AD/BELL 206/5 - Cyclic Pitch Control System Lever - Inspection and Modification
1AD/BELL 206/5 - Cyclic Pitch Control System Lever - Inspection and Modification
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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 206/5 Cyclic Pitch Control System Lever - Inspection and Modification
7/68
Applicability: All model 206A with S/Nos. 6 to 10, 12 to 79, 81 to 83 85 to 91, 93 to 97 and 99 to
Document: Bell SB No. 206A-2.
Compliance: Inspect within 10 hours time in service and modify within 100 hours time in service after 6 June 1968.