AD/B-2/20 - Increased Tail Rotor Control - Modification (Cth)
Federal Register of Legislation
Full text
Select any passage to save a personal note with optional tags.
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
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
2. FAA AD 61-18-2.
Compliance: Forthwith.
s