EASA Regulations for Airbus Helicopters EC 225

116 airworthiness directives and regulations affecting Airbus Helicopters EC 225.

EASA AD 2022-0016-E

Jan 26, 2022

Equipment / Furnishings — Hoist Attachment Fittings — Inspection

EASA Airworthiness Directive 2022-0016-E is an emergency directive addressing inspection requirements for hoist attachment fittings on Airbus Helicopters AS 332 models C, C1, L, L1, and L2. The directive targets specific front upper, rear upper, and lower hoist attachment fittings with part numbers 332A87-1116-21, 332A87-1117-20, and 332A87-1176-20 respectively. It mandates inspections to detect cracks that could compromise structural integrity and lead to in-flight detachment of the hoist support.

Airworthiness Directive
  • Airbus Helicopters SA 330
  • Airbus Helicopters AS 332
  • Airbus Helicopters EC 225
  • Airbus Helicopters AS 332 C
  • Airbus Helicopters AS 332 C1
  • Airbus Helicopters AS 332 L
  • Airbus Helicopters AS 332 L1
  • Airbus Helicopters AS 332 L2

EASA AD 2021-0184R2

Jan 12, 2022

Tail Rotor — Tail Gearbox Angular Clearance — Inspection

EASA Airworthiness Directive 2021-0184R2 is an updated safety directive addressing the inspection of tail gearbox angular clearance on Airbus Helicopters AS 332 L2 and EC 225 LP models. It mandates repetitive inspections of specific tail gearbox parts to detect angular clearance issues that could lead to structural failure of the tail gearbox drive. The directive applies to tail gearboxes with part numbers 332A36.3001.00, 332A36.3002.00, and 332A36.5001.01.

Airworthiness Directive
  • Airbus Helicopters SA 330
  • Airbus Helicopters AS 332
  • Airbus Helicopters EC 225
  • Airbus Helicopters AS 332 L2
  • Airbus Helicopters EC 225 LP

EASA AD 2017-0042-CN

Jan 3, 2022

CANCELLED: Main Rotor Drive / Engine Oil — Main Gearbox Oil Cooler — Inspection

CANCELLED: Main Rotor Drive / Engine Oil — Main Gearbox Oil Cooler — Inspection is a document concerning Airbus Helicopters models SA 330, AS 332, and EC 225. It originally addressed inspection requirements related to the main rotor drive, engine oil, and main gearbox oil cooler systems. The document has now been officially cancelled and is no longer in effect.

Other
  • Airbus Helicopters SA 330
  • Airbus Helicopters AS 332
  • Airbus Helicopters EC 225

EASA AD 2021-0239

Nov 5, 2021

Time Limits / Maintenance Checks — Main Gearbox / Particle Detectors — Inspection / Modification / Replacement

The document titled 'Time Limits / Maintenance Checks — Main Gearbox / Particle Detectors — Inspection / Modification / Replacement' is an airworthiness directive applicable to AIRBUS HELICOPTERS models SA 330, AS 332, and EC 225. It addresses mandatory maintenance checks and inspections related to the main gearbox and particle detectors, including requirements for their inspection, modification, or replacement. The directive aims to ensure continued airworthiness and safety of these helicopter models by establishing clear maintenance time limits and procedures.

Airworthiness Directive
  • Airbus Helicopters SA 330
  • Airbus Helicopters AS 332
  • Airbus Helicopters EC 225

EASA AD 2021-0222

Oct 6, 2021

Fuselage — Main Gearbox Suspension Bar Attachment Fittings and Screws — Inspection

EASA Airworthiness Directive 2021-0222 is an airworthiness directive addressing Airbus Helicopters AS 332 C, C1, L, and L1 models. It mandates inspections of the main gearbox suspension bar attachment fittings and screws on the fuselage to detect corrosion and prevent potential structural failure. This directive applies to all manufacturer serial numbers of the specified helicopter models.

