It does not receive public funding
Editor in chief:

Facebook Twitter Youtube Instagram LinkedIn

Do you want to access to this and other private contents?
Log in if you are a subscriber or click here to request service

FAA Emergency AD on Agusta model A-109E helicopters

Washington, USA - To prevent fatigue failure of the tail rotor blade and subsequent loss of control of the helicopter

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 Docket No. 2002-SW-55-AD; AD 2002-25-51 Agusta S.p.A. (Agusta) Model A109E helicopters PDF Copy (If Available): Preamble Information Regulatory Information 2002-25-51 AGUSTA S.p.A (Agusta): Docket No. 2002-SW-55-AD. Supersedes AD 2002-17-51, Amendment...

AVIONEWS - World Aeronautical Press Agency - 37469

AVIONEWS - World Aeronautical Press Agency