AD/BELL 206/50 - Main Rotor Pitch Link Tubes - Inspection
1AD/BELL 206/50 - Main Rotor Pitch Link Tubes - Inspection
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text Bell Helicopter Textron Canada (BHTC) 206 and Agusta Bell 206 Series Helicopters
AD/BELL 206/50 Main Rotor Pitch Link Tubes - Inspection 6/73
Applicability: All models.
Document: Bell SB No. 206-04-2-73-1.
Compliance: Initially within 25 hours time in service after 25 May 1973 and thereafter in accordance with the requirement document.
Background: AD/Agusta 206/36 equivalent.