EASA Regulations & Airworthiness Directives

Browse 5,166 EASA regulations with AI-powered summaries.

Aircraft:AllAirbus A320286Airbus A321285Airbus A319253Airbus A350224Airbus A330221Airbus A318189Airbus A380182Boeing 737175Airbus A340141Airbus A350-941134Airbus BD-500 (A220 Series)123Airbus Helicopters AS 332119Airbus Helicopters EC 225116Airbus Helicopters SA 330116Boeing 787116Show all...

EASA AD 2019-0004

Jan 17, 2019

[Correction] THALES AVS FRANCE SAS - Global Navigation Satellite System — Operational Limitations

EASA Airworthiness Directive 2019-0004 is a correction issued by the European Union Aviation Safety Agency concerning operational limitations of the Thales AVS France SAS Topstar 200 LPV GPS/SBAS receivers. This directive applies to certain ATR 42-500 and ATR 72-212A aeroplanes, as well as Sikorsky S-76D helicopters equipped with these receivers. It addresses potential erroneous GPS position outputs that could affect navigation safety during LPV and RNP-AR operations.

Airworthiness Directive
  • ATR 42-500
  • ATR 72-212A
  • Sikorsky S-76D

EASA AD 2018-0084R2

Jan 17, 2019

Engine – Intermediate Pressure Compressor Blades / Shaft – Inspection

EASA Airworthiness Directive 2018-0084R2 is a regulatory update addressing safety concerns for Rolls-Royce Trent 1000 series engines installed on Boeing 787 aircraft. It mandates repetitive inspections of intermediate pressure compressor (IPC) Rotor 1 and Rotor 2 blades and shaft to detect cracks that could lead to in-flight blade release. The directive excludes engines modified with RR mod 72-J941 and introduces a modification service bulletin as terminating action for inspections.

Airworthiness DirectiveSuperseded
  • Rolls-Royce Deutschland Ltd & Co Kg TRENT 1000
  • Boeing 787

EASA AD 2019-0006

Jan 17, 2019

Stabilizers — Composite Vertical Tailplane Attachment Fittings — Inspection

EASA Airworthiness Directive 2019-0006 is an airworthiness directive addressing inspection requirements for composite vertical tailplane attachment fittings on Airbus A310, A300-600, and A300-600ST aircraft. It mandates review and inspection of affected parts to detect potential delamination that could compromise the vertical tailplane attachment fittings. The directive applies to all certified models with Airbus modification 04886 embodied in production.

Airworthiness Directive
  • Airbus A300-600
  • Airbus A300-600ST (Beluga)
  • Airbus A310
  • Airbus A300-600ST

EASA SIB CASA-2018-11

Jan 16, 2019

Bell Helicopter 206 Helicopters - Unporting of Fuel Boost Pump

The Transport Canada Civil Aviation Safety Alert CASA 2018-11 addresses the risk of engine flameout due to unporting of fuel boost pumps in Bell Helicopter 206 series models, including 206A, 206B (including 206B3 commercial designation), and 206L variants. This alert highlights the danger during low fuel levels combined with uncoordinated flight maneuvers, which can cause fuel starvation and sudden loss of engine power. The document raises awareness for owners, operators, and maintainers of these helicopters to mitigate this safety risk.

Safety Information Bulletin

EASA AD US-2018-25-11

Jan 16, 2019

Engine Exhaust - Electronic Engine Control Wiring - Inspection

Federal Register Volume 83, Number 240 (AD 2018-25-11) is a final rule airworthiness directive issued by the FAA for certain Boeing 777-200 and -300 series airplanes equipped with Rolls-Royce RB211-Trent 800 engines. It addresses inadequate clearance between thermal protection system insulation blankets and electronic engine control wiring, which has caused wire damage. The directive mandates repetitive inspections and corrective actions to ensure continued airworthiness.

Airworthiness Directive
  • Boeing 777200300

EASA AD 2018-0276R1

Jan 15, 2019

[Correction] Fuselage — Structural Parts / Joints — Modification / Reinforcement

EASA Airworthiness Directive 2018-0276R1 is a corrective revision addressing structural modifications and reinforcements for Airbus A330 series aeroplanes. It applies to multiple A330 variants including A330-200, A330-200F, and A330-300 models, focusing on fuselage structural parts and joints to prevent widespread fatigue damage. The directive mandates compliance with specific Airbus Service Bulletins to ensure continued airworthiness.

Airworthiness Directive
  • Airbus A330200200F300

EASA AD 2019-0005

Jan 14, 2019

Equipment / Furnishings — Cabin Attendant Seat — Modification

EASA Airworthiness Directive 2019-0005 is an airworthiness directive issued by the European Union Aviation Safety Agency concerning the modification of cabin attendant seats on Airbus A320 and A321 aeroplanes. It specifically applies to certain serial numbers of the A320-214, A320-271N, A321-211, and A321-231 models. The directive addresses a safety issue related to the deformation of the seat backrest which could impede evacuation.

