EASA Regulations for Airbus Helicopters AS 332

110 airworthiness directives and regulations affecting Airbus Helicopters AS 332.

EASA AD 2016-0232R1

Rotor Drive(s) — Main Gear Box / Emergency Spraying System — Modification / Functional Test

EASA Airworthiness Directive 2016-0232R1 is an updated regulatory requirement affecting Airbus Helicopters EC 225 LP models. It addresses issues related to oil leaks from the main gearbox caused by inadvertent opening of the emergency lubrication system valve during engine start-up. The directive mandates modifications and functional testing to ensure continued safe operation of the main gearbox lubrication system.

Dec 12, 2019

Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SA 330Airbus Helicopters AS 332Airbus Helicopters EC 225Airbus Helicopters EC 225 LP

EASA AD 2018-0142R1

SUPERSEDED BY EASA AD 2024-0100

EASA Airworthiness Directive 2018-0142R1 is an amendment addressing Airbus Helicopters AS 332 C, C1, L, and L1 models equipped with dual hoist installations and de-icing systems. This directive focuses on mitigating a vibration issue around 12 Hz caused by specific helicopter configurations that could lead to structural failure or loss of control. It provides requirements for removal of certain dual hoist parts or the de-icing system, or alternatively, operational flight envelope limitations for AS 332 L and L1 helicopters.

Dec 9, 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 2019-0295

SUPERSEDED BY EASA AD 2021-0222

EASA Airworthiness Directive 2019-0295 is an airworthiness directive issued by the European Union Aviation Safety Agency concerning Airbus Helicopters AS 332 C, C1, L, and L1 models. It addresses corrosion found on the main gearbox suspension bar attachment fittings and screws, which could lead to structural failure and detachment of the suspension bars. The directive mandates inspections and corrective actions to ensure continued airworthiness.

Dec 5, 2019

EASA AD 2019-0287

Equipment / Furnishings — External Life Raft Jettison System / Inflation Cylinder Percussion System / Bellcrank — Inspection

EASA Airworthiness Directive 2019-0287 is an airworthiness directive addressing Airbus Helicopters EC 225 LP models equipped with emergency life rafts installed in the multi-purpose sponsons. It focuses on inspection, cleaning, lubrication, and replacement of the external life raft jettison system's inflation cylinder percussion system bellcranks to prevent jamming issues. The directive applies to specific bellcrank part numbers and mandates corrective actions to ensure safe release of life rafts during emergencies.

Nov 27, 2019

Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SA 330Airbus Helicopters AS 332Airbus Helicopters EC 225Airbus Helicopters EC 225 LP

EASA AD 2019-0088R1

Placards and Markings — Inspection / Installation

The document titled "Placards and Markings — Inspection / Installation" applies to Airbus Helicopters models SA 330, AS 332, EC 225, SA/AS 365, and EC 155. It provides guidance on the inspection and proper installation of placards and markings on these helicopter types to ensure compliance with safety and regulatory standards. The document aims to maintain the visibility and legibility of critical information displayed on the aircraft.

Nov 8, 2019

OtherMaintenanceSafety MgmtAirbus Helicopters SA 330Airbus Helicopters AS 332Airbus Helicopters EC 225Airbus Helicopters SAAirbus Helicopters AS 365Airbus Helicopters EC 155Airbus Helicopters SA 365

EASA AD 2019-0195

SUPERSEDED BY EASA AD 2020-0086

EASA Airworthiness Directive 2019-0195 is an airworthiness directive issued by the European Union Aviation Safety Agency concerning Airbus Helicopters AS 332 and SA 330 models. It addresses inspection and replacement requirements for tail rotor hub assembly components, specifically flapping hinge components and spindle bolts, to prevent potential failures that could lead to loss of helicopter control.

Aug 13, 2019

Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SA 330Airbus Helicopters AS 332Airbus Helicopters EC 225

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

EASA AD 2019-0157

Rotor(s) — Main Rotor Hub Drag and Flapping Hinges — Inspection

Rotor(s) — Main Rotor Hub Drag and Flapping Hinges — Inspection is an airworthiness directive applicable to AIRBUS HELICOPTERS models SA 330, AS 332, and EC 225. The document mandates inspections of the main rotor hub drag and flapping hinges to ensure continued airworthiness and safety. It targets specific components critical to rotor integrity on these helicopter types.

Jul 3, 2019

Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SA 330Airbus Helicopters AS 332Airbus Helicopters EC 225

EASA AD 2019-0152-E

SUPERSEDED BY EASA AD 2023-0148

EASA Airworthiness Directive 2019-0152-E is an emergency directive addressing Airbus Helicopters EC 225 LP models equipped with certain main gearboxes (MGB) identified by specific part numbers. The directive mandates inspection and replacement of affected MGBs and installation of operational restrictions related to the ENG1 Training Idle switch. It aims to prevent reduced power transfer capacity in one-engine inoperative scenarios due to detected wear and damage in the main gearbox components.

