AD/BELL 206/98 - Main Rotor Blade - Inspection
1AD/BELL 206/98 - Main Rotor Blade - Inspection
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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.