AD/BELL 206/98 - Main Rotor Blade - Inspection

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Legislation au F2006B04545 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 Canada (BHTC) 206 and Agusta Bell 206 Series Helicopters

 

AD/BELL 206/98 Main Rotor Blade - Inspection 5/85

TX

Applicability: All models 206L and 206L-1 with S/Nos 45001 to 45790 and 46601 to 46617. All model 206L-3 with S/Nos 51001 to 51109, 51111 to 51117 and 51119 to 51124.

 

Requirement: Bell Alert Service Bulletin No. 206L-85-35.

 

Compliance: PART 1: At each daily inspection after 22 March 1985 until compliance with Part 2.

 

Note: This inspection may be accomplished by the pilot in command in which case he/she shall enter and certify for this AD in Col. 2 Part 3 of the Maintenance Release on each occasion.

 

PART 2: Prior to 1 June 1985.

 

Background: The manufacturer reports cases of chordwise cracking.

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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.