Jun 28, 2019

Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SA 330Airbus Helicopters AS 332Airbus Helicopters EC 225Airbus Helicopters EC 225 LP

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

EASA AD 2019-0108

Main Rotor Drive — Main Gearbox Particle Detector — Replacement

EASA Airworthiness Directive 2019-0108 is an airworthiness directive issued by the European Union Aviation Safety Agency concerning Airbus Helicopters SA 330 J models. It mandates the replacement of main gearbox particle detectors with an improved version to enhance safety monitoring. This directive applies to all serial numbers of the SA 330 J helicopter.

May 17, 2019

Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SA 330Airbus Helicopters AS 332Airbus Helicopters EC 225Airbus Helicopters SA 330 J

EASA AD 2019-0107

SUPERSEDED BY EASA AD 2020-0061

EASA Airworthiness Directive 2019-0107 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus Helicopters AS 332 L2 and EC 225 LP models. The directive addresses issues with the window jettisoning system on specific serial numbers of these helicopters to ensure safe evacuation during emergencies.

May 16, 2019

Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SA 330Airbus Helicopters AS 332Airbus Helicopters EC 225Airbus Helicopters AS 332 L2Airbus Helicopters EC 225 LP

EASA AD 2019-0102

SUPERSEDED BY EASA AD 2019-0287

EASA Airworthiness Directive 2019-0102 is an airworthiness directive affecting Airbus Helicopters EC 225 LP models equipped with emergency life rafts installed in multi-purpose sponsons with modification 07 25749. The directive addresses issues with the life raft release bellcranks, specifically part numbers 332A41-4396-20 and 332A41-4396-21, which may jam due to foreign coating material or corrosion. It mandates inspections, cleaning, lubrication, and eventual replacement of affected parts to ensure proper life raft deployment during emergencies.

May 9, 2019

Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SA 330Airbus Helicopters AS 332Airbus Helicopters EC 225Airbus Helicopters EC 225 LP

EASA AD 2019-0092

SUPERSEDED BY EASA AD 2021-0156

EASA Airworthiness Directive 2019-0092 is an airworthiness directive issued for Airbus Helicopters EC 225 LP models. It addresses a safety concern involving the left hand side engine fuel supply hose, part number 704A34416087, which may become twisted and restrict fuel flow, potentially causing engine power loss during flight. The directive mandates inspection and corrective actions to ensure continued airworthiness.

Apr 26, 2019

Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SA 330Airbus Helicopters AS 332Airbus Helicopters EC 225Airbus Helicopters EC 225 LP

EASA AD 2019-0021

[Correction] Rotorcraft Flight Manual / Emergency Procedures — Amendment ; Navigation — Attitude and Heading Reference System — Modification

The [Correction] Rotorcraft Flight Manual / Emergency Procedures — Amendment ; Navigation — Attitude and Heading Reference System — Modification is a regulatory document affecting AIRBUS HELICOPTERS models SA 330, AS 332, and EC 225. It addresses corrections and modifications related to the rotorcraft flight manual emergency procedures and updates to the navigation system, specifically the attitude and heading reference system. This amendment ensures updated operational guidance and system modifications for these helicopter types.

Feb 4, 2019

CorrectionFlight OpsSafety MgmtAirbus Helicopters SA 330Airbus Helicopters AS 332Airbus Helicopters EC 225

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

EASA AD 2018-0272

SUPERSEDED BY EASA AD 2021-0239

EASA Airworthiness Directive 2018-0272 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus Helicopters SA 330 J models. It mandates inspections of the main gearbox particle detectors and bottom housing (oil sump) to detect potential failures of the second stage planet gear, which could lead to loss of helicopter control.

Dec 13, 2018

Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SA 330Airbus Helicopters AS 332Airbus Helicopters EC 225Airbus Helicopters SA 330 J

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

EASA AD 2018-0248

SUPERSEDED BY EASA AD 2019-0195

EASA Airworthiness Directive 2019-0195 is an airworthiness directive applicable to Airbus Helicopters models SA 330, AS 332, and EC 225. This directive supersedes previous related directives and addresses safety concerns specific to these helicopter types. It provides updated instructions to ensure continued airworthiness and operational safety.

Nov 15, 2018

Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SA 330Airbus Helicopters AS 332Airbus Helicopters EC 225

EASA AD 2018-0209

Fuselage — Fuel Draining System — Modification

EASA Airworthiness Directive 2018-0209 is an official regulatory document addressing Airbus Helicopters AS 332 series models, including AS 332 C, C1, L, L1, and L2. This directive mandates a modification to the fuel draining system of these helicopters to enhance safety. The modification involves removing fuel tank drain plugs to prevent fuel accumulation and reduce fire risk.

Sep 21, 2018

Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SA 330Airbus Helicopters AS 332Airbus Helicopters EC 225