EASA Regulations & Airworthiness Directives

Browse 252 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 A319Clear filter

EASA AD 2020-0153

Jul 10, 2020

Fuselage — Rear Fuselage Clips, Shear Webs and Angles — Replacement

EASA Airworthiness Directive 2020-0153 is an airworthiness directive addressing the replacement of rear fuselage clips, shear webs, and angles on Airbus A319, A320, and A321 aeroplanes. It applies to specific models except those with Airbus modification 30975 embodied in production. The directive aims to ensure structural integrity by mandating replacement of affected parts identified during fatigue testing.

Airworthiness Directive
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2020-0148

Jul 6, 2020

Fuel — Low Pressure Shut Off Valve — Inspection

EASA Airworthiness Directive 2020-0148 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A319, A320, and A321 aircraft models. It addresses a potential unsafe condition related to fuel leaks from low pressure shut off valves located on engine #1 and engine #2 pylon areas. The directive mandates inspection and corrective actions to prevent possible fuel spillage and fire hazards.

Airworthiness Directive
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2020-0036R1

Jun 24, 2020

Superseded by EASA AD 2022-0085

EASA Airworthiness Directive 2020-0036R1 is an updated regulatory requirement issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aircraft models. It mandates compliance with the Airworthiness Limitations Section (ALS) Part 2, which includes damage tolerant airworthiness limitation items essential for continued airworthiness. This directive ensures operators maintain the structural integrity of these aircraft by following specified maintenance tasks and intervals.

Airworthiness DirectiveSuperseded
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2020-0040R1

Jun 16, 2020

Fuselage — Overwing Emergency Exit Cut-Outs in Section 15 — Modification

EASA Airworthiness Directive 2020-0040R1 is a regulatory update addressing structural cracks found on overwing emergency exit door cut-outs in fuselage section 15 of Airbus A319 and A320 aeroplanes. This directive applies to various A319 and A320 models except those with specific Airbus modifications or service bulletins already embodied. It mandates inspections, repairs, and modifications to ensure continued structural integrity and compliance with extended service goals.

Airworthiness Directive
  • Airbus A319
  • Airbus A320

EASA AD 2020-0135

Jun 15, 2020

Engine — High Pressure Turbine Rotor Stage 2 Disc — Inspection

EASA Airworthiness Directive 2020-0135 is an airworthiness directive addressing the inspection and replacement of high pressure turbine rotor stage 2 discs on CFM International LEAP-1A engines. This directive applies to various LEAP-1A engine models installed on Airbus A319, A320, and A321 aircraft. It mandates inspection and replacement of specific affected turbine discs to ensure continued airworthiness.

Airworthiness Directive
  • CFM International LEAP-1A
  • CFM International LEAP-1C
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2020-0133

Jun 10, 2020

Superseded by EASA AD 2021-0049

EASA Airworthiness Directive 2020-0133 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes. It addresses the issue of air leakage through certain cargo door seals that could reduce the effectiveness of the cargo compartment fire extinguishing system. The directive applies to specific part numbers of forward, aft, and bulk cargo door seals installed on these aircraft models.

Airworthiness DirectiveSuperseded
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2020-0130

Jun 8, 2020

Landing Gear — Main Landing Gear Torque Link Apex Pin — Replacement / Inspection

EASA Airworthiness Directive 2020-0130 is an airworthiness directive addressing the replacement and inspection of the main landing gear torque link Apex pins on Airbus A318, A319, A320, and A321 aeroplanes. The directive targets specific parts identified by part number 201383606 and serial numbers listed in Airbus Alert Operators Transmission A32N018-20 Revision 01. It aims to ensure continued airworthiness by mitigating risks associated with torque link pin failures.

Airworthiness Directive
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2020-0118

May 22, 2020

Superseded by EASA 2022-0096

EASA Airworthiness Directive 2020-0118 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A319, A320, and A321 aeroplanes. It addresses a flight safety issue related to automatic go-around procedures when the autopilot is engaged, which can cause an unexpected pitch-up attitude and autopilot disconnection. The directive applies to various Airbus A320 family models with specific serial numbers.

Airworthiness DirectiveSuperseded
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2020-0103

May 8, 2020

[Correction] Equipment / Furnishings — Emergency Locator Transmitter Protection — Modifications

EASA Airworthiness Directive 2020-0103 is a correction issued by the European Union Aviation Safety Agency concerning Airbus A318, A319, A320, and A321 aeroplanes. It addresses modifications related to the Emergency Locator Transmitter (ELT) protection, specifically targeting ELTs with Part Number 01N65900. The directive mandates modifications to improve ELT battery current injection protection to prevent potential battery fires.

Airworthiness Directive
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2020-0080

Apr 1, 2020

Superseded by EASA AD 2022-0082

EASA Airworthiness Directive 2020-0080 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes. It mandates compliance with updated safe life airworthiness limitations as specified in the Airbus A318/A319/A320/A321 Airworthiness Limitations Section (ALS) Part 1 Revision 07. This directive ensures continued airworthiness by requiring operators to adhere to new or more restrictive maintenance tasks and life limits for components.

Airworthiness DirectiveSuperseded
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2020-0073

Mar 26, 2020

Superseded by EASA AD 2024-0203

EASA Airworthiness Directive 2020-0073 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes. It addresses issues with certain trimmable horizontal stabilizer actuators (THSA) that may have deviations from the Component Maintenance Manual acceptance test procedure. The directive mandates replacement of affected THSA parts to ensure continued safe operation of the aircraft.

