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EASA Regulations & Airworthiness Directives

Browse 4995 EASA regulations with AI-powered summaries.

Aircraft:AllAirbus A320280Airbus A321276Airbus A319246Airbus A350214Airbus A330210All194Airbus A318185Airbus A380171Boeing 737170Airbus A340140Airbus A350-941125Airbus BD-500 (A220 Series)116Airbus Helicopters AS 332116Airbus Helicopters EC 225113Airbus Helicopters SA 330113Show all...

EASA AD 2019-0291R1

SUPERSEDED BY EASA AD 2020-0283

EASA Airworthiness Directive 2019-0291R1 is an updated safety directive addressing fuel pump erosion issues on Airbus A330 and A340 aeroplanes, including the A330-941 variant. It mandates inspections and potential replacement of specific fuel pumps with part numbers 568-1-28300-101, 568-1-28300-103, and 568-1-28300-200 installed at designated locations to prevent fuel tank ignition risks. This directive applies to all manufacturer serial numbers of the affected models.

Mar 4, 2020
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A330Airbus A340

EASA AD 2020-0047

SUPERSEDED BY EASA AD 2021-0081

EASA Airworthiness Directive 2020-0047 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all serial numbers of Sukhoi Civil Aircraft JSC RRJ-95B aeroplanes. It mandates compliance with updated airworthiness limitations and maintenance tasks as specified in the Sukhoi RRJ-95B Maintenance Manual, Chapter 04, Issue 01, Revision 03. This directive ensures continued airworthiness by enforcing life limits and maintenance intervals for critical components.

Mar 4, 2020
Airworthiness DirectiveMaintenanceSafety MgmtIrkut Corporation Jsc RRJ-95Sukhoi RRJ-95B

EASA AD 2020-0044

SUPERSEDED BY EASA AD 2024-0002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.

Mar 3, 2020
Airworthiness DirectiveMaintenanceSafety MgmtCFM International CFM56-5BCFM International CFM56-5CCFM International CFM56-7BAirbus A318Airbus A319Airbus A320Airbus A321Airbus A340Boeing 737

EASA SIB CASA-2020-01

Bombardier CL-600-2B19 Aeroplanes - Inspection of the Translating Cowl Doors

The document titled Bombardier CL-600-2B19 Aeroplanes - Inspection of the Translating Cowl Doors is a Civil Aviation Safety Alert issued by Transport Canada addressing safety concerns for Bombardier CL-600-2B19 (CRJ 100 & 440 series) aircraft. It highlights issues with the translating cowl doors becoming dislodged during flight, causing damage to the airplane fuselage. The alert emphasizes the importance of following the latest Aircraft Maintenance Manual inspection procedures for these components.

Mar 2, 2020
Safety Information BulletinMaintenanceSafety Mgmt

EASA AD 2020-0043

Main Rotor Drive — Main Gearbox — Replacement

EASA Airworthiness Directive 2020-0043 is an airworthiness directive issued by the European Union Aviation Safety Agency concerning Airbus Helicopters EC 155 B and EC 155 B1 models. It addresses the replacement of main gearboxes (MGB) with specific part numbers and serial numbers due to potential manufacturing inspection errors. The directive mandates actions to ensure continued safe operation of affected helicopters.

Mar 2, 2020
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SAAirbus Helicopters AS 365Airbus Helicopters EC 155Airbus Helicopters EC 155 BAirbus Helicopters EC 155 B1

EASA AD 2020-0037

[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.

Feb 28, 2020
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD US-2020-01-18

[Correction] Time Limits / Maintenance Checks - Airworthiness Limitations Instructions - Principal Structural Elements - Inspections / Maintenance or Inspection Program Revision

Correction to Airworthiness Directive 2020-01-18 issued by the Federal Aviation Administration (FAA) affecting all Boeing Company Model 757 airplanes. This correction clarifies the proper reference for revising the maintenance or inspection program related to airworthiness limitations and principal structural element inspections. The directive mandates incorporation of updated structural inspection requirements to ensure continued airworthiness.