Airworthiness Directive
  • Airbus Helicopters SA 330
  • Airbus Helicopters AS 332
  • Airbus Helicopters EC 225
  • Airbus Helicopters AS 332 C
  • Airbus Helicopters AS 332 C1
  • Airbus Helicopters AS 332 L
  • Airbus Helicopters AS 332 L1

EASA AD 2021-0196

Aug 23, 2021

Placards and Markings — Emergency Exit Placards — Installation

EASA Airworthiness Directive 2021-0196 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus Helicopters AS 332 and EC 225 models equipped with specific cabin plug doors. The directive mandates the installation of additional emergency exit placards on cabin plug doors to ensure clear and accurate instructions for emergency door operation. This AD applies to helicopters with cabin plug door part numbers 332A221301.XX, 332A251406.XX, and 332P222000.XX.

Airworthiness Directive
  • Airbus Helicopters SA 330
  • Airbus Helicopters AS 332
  • Airbus Helicopters EC 225

EASA AD 2021-0174

Jul 21, 2021

Rotorcraft Flight Manual — Supplements / One-Engine Inoperative Performance Limitations — Amendment

EASA Airworthiness Directive 2021-0174 is an amendment concerning the Rotorcraft Flight Manual supplements related to One-Engine Inoperative performance limitations for Airbus Helicopters AS 332 L2 and EC 225 LP models. The directive addresses discrepancies in the flight manuals regarding stay-up flying capabilities for Category B operations. It mandates updates to the Rotorcraft Flight Manual to ensure compliance with applicable airworthiness standards.

Airworthiness Directive
  • Airbus Helicopters SA 330
  • Airbus Helicopters AS 332
  • Airbus Helicopters EC 225
  • Airbus Helicopters AS 332 L2
  • Airbus Helicopters EC 225 LP

EASA AD 2021-0152R1

Jul 20, 2021

Fuselage — Main Gearbox Suspension Bar Fittings and Screws — Replacement [Life Limitation]

EASA Airworthiness Directive 2021-0152R1 is a regulatory document addressing the replacement and life limitation of main gearbox suspension bar fittings and screws on Airbus Helicopters SA 330 J models. It applies specifically to parts modified in service per Eurocopter France Service Bulletin No. 01.20, excluding those replaced with new parts during the retrofit mod 07 40043. The directive mandates inspection and potential replacement of affected parts to prevent structural failure and loss of helicopter control.

Airworthiness Directive
  • Airbus Helicopters SA 330
  • Airbus Helicopters AS 332
  • Airbus Helicopters EC 225
  • Airbus Helicopters SA 330 J

EASA AD 2021-0156

Jul 2, 2021

Fuel – Engine Fuel Supply Hoses – Inspection / Replacement

EASA Airworthiness Directive 2021-0156 is an airworthiness directive issued for Airbus Helicopters EC 225 LP models concerning the left-hand side engine fuel supply hose, part number 704A34416087. It mandates inspection and replacement of this fuel supply hose to prevent power loss due to fuel flow restriction caused by a twisted hose. The directive applies to all serial numbers of EC 225 LP helicopters and introduces requirements for inspection, corrective actions, and replacement with an improved part.

Airworthiness DirectiveSuperseded
  • Airbus Helicopters SA 330
  • Airbus Helicopters AS 332
  • Airbus Helicopters EC 225
  • Airbus Helicopters EC 225 LP

EASA AD 2021-0086

Mar 24, 2021

Rotors Flight Control — Yaw Control Damper Support — Inspection / Replacement

EASA Airworthiness Directive 2021-0086 is an airworthiness directive addressing the Airbus Helicopters AS 332 L2 model. It mandates inspection and replacement requirements for the yaw control damper support, specifically part number 332A25-1334-00, to prevent structural failure and potential loss of yaw flight control.

