EASA Regulations & Airworthiness Directives

Browse 116 EASA regulations with AI-powered summaries.

Aircraft:AllAirbus A320286Airbus A321285Airbus A319253Airbus A350222Airbus A330220Airbus A318189Airbus A380182Boeing 737175Airbus A340141Airbus A350-941132Airbus BD-500 (A220 Series)123Airbus Helicopters AS 332119Airbus Helicopters EC 225116Airbus Helicopters SA 330116Boeing 787114Show all...
Filtered by: Airbus Helicopters SA 330Clear filter

EASA AD 2019-0102

May 9, 2019

Superseded by EASA AD 2019-0287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.

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

EASA AD 2019-0092

Apr 26, 2019

Superseded by EASA AD 2021-0156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.

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

EASA AD 2019-0021

Feb 4, 2019

[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.

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

EASA AD 2018-0282

Dec 19, 2018

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.

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 2018-0272

Dec 13, 2018

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.

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

EASA AD 2018-0260

Dec 3, 2018

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.

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

EASA AD 2018-0248

Nov 15, 2018

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.

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

EASA AD 2018-0209

Sep 21, 2018

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.

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

EASA AD 2018-0173-E

Aug 8, 2018

Equipment & Furnishings — Hoist Carrier Assembly — Inspection

EASA Airworthiness Directive 2018-0173-E is an emergency directive addressing inspection requirements for the Goodrich electrical hoist carrier assembly installed on Airbus Helicopters AS 332 L2, EC 225 LP, AS 365 N3, and EC175 B models. The directive mandates inspection of specific hoist part numbers to detect incorrect assembly that could lead to carrier assembly loosening and potential load loss. It applies to all serial numbers of the affected helicopter models and requires compliance with Airbus Helicopters Alert Service Bulletins.

Airworthiness Directive
  • Airbus Helicopters EC175
  • Airbus Helicopters SA 330
  • Airbus Helicopters AS 332
  • Airbus Helicopters EC 225
  • Airbus Helicopters SA
  • Airbus Helicopters AS 365
  • Airbus Helicopters EC 155
  • Airbus Helicopters AS 332 L2
  • Airbus Helicopters EC 225 LP
  • Airbus Helicopters AS 365 N3
  • Airbus Helicopters EC175 B

EASA AD 2018-0172

Aug 7, 2018

Main Rotor Blade Attachment Pin — Inspection

EASA Airworthiness Directive 2018-0172 is an airworthiness directive addressing inspection requirements for the main rotor blade attachment pin assemblies on Airbus Helicopters AS 332 L2 and EC 225 LP models. It mandates inspections and measurements of specific part numbers 332A31-2123-00, 332A31-2115-20, and 332A31-3204-20 to detect corrosion and cracking. The directive aims to ensure continued airworthiness and prevent potential failure of these critical components.

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 2018-0106

May 10, 2018

Rotors Flight Control — Collective Controls / Protective Cover — Modification

EASA Airworthiness Directive 2018-0106 is issued for Airbus Helicopters EC 225 LP models to address a safety issue with the protective cover of the "SHEAR" control pushbutton on pilot and copilot collective sticks. The directive mandates modification of the protective cover to an improved design to prevent mechanical deformation that could lead to unintended shearing of the hoist cable. This AD applies to all serial numbers of the EC 225 LP helicopter.

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

EASA AD 2018-0090

Apr 20, 2018

Landing Gear — Emergency Flotation Gear Upper Fitting Attaching Screws — Inspection / Replacement / Modification

EASA Airworthiness Directive 2018-0090 is an official regulatory document addressing the inspection, replacement, and modification of emergency flotation gear upper fitting attaching screws on Airbus Helicopters AS 332 and EC 225 models. It applies to AS 332 C, C1, L, L1, L2, and EC 225 LP helicopters equipped with emergency flotation gear, excluding those with modification 0728456. The directive mandates inspections and corrective actions to ensure the integrity of the flotation gear screws to prevent failure during ditching scenarios.

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

EASA AD 2018-0065

Mar 23, 2018

Superseded by EASA AD 2018-0272

EASA Airworthiness Directive 2018-0065 is an airworthiness directive issued by the European Aviation Safety Agency affecting all Airbus Helicopters SA 330 J models. It mandates repetitive inspections of the main gearbox particle detector to detect and analyze particles, ensuring continued airworthiness and safety. This directive aligns inspection standards with those applied to EC 225 LP and AS 332 L2 helicopters.

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

EASA AD 2018-0066

Mar 23, 2018

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.

Airworthiness DirectiveSuperseded
  • 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 2018-0042

Feb 14, 2018

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.

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 SA 330 J

EASA AD 2017-0191R2

Dec 15, 2017

Superseded by EASA AD 2019-0074

EASA Airworthiness Directive 2017-0191R2 is an updated safety directive addressing Airbus Helicopters EC 225e LP models equipped with main rotor rotating swashplate part numbers 332A31-3074-00 or 332A31-3074-01. The directive mandates inspections and rework of the main rotor rotating swashplate yokes to detect and correct cracks caused by aging, which could lead to structural failure and loss of helicopter control.

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