RegNotify

EASA Regulations for Airbus Helicopters EC 120 B

24 airworthiness directives and regulations affecting Airbus Helicopters EC 120 B.

EASA AD 2019-0272R1

SUPERSEDED BY EASA AD 2021-0069

EASA Airworthiness Directive 2019-0272R1 is an amendment addressing safety concerns for Airbus Helicopters EC 120 B models. It mandates inspections and potential replacement of the tail rotor hub body, part number C642A0100103, to prevent loss of tail rotor drive and yaw control. The directive includes detailed inspection and replacement procedures to ensure continued airworthiness.

Nov 18, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters EC 120 B

EASA AD 2019-0139

SUPERSEDED BY EASA AD 2021-0046

EASA Airworthiness Directive 2019-0139 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all Airbus Helicopters EC 120 B helicopters. It addresses the inspection and replacement requirements for main rotor hub scissors attachment bolts, specifically part number C623A21101, to prevent potential failure due to corrosion and mechanical stress. The directive mandates inspections, markings, and corrective actions to ensure continued safe operation of the affected helicopters.

Jun 12, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters EC 120 B

EASA AD 2018-0183

Tail Rotor — Blade — Life Limit / Re-identification

EASA Airworthiness Directive 2018-0183 is an airworthiness directive addressing tail rotor blades on Airbus Helicopters EC 120 B helicopters. It applies to tail rotor blades with part numbers C642A0300103, C642A0300104, and C642A0300105. The directive mandates re-identification and implementation of a new service life limit for certain tail rotor blades due to changes in manufacturing processes.

Aug 28, 2018
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters EC 120 B