EASA Regulations for Airbus Helicopters MBB-BK117 C-2

EASA AD 2024-0131

Main Rotor — Control Rod Assembly / Pitch Link Assembly — Inspection

EASA Airworthiness Directive 2024-0131 is an airworthiness directive issued by the European Union Aviation Safety Agency concerning Airbus Helicopters Deutschland GmbH MBB-BK117 C-2 and D-2 helicopters. It mandates inspection of the main rotor control rod assembly and pitch link assembly, specifically parts with certain part numbers, to detect wear in spherical bearings that could affect rotor blade pitch and control.