EASA AD 2024-0250
Tail Rotor — Rotor Head Bearing Stack of the Spindle-Sleeve Assembly — Life Limit
EASA Airworthiness Directive 2024-0250 is an airworthiness directive affecting Airbus Helicopters SA 330 J and AS 332 C, C1, L, and L1 models. It addresses the tail rotor rotor head bearing stack of the spindle-sleeve assembly by introducing a life limit to prevent fatigue cracks and potential structural failure. The directive mandates replacement of affected bearing stacks to ensure continued safe operation of these helicopters.