FAA 2020-19-02

Supersedes AD 2000-22-19, which required repetitively inspecting certain tail rotor blades for skin debonding and a crack. New AD revises the applicability, requires repetitively inspecting affected tail rotor blades with new inspection procedures an,d depending on the inspection results, repairing or replacing the tail rotor blade. It also prohibits installing an affected tail rotor blade unless it has passed the inspections.