Airworthiness DirectiveSuperseded
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2020-0067

Mar 23, 2020

Superseded by EASA AD 2022-0091

EASA Airworthiness Directive 2020-0067 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aircraft models. It mandates compliance with the Airbus Airworthiness Limitations Section Part 3 Revision 07, which includes certification maintenance requirements and updated maintenance tasks for these aircraft. This directive ensures continued airworthiness by enforcing updated maintenance limits and tasks.

Airworthiness DirectiveSuperseded
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2020-0052

Mar 10, 2020

Fuselage — Satellite Communications Antenna Doubler — Inspection / Replacement

EASA Airworthiness Directive 2020-0052 is an airworthiness directive affecting Airbus A319 aeroplanes, specifically models A319-111 through A319-133 with certain exceptions. It mandates inspection and replacement of the satellite communications (SATCOM) antenna doubler on the fuselage to address potential structural integrity issues. The directive applies to aircraft without specific Airbus modifications or service bulletin embodiments that mitigate the issue.

Airworthiness Directive
  • Airbus A319

EASA AD 2020-0044

Mar 3, 2020

Superseded by EASA AD 2024-0002

EASA Airworthiness Directive 2020-0044 is an airworthiness directive issued by the European Union Aviation Safety Agency addressing certain CFM International CFM56-5B, CFM56-5C, and CFM56-7B engine models installed on Airbus A318, A319, A320, A321, A340, and Boeing 737 series aircraft. The directive mandates inspection and potential replacement of high-pressure turbine inner stationary seals to prevent damage caused by honeycomb separation. This directive aims to ensure continued airworthiness and safety of affected engines and aircraft.

Airworthiness DirectiveSuperseded
  • CFM International CFM56-5B
  • CFM International CFM56-5C
  • CFM International CFM56-7B
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321
  • Airbus A340
  • Boeing 737

EASA AD 2020-0037

Feb 28, 2020

[Correction] Fuselage — Frame Foot Coupling at Frame 43 — Inspection / Repair

EASA Airworthiness Directive 2020-0037 is a corrective directive addressing inspection and repair requirements for the fuselage frame foot coupling at frame 43 on Airbus A318, A319, A320, and A321 aircraft. It applies to all serial numbers except those with Airbus modifications 153126 or 153742 incorporated during production. The directive mandates a one-time special detailed inspection and subsequent repair or modification to ensure structural integrity.

Airworthiness Directive
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2020-0034

Feb 25, 2020

Superseded by EASA AD 2022-0102

EASA Airworthiness Directive 2020-0034 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes. It mandates compliance with the Airbus Airworthiness Limitations Section (ALS) Part 4 Revision 07, which includes system equipment maintenance requirements and life limits for components. This directive ensures continued airworthiness by requiring operators to follow updated maintenance tasks and replacement intervals.

Airworthiness DirectiveSuperseded
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2020-0030

Feb 18, 2020

Fuselage — External Fuselage Skin — Inspection / Repair

EASA Airworthiness Directive 2020-0030 is an airworthiness directive issued by the European Union Aviation Safety Agency that applies to Airbus A318, A319, and A320 aeroplanes. It addresses inspection and repair requirements for the external fuselage skin panels at frame 34 underneath the fairing structure between stringer 43 left-hand and right-hand sides. The directive mandates repetitive detailed inspections and corrective actions to ensure structural integrity of the affected fuselage area.

Airworthiness Directive
  • Airbus A318
  • Airbus A319
  • Airbus A320

EASA AD 2020-0019

Feb 5, 2020

Fuselage — Lateral Window Frame Upper Fastener Holes — Inspection

EASA Airworthiness Directive 2020-0019 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes. It mandates inspections of the lateral window frame upper fastener holes to detect cracks that could compromise structural integrity. The directive applies to specific serial numbers except those with certain Airbus modifications or service bulletins already embodied.

Airworthiness Directive
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2020-0007

Jan 15, 2020

Engine — Rotating Air High Pressure Turbine Front Seal — Replacement

EASA Airworthiness Directive 2020-0007 is a regulatory document addressing the replacement of rotating air high pressure turbine (HPT) front seals on CFM International CFM56-5B, CFM56-5C, and CFM56-7B engines. These engines are installed on various Airbus models including A318, A319, A320, A321, A340, and Boeing 737-600, 737-700, 737-800, and 737-900 aircraft. The directive mandates inspections and replacement of specific affected HPT front seals to prevent potential uncontained engine failures.

Airworthiness Directive
  • CFM International CFM56-5B
  • CFM International CFM56-5C
  • CFM International CFM56-7B
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321
  • Airbus A340
  • Boeing 737-600
  • Boeing 737-700
  • Boeing 737-800
  • Boeing 737-900

EASA AD 2019-0316

Dec 23, 2019

Superseded by EASA AD 2020-0236

EASA Airworthiness Directive 2019-0316 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes. It addresses a safety issue related to emergency escape slides and rafts, specifically the inflation reservoirs which may have defective rupture disk assemblies. The directive mandates repetitive pressure checks of these inflation reservoirs to ensure proper functionality.

Airworthiness Directive
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321