EASA Regulations for Airbus Helicopters EC 130 T2

22 airworthiness directives and regulations affecting Airbus Helicopters EC 130 T2.

EASA AD 2018-0273

SUPERSEDED BY EASA AD 2022-0083

EASA Airworthiness Directive 2018-0273 is an airworthiness directive issued by the European Aviation Safety Agency concerning SAFRAN Helicopter Engines ARRIEL 2D, 2E, and 2N models. It applies to these engines installed on Airbus Helicopters AS 350 B3 (H125), EC 130 T2 (H130), and MBB-BK117 D-2 (EC 145 T2 or H145) helicopters. The directive mandates compliance with updated airworthiness limitations and maintenance tasks as specified in the latest SAFRAN ARRIEL 2 Maintenance and Overhaul Manuals.

Dec 13, 2018

Airworthiness DirectiveMaintenanceSafety MgmtSafran ARRIEL 2Airbus Helicopters AS 350 B3Airbus Helicopters EC 130 T2MBB-BK117 D-2

EASA AD 2018-0182

Tail Rotor — Blade — Life Limit / Re-identification

EASA Airworthiness Directive 2018-0182 is an airworthiness directive affecting Airbus Helicopters EC 130 B4 and EC 130 T2 models. It addresses the life limit and re-identification requirements for tail rotor blades with specific part numbers, ensuring continued airworthiness and safety. The directive mandates compliance with new service life limits and proper identification of affected tail rotor blades.

Aug 28, 2018

Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters AS 350Airbus Helicopters EC 130Airbus Helicopters EC 130 B4Airbus Helicopters EC 130 T2