Feb 28, 2020
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 757

EASA AD 2020-0042

Main Rotor Drive — Main Gearbox Top Sensor / Main Rotor Mast Lubrication System — Inspection

EASA Airworthiness Directive 2020-0042 is an airworthiness directive affecting all Airbus Helicopters EC 175 B models. It mandates inspections of the main gearbox top sensor and the main rotor mast lubrication system to detect foreign object debris that could cause mast bearing seizure and potential loss of helicopter control. The directive includes specific inspection procedures and corrective actions to ensure continued airworthiness.

Feb 28, 2020
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters EC175Airbus Helicopters EC 175 B

EASA AD 2020-0041

SUPERSEDED BY EASA AD 2020-0208

EASA Airworthiness Directive 2020-0041 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Rolls-Royce RB211 Trent 970-84, Trent 972-84, and Trent 972E-84 engines. It addresses inspection requirements for the intermediate pressure compressor rotor shaft, part number FW20677, due to detected cracks that could lead to rotor shaft failure and potential damage to the aircraft. The directive mandates specific inspections and corrective actions to ensure continued airworthiness.

Feb 28, 2020
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg RB211 TRENT 900

EASA AD US-2020-03-22

Wings - Frame Tie Rod Assemblies & Stub Beam Upper Chords - Inspection

The Federal Aviation Administration's Airworthiness Directive 2020-03-22 addresses certain Boeing Model 787-8 airplanes. It mandates repetitive inspections of the wing's left- and right-side frame tie rod assemblies and stub beam upper chords to detect fatigue cracking. The directive aims to maintain structural integrity and prevent possible airplane decompression.

Feb 28, 2020
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 787Boeing 787-8

EASA AD 2020-0039

Fire Protection — Hand-held Fire Extinguishers — Replacement

EASA Airworthiness Directive 2020-0039 is an airworthiness directive addressing fire protection on various helicopter models including Bell 222, 230, 430, 204, 205, 212, 214, 412, Erickson S-64F, Kamov Ka-32A11BC, and Sikorsky S-58, S-61, S-76, and S-92 helicopters. The directive focuses on the replacement of certain Halon-free hand-held fire extinguishers manufactured by umlaut engineering GmbH that have a manufacturing defect. It mandates the removal and replacement of affected fire extinguishers to ensure continued airworthiness and safety.

Feb 27, 2020
Airworthiness DirectiveMaintenanceSafety MgmtBell 222Bell 230Bell 430Bell Textron Inc. (Bti) 204BBell Textron Inc. (Bti) 205Bell Textron Inc. (Bti) 212Bell Textron Inc. (Bti) 214STBell Textron Inc. (Bti) 412Centerpointe Aerospace, Inc S-58Erickson Air-Crane S-64Kamov KA32Mcdermott 214 Holdings, 214Sikorsky S-61Sikorsky S-76Sikorsky S-92Bell 204Bell 205Bell 212Bell 214Bell 412Erickson S-64FKamov Ka-32A11BCSikorsky S-58

EASA AD 2020-0038

Main Rotor — Vibration Absorber Fairing — Installation

EASA Airworthiness Directive 2020-0038 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all PZL W-3A and PZL W-3AS helicopters. It addresses the installation of the main rotor vibration absorber fairing, specifically focusing on the affected fairing part number 30.23.015.00.03 and associated hardware. The directive mandates compliance with updated installation instructions to ensure proper securing of the fairing to the vibration absorber.

Feb 27, 2020
Airworthiness DirectiveMaintenanceSafety MgmtWsk Pzl-Swidnik PZL W-3APZL W-3APZL W-3AS

EASA AD 2020-0035

Engine Fuel & Control — Engine Electronic Controller Software — Update

EASA Airworthiness Directive 2020-0035 is an official directive addressing the Rolls-Royce Trent XWB-97 engines, commonly installed on Airbus A350 aircraft. The directive mandates an update to the engine electronic controller software to correct issues related to air pressure sensing that could affect thrust control. This update ensures continued safe operation of affected engines.

