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AD/B-2/20 - Increased Tail Rotor Control - Modification
1AD/B-2/20 - Increased Tail Rotor Control - 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 Brantly B-2 Series Helicopters
AD/B-2/20 Increased Tail Rotor Control - Modification NK
Applicability: Model B-2 prior to S/No. 112. Document: 1. Brantly SB No. 15; or
- FAA AD 61-18-2.
Compliance: Forthwith.
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