RegNotify

EASA Regulations for Airbus Helicopters AS 332 L1

28 airworthiness directives and regulations affecting Airbus Helicopters AS 332 L1.

EASA AD 2019-0209

Power Plant — Control and Monitoring Harness — Identification / Replacement

EASA Airworthiness Directive 2019-0209 addresses an unsafe condition in SAFRAN HELICOPTER ENGINES MAKILA 1A and 1A1 turboshaft engines, commonly installed on Airbus Helicopters AS 332 C, C1, L, and L1 models. The directive mandates identification and replacement of certain control and monitoring harnesses that were found to be incorrectly manufactured, potentially causing in-flight activation of the "85% NG" backup law. This AD ensures continued airworthiness by requiring corrective actions on affected parts.

Aug 23, 2019
Airworthiness DirectiveMaintenanceSafety MgmtSafran MAKILA 1Airbus Helicopters AS 332 CAirbus Helicopters AS 332 C1Airbus Helicopters AS 332 LAirbus Helicopters AS 332 L1

EASA AD 2019-0172

Main Rotor — Hub Assembly Lock Washer — Inspection

EASA Airworthiness Directive 2019-0172 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus Helicopters AS 332 C, C1, L, and L1 models. It mandates inspection of the main rotor hub assembly lock washer to ensure correct installation and prevent potential failure. The directive applies to specific main rotor hub assemblies with designated part numbers.

Jul 18, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SA 330Airbus Helicopters AS 332Airbus Helicopters EC 225Airbus Helicopters AS 332 CAirbus Helicopters AS 332 C1Airbus Helicopters AS 332 LAirbus Helicopters AS 332 L1

EASA AD 2019-0109

Tail Rotor — Rotor Blades — Inspection / Modification

EASA Airworthiness Directive 2019-0109 is an airworthiness directive addressing inspection and modification requirements for tail rotor rotor blades on Airbus Helicopters AS 332 C, L, and L1 models equipped with specific tail rotor de-icing units and blades. It targets rotor blades with part number 332A12-0055-XX and aims to prevent structural damage caused by overheating due to uncontrolled power supply to the de-icing system. The directive mandates inspections and modifications to ensure continued safe operation of the affected helicopters.

May 20, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SA 330Airbus Helicopters AS 332Airbus Helicopters EC 225Airbus Helicopters AS 332 CAirbus Helicopters AS 332 LAirbus Helicopters AS 332 L1

EASA AD 2018-0282

Fuselage — Main Gearbox Suspension Bar Rear Attachment Fitting Screws — Inspection

EASA Airworthiness Directive 2018-0282 is an airworthiness directive addressing Airbus Helicopters AS 332 C, C1, L, and L1 models delivered before 01 September 2018. It mandates inspection of the main gearbox suspension bar rear attachment fitting screws, specifically part number 330A22013520, to detect potential elongation and loss of nut tightening torque. The directive aims to prevent structural failure of the main gearbox rear attachment fittings that could lead to detachment of suspension bars.

Dec 19, 2018
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SA 330Airbus Helicopters AS 332Airbus Helicopters EC 225Airbus Helicopters AS 332 CAirbus Helicopters AS 332 C1Airbus Helicopters AS 332 LAirbus Helicopters AS 332 L1

EASA AD 2018-0260

SUPERSEDED BY EASA AD 2023-0194

EASA Airworthiness Directive 2018-0260 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus Helicopters AS 332 C, C1, L, and L1 models. It addresses the life limits and replacement requirements for main gearbox suspension bar fittings and screws to ensure continued airworthiness. The directive applies to specific part numbers related to the main gearbox suspension bar attachment fittings and screws.

Dec 3, 2018
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SA 330Airbus Helicopters AS 332Airbus Helicopters EC 225Airbus Helicopters AS 332 CAirbus Helicopters AS 332 C1Airbus Helicopters AS 332 LAirbus Helicopters AS 332 L1

EASA AD 2018-0066

SUPERSEDED BY EASA AD 2020-0022

EASA Airworthiness Directive 2018-0066 is an airworthiness directive issued by the European Aviation Safety Agency affecting Airbus Helicopters AS 332 L, L1, C, and C1 models. It addresses the inspection and replacement of certain second stage planet gear assemblies in the main gearbox to prevent failure due to higher outer race contact pressures. The directive mandates repetitive inspections and replacement of affected parts to ensure continued safe operation.

Mar 23, 2018
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SA 330Airbus Helicopters AS 332Airbus Helicopters EC 225Airbus Helicopters AS 332 LAirbus Helicopters AS 332 L1Airbus Helicopters AS 332 CAirbus Helicopters AS 332 C1

EASA AD 2018-0042

SUPERSEDED BY EASA AD 2018-0248

EASA Airworthiness Directive 2018-0042 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus Helicopters AS 332 C, AS 332 C1, AS 332 L, AS 332 L1, and SA 330 J models. It mandates inspections of the tail rotor blade flapping hinges to detect damage that could lead to failure and loss of helicopter control. The directive applies to all manufacturer serial numbers of these helicopter models.

Feb 14, 2018
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SA 330Airbus Helicopters AS 332Airbus Helicopters EC 225Airbus Helicopters AS 332 CAirbus Helicopters AS 332 C1Airbus Helicopters AS 332 LAirbus Helicopters AS 332 L1Airbus Helicopters SA 330 J

EASA SIB 2008-56

Main Rotor Blade De-Icing System Distributor Retaining Clamps - Check / Replacement

EASA Safety Information Bulletin 2008-56 is an informational bulletin concerning Eurocopter AS 332 C, C1, L, L1 and SA 330 F, G, J helicopters equipped with main rotor blade de-icing system distributor retaining clamps, part numbers 225000-18454 or D18454 without batch number or letter "V" marking. It addresses a safety issue identified by the French DGAC Emergency Airworthiness Directive UF-2008-008 regarding potential failure of the retaining clamp screws. The bulletin provides guidance on inspection and corrective actions but does not impose mandatory requirements under EASA regulations.

Jun 19, 2008
Safety Information BulletinMaintenanceSafety MgmtAirbus Helicopters AS 332 CAirbus Helicopters AS 332 C1Airbus Helicopters AS 332 LAirbus Helicopters AS 332 L1Aérospatiale SA 330 FAérospatiale SA 330 GAérospatiale SA 330 J