Manufacturer
Bell
Number
FAA 2020-12-10
Model(s)
205A, 205A-1, 205B, 212, 412, 412CF, and 412EP
Published Date
Effective Date
Summary
Supersedes but retains requirements of AD 2011-12-08, which mandated a one-time inspection of the tail rotor blade for corrosion and pitting. New AD excluded certain tail rotor blades from the applicability. Prompted by new manufacturing and inspection procedures implemented by Bell that correct the unsafe condition on more recently manufactured tail rotor blades.
UUID
318