Feb 26, 2020
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg TRENT XWBAirbus A350

EASA AD US-2020-04-01

Engine - LP10 Oil Supply Tube & Fuel Oil Cooler - Inspection

FAA Airworthiness Directive 2020-04-01 is a final rule addressing Pratt & Whitney PW1519G, PW1521G, PW1521GA, PW1524G, PW1525G, PW1521G-3, PW1524G-3, PW1525G-3, PW1919G, PW1921G, PW1922G, PW1923G, and PW1923G-A model turbofan engines. It mandates inspections and potential replacement of the LP10 oil supply tube and the fuel oil cooler (FOC) due to reports of in-flight shutdowns caused by oil leaks at their connection. This directive aims to prevent engine fires and damage to aircraft.

Feb 25, 2020
Airworthiness DirectiveMaintenanceSafety MgmtPratt & Whitney PW1500GPratt & Whitney PW1900G

EASA AD US-2020-03-10

Fuselage - Fairing Panel 194E, Wheel Well Panel 193D & Support Structure - Inspection

The Federal Aviation Administration's Airworthiness Directive 2020-03-10 addresses The Boeing Company Model 737 series airplanes, excluding the 737-100, -200, -200C, -300, -400, and -500 series. This directive mandates inspections and corrective actions for the lower aft wing-to-body fairing panel 194E, wheel well panel 193D, and their support structures due to reported in-flight separation caused by worn or damaged nutplates.

Feb 25, 2020
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 737

EASA AD 2020-0034

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.

Feb 25, 2020
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD US-2020-02-23

Equipment / Furnishings - Emergency Float Kit Pull Cables - Inspection

Federal Aviation Administration Airworthiness Directive 2020-02-23 is a final rule addressing certain Airbus Helicopters models AS350B series and AS355 series equipped with emergency float kits. It mandates repetitive inspections of the pull cable installation on the emergency float kits to ensure proper activation of the float inflation system. This directive aims to prevent asymmetric float inflation or failure to deploy, which could lead to capsizing during water landings.

Feb 21, 2020
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters AS 350Airbus Helicopters EC 130Airbus Helicopters AS 355Airbus Helicopters AS350BAirbus Helicopters AS355

EASA AD 2020-0027R1

Flight Controls — Aileron, Elevator and Rudder Electro-Hydrostatic Actuators — Inspection / Replacement

EASA Airworthiness Directive 2020-0027R1 is an updated regulatory requirement addressing inspection and replacement of Electro-Hydrostatic Actuators (EHAs) for the aileron, elevator, and rudder flight controls on Airbus A350-941 and A350-1041 aircraft. The directive mandates insulation resistance checks and corrective actions for affected EHAs to ensure continued safe operation of these flight control components.

Feb 21, 2020
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A350Airbus A350-941Airbus A350-1041

EASA AD 2005-0035-CN

CANCELLED: Landing Gear - Main Undercarriage Structure - Inspection

EASA Airworthiness Directive 2005-0035-CN is a cancellation notice for the previous directive concerning the inspection of the main landing gear cylinder torque link attachment lugs on Piper Aircraft PA-28 and PA-32 aeroplanes. The affected aircraft include various PA-28 models and the PA-32-260, with specific serial numbers detailed in the directive. This cancellation reflects updated safety assessments and improved inspection procedures.

Feb 20, 2020
Airworthiness DirectiveMaintenanceSafety MgmtPiper Aircraft PA-28 (Archer)Piper Aircraft PA-28 (Cadet)Piper Aircraft PA-28 (Cherokee)Piper Aircraft PA-28 (Warrior)Piper Aircraft PA-32 (Cherokee Six)Piper PA-28Piper PA-32

EASA AD 2020-FATA-01020A-03

NOT ADOPTED - EASA DECISION ATTACHED

The NOT ADOPTED - EASA DECISION ATTACHED is a Russian Federation Federal Air Transport Agency Airworthiness Directive issued on 2020-02-28 concerning the RRJ-95 aircraft. It addresses mandatory corrective actions related to the emergency exit door and emergency escape slide system, focusing on additional operational tests and inspections to ensure proper functionality and airworthiness support.

Feb 20, 2020
Airworthiness DirectiveMaintenanceSafety MgmtIrkut Corporation Jsc RRJ-95RRJ-95