Airworthiness Directive
  • Airbus Helicopters SA 330
  • Airbus Helicopters AS 332
  • Airbus Helicopters EC 225
  • Airbus Helicopters AS 332 L2

EASA AD 2021-0075

Mar 16, 2021

Fuselage — Splice of Frame X5295 — Inspection / Repair / Modification

EASA Airworthiness Directive 2021-0075 addresses inspection, repair, and modification requirements for the fuselage splice of frame X5295 on Airbus Helicopters AS 332 L2 and EC 225 LP models. It applies to helicopters equipped with extended aluminium splices installed under specific Airbus Helicopters modifications or service bulletins. The directive mandates inspections and corrective actions to detect and repair cracks that could compromise structural integrity.

Airworthiness Directive
  • Airbus Helicopters SA 330
  • Airbus Helicopters AS 332
  • Airbus Helicopters EC 225
  • Airbus Helicopters AS 332 L2
  • Airbus Helicopters EC 225 LP

EASA AD 2021-0003

Jan 6, 2021

Placards and Markings – Emergency Exit Labels – Installation

EASA Airworthiness Directive 2021-0003 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus Helicopters AS 332 C, C1, L, L1, L2 and EC 225 LP models equipped with specific cabin plug doors (Part Numbers 332A221301.XX or 332AS251406.XX). The directive addresses the installation of additional emergency exit placards on cabin plug doors to improve passenger understanding of emergency door jettisoning procedures.

Airworthiness DirectiveSuperseded
  • Airbus Helicopters SA 330
  • Airbus Helicopters AS 332
  • Airbus Helicopters EC 225
  • Airbus Helicopters AS 332 C
  • Airbus Helicopters AS 332 C1
  • Airbus Helicopters AS 332 L
  • Airbus Helicopters AS 332 L1
  • Airbus Helicopters AS 332 L2
  • Airbus Helicopters EC 225 LP

EASA AD 2020-0022R2

Dec 23, 2020

Time Limits / Maintenance Checks — Main Gear Box / Particle Detectors — Inspection; Main Rotor Drive — Planet Gear Assemblies — Replacement / Modification

EASA Airworthiness Directive 2020-0022R2 is an updated regulatory requirement affecting Airbus Helicopters AS 332 L, L1, C, and C1 models. It addresses inspection, replacement, and modification requirements related to the main gearbox (MGB) planet gear assemblies and particle detectors to mitigate risks associated with gear spalling and cracking. The directive mandates specific inspections and installation of a Full Flow Magnetic Plug (FFMP) device to enhance safety and continued airworthiness.

Airworthiness Directive
  • Airbus Helicopters SA 330
  • Airbus Helicopters AS 332
  • Airbus Helicopters EC 225
  • Airbus Helicopters AS 332 L
  • Airbus Helicopters AS 332 L1
  • Airbus Helicopters AS 332 C
  • Airbus Helicopters AS 332 C1

EASA AD 2020-0281

Dec 16, 2020

Equipment / Furnishings — Hoist Control Power Supply — Modification

EASA Airworthiness Directive 2020-0281 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 a design deficiency related to the hoist control power supply wiring on specific serial-numbered helicopters. It mandates a modification to ensure electrical protection and prevent potential safety hazards.

Airworthiness Directive
  • Airbus Helicopters SA 330
  • Airbus Helicopters AS 332
  • Airbus Helicopters EC 225
  • Airbus Helicopters AS 332 L2
  • Airbus Helicopters EC 225 LP

EASA AD 2018-0204R1

Dec 8, 2020

Air Conditioning — Clearance between Air Conditioning Unit and Landing Light Connectors — Measurement

The document titled Air Conditioning — Clearance between Air Conditioning Unit and Landing Light Connectors — Measurement is a regulatory communication concerning AIRBUS HELICOPTERS models SA 330, AS 332, and EC 225. It addresses the required clearance measurements between the air conditioning units and the landing light connectors on these helicopter types to ensure safe operation and maintenance.

