FAA Proposes Superseding Bell 212/204/205 AD

AINmxReports » April 17, 2013
April 17, 2013, 12:40 PM

The FAA is superseding an existing airworthiness directive for the Bell 212 and adopting requirements for Bell 204B, 205A, 205A-1, 205B and 210 helicopters with certain part-numbered main rotor hub inboard strap fittings. The AD requires magnetic particle inspection of the fittings for a crack, and if a crack exists, replacing the fittings with airworthy fittings. It was prompted by reports of additional cracked fittings and the determination that additional part-numbered fittings may not have been manufactured in accordance with approved manufacturing processes and controls. These actions are intended to identify a crack in the fitting, which may lead to the fitting’s failure, loss of a main rotor blade and subsequent loss of the helicopter.

Share this...

Please Register

In order to leave comments you will now need to be a registered user. This change in policy is to protect our site from an increased number of spam comments. Additionally, in the near future you will be able to better manage your AIN subscriptions via this registration system. If you already have an account, click here to log in. Otherwise, click here to register.

 
X