Airworthiness Directive
  • Airbus A320
  • Airbus A321

EASA SIB NM-18-33

Jan 11, 2019

Boeing 717, 737, 747, 757, 767, 787, MD-11 and MD-90 Aeroplanes - Fuel Control Switch Locking

The FAA Special Airworthiness Information Bulletin SAIB: NM-18-33 addresses the potential disengagement of the fuel control switch locking feature on various Boeing aeroplanes including models 717-200, 737 series, 747 series, 757 series, 767 series, 787 series, MD-11, and MD-90-30. The bulletin informs operators about the risk of inadvertent fuel control switch operation due to the locking feature being disengaged, which could lead to unintended engine shutdowns. This information bulletin is advisory and does not mandate regulatory action.

Safety Information Bulletin

EASA AD US-2018-23-12

Jan 11, 2019

[Correction] ZODIAC AERO EVACUATION SYSTEMS - Fusible Plugs - Replacement

Correction to FAA Airworthiness Directive 2018-23-12 concerning Zodiac Aero Evacuation Systems fusible plugs installed on emergency evacuation equipment for various transport category airplanes including models from Airbus, Boeing, BAE Systems, and Fokker. The correction updates the previously published email address for requesting service information related to the inspection and replacement of affected fusible plugs. The directive addresses fusible plugs that may activate below their rated temperature, potentially compromising evacuation system functionality.

Airworthiness Directive
  • Airbus
  • Boeing
  • BAE Systems
  • Fokker

EASA AD US-2018-26-06

Jan 11, 2019

Doors - Main Landing Gear Center Door Assemblies - Inspection

Federal Aviation Administration Airworthiness Directive 2018-26-06 is a final rule addressing all Boeing 737-600, -700, -700C, -800, -900, and -900ER series airplanes. It mandates inspections of the main landing gear center door assemblies due to reports of loose, worn, or missing attachment bolts. The directive aims to ensure the structural integrity of the main landing gear doors to prevent potential damage and loss of airplane control.

Airworthiness Directive
  • Boeing 737600700700C800900900ER

EASA AD US-2018-26-05

Jan 11, 2019

Fuel - Motor-Operated Valve Actuators / Maintenance or Inspection Program - Inspection / Replacement / Revision

The Federal Aviation Administration's Airworthiness Directive 2018-26-05 addresses certain Boeing Model 777 airplanes. It requires inspection and possible replacement of motor-operated valve (MOV) actuators at the engine fuel shutoff spar valve positions and mandates revising the maintenance or inspection program to include a new airworthiness limitation. This directive aims to prevent latent failures of engine fuel shutoff spar valves that could compromise fuel flow termination during emergencies.

Airworthiness Directive
  • Boeing 777

EASA AD 2019-0002

Jan 11, 2019

Nacelles / Pylons – Inboard and Outboard Pylon Drain System – Inspection

EASA Airworthiness Directive 2019-0002 is an airworthiness directive issued by the European Aviation Safety Agency affecting Airbus A380-841 and A380-842 aeroplanes, excluding those with certain production modifications (77710, 77711, 77712, and 77713). The directive mandates inspection of the inboard and outboard pylon drain systems to detect potential clogging and damage that could lead to hydraulic fluid leakage and fire risk. It addresses a safety concern related to flame and smoke detected near engine nozzle exhausts due to damaged sealant and clogged drain lines.

Airworthiness DirectiveSuperseded
  • Airbus A380

EASA AD 2019-0003

Jan 11, 2019

Rotor Drive – Main Gearbox Top Sensor – Inspection

EASA Airworthiness Directive 2019-0003 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus Helicopters EC 175 B models equipped with main gearboxes manufactured before 1 December 2018. The directive mandates inspections of the main gearbox top sensor to detect potential foreign object debris that could cause loss of lubrication and mast bearing seizure. This directive aims to ensure continued safe operation of the affected helicopters by requiring repetitive inspections and corrective actions as necessary.

Airworthiness DirectiveSuperseded
  • Airbus Helicopters EC175
  • Airbus Helicopters EC 175 B

EASA AD US-2018-22-07

Jan 11, 2019

Superseded by FAA AD 2019-15-06

FAA Airworthiness Directive 2018-22-07 is a final rule applicable to all Engine Alliance GP7270, GP7272, and GP7277 model turbofan engines. It mandates inspections of the stage 6 seal ring installation and the high-pressure compressor (HPC) stages 2-5 spool for cracks to address an unsafe condition caused by axial cracks in the HPC spool spacer arm. The directive aims to prevent uncontained failures that could damage the engine and aircraft.

