AD/BELL 205/46 - Anti-Torque Control System - Modification to Pushrod Status
1AD/BELL 205/46 - Anti-Torque Control System - Modification to Pushrod Status
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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 205 Series Helicopters
AD/BELL 205/46 Anti-Torque Control System - Modification
to Pushrod Status
12/79
Applicability: All model 205A-1. Document: 1 Bell SB No. 205-78-5; or
- FAA AD 76-12-07, revised September 21, 1979. Compliance: Before 31 December 1979.
Background: Numerous cases have occurred of cracking to tail rotor control chain links. the manufacturer has introduced an alternative control system which utilises pushrods.