EASA Regulations for Airbus Helicopters EC 120 B

23 airworthiness directives and regulations affecting Airbus 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SUPERSEDED BY EASA AD 2021-0046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 2018-0186

SUPERSEDED BY EASA AD 2019-0139

EASA Airworthiness Directive 2018-0186 is an airworthiness directive issued for Airbus Helicopters EC 120 B models. It mandates inspection and potential replacement of main rotor hub scissors attachment bolts to address corrosion and damage risks. This directive aims to prevent possible detachment of these bolts, which could lead to loss of helicopter control.

Aug 29, 2018

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