EASA AD 2025-0001
Tail Rotor — Rotor Head Slide of the Control Plate — Inspection
EASA Airworthiness Directive 2025-0001 is an airworthiness directive addressing Airbus Helicopters AS 332 C, C1, L, and L1 models. It mandates a one-time inspection of the tail rotor head slide of the control plate to detect corrosion, scores, scratches, or cracks. The directive provides instructions for corrective actions including repair or replacement of affected parts to ensure continued safe operation.