Airworthiness Directive
  • Engine Alliance GP7200

EASA AD 2018-0265R1

Jan 10, 2019

[Correction] Engine — Exhaust Valve — Replacement

EASA Airworthiness Directive 2018-0265R1 is a correction to the original directive addressing the replacement of affected exhaust valves on BRP-Rotax 914 and 915 series engines. This directive applies to Rotax 915 iSc3 A, 915 iSc3 B, and Rotax 914 F2, F3, and F4 engines installed on various light aircraft models. The directive mandates replacement of exhaust valves with specific part and lot numbers to prevent potential in-flight engine shutdowns.

Airworthiness Directive
  • Brp-Rotax Gmbh & Co Kg 914 F
  • Brp-Rotax Gmbh & Co Kg 915

EASA AD 2019-0001

Jan 10, 2019

Doors – Sliding Door Opening Mechanism – Inspection

EASA Airworthiness Directive 2019-0001 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all Airbus Helicopters EC 130 B4 models. It addresses the risk of in-flight detachment of the left-hand cabin sliding door due to degradation of the door locking mechanism. The directive mandates inspections and corrective actions to ensure the sliding door locking mechanism operates within safe parameters.

Airworthiness DirectiveSuperseded
  • Airbus Helicopters AS 350
  • Airbus Helicopters EC 130
  • Airbus Helicopters EC 130 B4

EASA AD CF-2018-36

Jan 10, 2019

Navigation — Flight Instruments — Unreliable Air Data in the Cockpit

The Canadian Airworthiness Directive CF-2018-36 titled 'Navigation — Flight Instruments — Unreliable Air Data in the Cockpit' addresses issues related to unreliable anemobarometric data in the cockpit for Bombardier Inc. aircraft models CL-600-1A11 (variant 600), CL-600-2A12 (variant 601), and CL-600-2B16 (variant 601-3A/3R) within specified serial number ranges. This directive mandates updates to the aircraft flight manuals to include emergency procedures for unreliable airspeed indications caused by high-altitude icing conditions. The directive aims to enhance flight safety by providing crews with procedures to stabilize airspeed and attitude during such events.

Airworthiness Directive
  • Bombardier CL-600 (Challenger)
  • Bombardier CL-600-1A11
  • Bombardier CL-600-2A12
  • Bombardier CL-600-2B16

EASA AD CF-2019-01

Jan 10, 2019

Standard Practices — Helicopter External Transport System (HETS—¢) - Unapproved Parts, Inadequate Service Life Limits and Maintenance Requirements

Airworthiness Directive CF-2019-01 is a Canadian regulatory document addressing the Helicopter External Transport System (HETS™) certified under Transport Canada Supplemental Type Certificate SH98-35 installed on specific helicopter models including Bell 206B, 206L series, 407, Airbus Helicopters AS350 and AS355 series, and MD Helicopter 369 and 500N series. The directive focuses on issues related to unapproved parts, inadequate service life limits, and maintenance requirements for HETS™ components. It mandates inspections, component removals, and flight manual amendments to ensure continued airworthiness and safety.

Airworthiness Directive
  • Airbus Helicopters AS 350
  • Airbus Helicopters EC 130
  • Airbus Helicopters AS 355
  • Bell 206
  • Bell 407
  • Md Helicopters Inc (Mdhi) 369
  • Md Helicopters Inc (Mdhi) 500N
  • Bell 206B
  • Bell 206L
  • Airbus Helicopters AS350
  • Airbus Helicopters AS355
  • MD Helicopter 369
  • MD Helicopter 500N

EASA AD CF-2019-02

Jan 10, 2019

Time Limits / Maintenance Checks — Airworthiness Limitations - Implementation

Airworthiness Directive CF-2019-02 is issued by Transport Canada and applies to Viking Air Ltd. DHC-6 series 1, 100, 110, 200, 210, 300, 310, 320, and 400 aeroplanes. It mandates compliance with the airworthiness limitations specified in Viking Air Ltd.'s Airframe Airworthiness Limitations Manual, Product Support Manual 1-6-11 Revision 9, which includes updated maintenance tasks and life limits for various airframe components.

Airworthiness Directive
  • Viking Air DHC-6 (Twin Otter)
  • Viking Air DHC-6 Series 1
  • Viking Air DHC-6 Series 100
  • Viking Air DHC-6 Series 110
  • Viking Air DHC-6 Series 200
  • Viking Air DHC-6 Series 210
  • Viking Air DHC-6 Series 300
  • Viking Air DHC-6 Series 310
  • Viking Air DHC-6 Series 320
  • Viking Air DHC-6 Series 400