Bell Helicopter Textron Canada (BHTC) 206 and Agusta Bell 206 Series Helicopters

AD/BELL 206/122 Tail Rotor Blade 12/90 TX

Applicability: All model 206L, 206L-1, and 206L-3 helicopters equipped with tail rotor blades P/N 206-016-201-127.

All model 206A, 206A-1, 206B-1, 206JRII, 206JRIII, TH-57 series, and OH-58B

helicopters equipped with tail rotor blades P/N 206-016-201-125 or -127.

Requirement: a. For model 206L, 206L-1, and 206L-3; inspect the tail rotor blades, and remove from service any blade with a serial number identified in Bell Alert Service Bulletin No 206L-90-71.

b. For model 206A, 206A-1, 206B-1, 206BJRII, 206BJRIII, TH-57 series, and OH- 58B; inspect the tail rotor blades, and remove from service any blade with a serial number identified in Bell Alert Service Bulletin No 206-90-58.

Compliance: Prior to further flight.

Background: An incident was recently reported to the manufacturer in which one tail rotor blade tip weight became dislodged in flight. Investigation has revealed that blades having 5/16 inch diameter threaded tip weights at the centre tip location are suspect. Non- destructive testing methods may not positively identify the condition.

Source text

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

1 AD/BELL 206/122 - Tail Rotor Blade