Safety Information Bulletin
  • Airbus Helicopters SA 330
  • Airbus Helicopters AS 332
  • Airbus Helicopters EC 225

EASA AD 2020-0264

Dec 2, 2020

Main Rotor – Mast – Inspection

EASA Airworthiness Directive 2020-0264 is an airworthiness directive issued for Airbus Helicopters EC 225 LP models. It addresses a manufacturing defect in the ceramic balls of the swashplate bearing in the main rotor mast assembly, which could lead to premature bearing failure and reduced helicopter control. The directive mandates inspections and possible replacement of affected main rotor mast assemblies with specified part numbers.

Airworthiness DirectiveSuperseded
  • Airbus Helicopters SA 330
  • Airbus Helicopters AS 332
  • Airbus Helicopters EC 225
  • Airbus Helicopters EC 225 LP

EASA AD 2018-0039R1

Sep 25, 2020

Windows — Jettisoning System — Installation

EASA Airworthiness Directive 2018-0039R1 is a regulatory document addressing the installation of the windows jettisoning system on Airbus Helicopters AS 332 and EC 225 LP models. It mandates modifications to reduce friction between the window seal and the helicopter airframe to ensure proper jettisoning of windows in emergency situations. The directive applies to various AS 332 and EC 225 LP helicopter variants, excluding those already modified according to specified Airbus Helicopters modifications and Alert Service Bulletins.

Airworthiness DirectiveSuperseded
  • Airbus Helicopters SA 330
  • Airbus Helicopters AS 332
  • Airbus Helicopters EC 225
  • Airbus Helicopters EC 225 LP

EASA AD 2020-0141R1

Jul 30, 2020

Main Rotor Drive — Main Gearbox Freewheel Shafts — Replacement ; Placards and Markings — ENG1 Training Idle Switch — Installation / Operational Restriction

EASA Airworthiness Directive 2020-0141R1 is an updated regulatory requirement affecting Airbus Helicopters AS 332 L2 models. It addresses the replacement of main gearbox freewheel shafts and installation of placards related to the ENG1 Training Idle switch to impose operational restrictions during flight. The directive aims to ensure continued airworthiness and safe operation of helicopters equipped with specific main gearbox configurations.

Airworthiness Directive
  • Airbus Helicopters SA 330
  • Airbus Helicopters AS 332
  • Airbus Helicopters EC 225
  • Airbus Helicopters AS 332 L2

EASA AD 2020-0171

Jul 28, 2020

Rotors – Main Gearbox Oil Cooling Fan – Inspection / Replacement

EASA Airworthiness Directive 2020-0171 is an airworthiness directive issued for Airbus Helicopters SA 330 J helicopters. It addresses the risk of main gearbox (MGB) oil cooling fan rotor shaft bearing degradation that could lead to rotor burst and damage to critical hydraulic pipes and flight controls. The directive mandates inspections and replacement of specific MGB oil cooling fan rotor shaft bearings to ensure continued safe operation.

Airworthiness DirectiveSuperseded
  • Airbus Helicopters SA 330
  • Airbus Helicopters AS 332
  • Airbus Helicopters EC 225
  • Airbus Helicopters SA 330 J

EASA AD 2017-0134R2

Apr 16, 2020

Time Limits / Maintenance Checks — Main Gearbox Particle Detector / Oil Filter / Oil Cooler — Inspection Main Rotor Drive — Epicyclic Module — Replacement / Modification / Reduced Service Life Limit

EASA Airworthiness Directive 2024-0198 addresses time limits and maintenance checks for the main gearbox particle detector, oil filter, and oil cooler inspections, as well as replacement, modification, and reduced service life limits for the main rotor drive epicyclic module. This directive applies specifically to Airbus Helicopters models SA 330, AS 332, and EC 225. It aims to ensure continued airworthiness and safety of these helicopter models by updating inspection and replacement requirements.

Airworthiness Directive
  • Airbus Helicopters SA 330
  • Airbus Helicopters AS 332
  • Airbus Helicopters EC 225