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EASA Regulations & Airworthiness Directives

Browse 4771 EASA regulations with AI-powered summaries.

Aircraft:AllAirbus A320262Airbus A321257Airbus A319229Airbus A350206Airbus A330197All177Airbus A318172Boeing 737164Airbus A380162Airbus A340136Airbus A350-941119Airbus Helicopters AS 332110Airbus Helicopters EC 225107Airbus Helicopters SA 330107Boeing 787106Show all...

EASA AD 2019-0220R1

SUPERSEDED BY EASA AD 2021-0226

EASA Airworthiness Directive 2019-0220R1 is an amendment addressing structural integrity issues on Airbus A380-841, A380-842, and A380-861 aeroplanes. It mandates modification of the fuselage rear cone frame feet 102 and 103 between stringers 19 and 20 on both left and right sides to reinforce the skin-to-frame attachment. This directive applies to all serial numbers except those with Airbus modifications 77936 or 77140 incorporated during production.

Dec 17, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380

EASA AD US-2019-22-01

Wings - Side of Body Rib - Inspection

FAA Airworthiness Directive 2019-22-01 is a final rule addressing certain Boeing 787-8 airplanes. It mandates repetitive inspections of the side of body (SOB) rib webs at wing spar terminal fitting fastener locations to detect fatigue cracking. This directive aims to maintain structural integrity by preventing fatigue-related failures in primary wing structures.

Dec 17, 2019
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 787Boeing 787-8

EASA AD 2019-0303

Landing Gear — Main Landing Gear — Inspection / Replacement

EASA Airworthiness Directive 2019-0303 is an airworthiness directive issued for Airbus Helicopters EC 175 B models. It addresses inspection and replacement requirements for specific left-hand and right-hand main landing gear shock absorbers identified by certain part and serial numbers. The directive aims to ensure continued airworthiness by mandating removal and replacement of affected parts to prevent landing gear failure.

Dec 16, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters EC175Airbus Helicopters EC 175 B

EASA AD US-2019-25-01

NOT ADOPTED - EASA DECISION ATTACHED

The document titled 'NOT ADOPTED - EASA DECISION ATTACHED' is a Federal Aviation Administration (FAA) Airworthiness Directive (AD 2019-25-01) addressing certain International Aero Engines, LLC (IAE LLC) turbofan engines including models PW1122G-JM, PW1124G-JM, PW1124G1-JM, PW1127G1-JM, PW1127GA-JM, PW1127G-JM, PW1129G-JM, PW1130G-JM, PW1133GA-JM, and PW1133G-JM. This AD mandates the replacement of specific low-pressure turbine (LPT) 3rd-stage blades due to multiple reported failures that reduce engine thrust and pose safety risks. The directive aims to mitigate the unsafe condition caused by impact damage to these blades.

Dec 16, 2019
Airworthiness DirectiveMaintenanceSafety MgmtInternational Aero Engines PW1100International Aero Engines PW1400

EASA AD US-2019-22-05

SUPERSEDED BY FAA AD 2022-09-14

Airworthiness Directive 2019-22-05 is a final rule issued by the Federal Aviation Administration (FAA) that supersedes AD 2017-23-06. It applies to General Electric Company CF34-8C series turbofan engines, including models CF34-8C1, CF34-8C5, CF34-8C5A1, CF34-8C5B1, CF34-8C5A2, and CF34-8C5A3. The directive addresses safety concerns related to the operability bleed valve (OBV) to prevent engine fires and potential damage to aircraft.

Dec 16, 2019
Airworthiness DirectiveMaintenanceSafety MgmtGeneral Electric CF34-8

EASA AD US-2019-23-06

SUPERSEDED BY FAA AD 2022-15-09

FAA Airworthiness Directive 2019-23-06 is a final rule addressing certain Boeing 757-200, -200CB, and -300 series airplanes. It mandates inspections for cracks initiating in the fuselage frame web at body station 1640, including visual and high frequency eddy current inspections, with applicable corrective actions. This directive aims to maintain structural integrity and safety of the affected aircraft.

Dec 16, 2019
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 757Boeing 757-200Boeing 757-200CBBoeing 757-300

EASA AD US-2019-22-02

SUPERSEDED BY FAA AD 2025-01-08

FAA Airworthiness Directive 2019-22-02 is a final rule addressing uncommanded fore and aft movement of the Captain's and First Officer's seats on all Boeing 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, 747-8F, and 747-8 series airplanes. The directive mandates repetitive inspections and checks of the horizontal movement system and actuators, detailed inspections for certain airplanes, and applicable corrective actions. It also provides an optional terminating action for certain seat models to resolve the unsafe condition.

Dec 16, 2019
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 747Boeing 747-200BBoeing 747-200CBoeing 747-200FBoeing 747-300Boeing 747-400Boeing 747-400DBoeing 747-400FBoeing 747-8FBoeing 747-8

EASA AD BR-2019-12-01

SUPERSEDED BY ANAC BRAZIL AD 2021-02-01

The Brazilian Emergency Airworthiness Directive EAD No. 2019-12-01 issued by ANAC applies to all Embraer S.A. ERJ 190-300 and ERJ 190-400 aircraft of all serial numbers. It addresses an issue where the smoke detection system in the forward and aft electronic bays may falsely indicate smoke presence during a complete loss of the electrical DC essential bus 2, leading to potentially unsafe electrical shutdown procedures. This directive mandates a revision of the Airplane Flight Manual (AFM) procedures related to electronic bay smoke warnings to ensure safe aircraft operation.

Dec 13, 2019
Airworthiness DirectiveFlight OpsSafety MgmtEmbraer ERJ 190Embraer ERJ 190-300Embraer ERJ 190-400

EASA AD 2019-0302

SUPERSEDED BY EASA AD 2023-0013

EASA Airworthiness Directive 2019-0302 is an airworthiness directive issued for Diamond Aircraft Industries GmbH DA 42 series aeroplanes, including DA 42, DA 42 M, DA 42 NG, and DA 42 M-NG models. The directive addresses the inspection and maintenance of the rudder T-yoke axle self-locking nut to ensure proper installation and prevent potential rudder control issues. It applies to all manufacturer serial numbers of these aircraft.

Dec 13, 2019
Airworthiness DirectiveMaintenanceSafety MgmtDiamond Aircraft Industries DA 42Diamond Aircraft Industries GmbH DA 42Diamond Aircraft Industries GmbH DA 42 MDiamond Aircraft Industries GmbH DA 42 NGDiamond Aircraft Industries GmbH DA 42 M-NG

EASA AD US-2019-20-08

Time Limits / Maintenance Checks - Airworthiness Limitations Section - Amendment

The document titled "Time Limits / Maintenance Checks - Airworthiness Limitations Section - Amendment" is a final rule airworthiness directive issued by the FAA for Gulfstream Aerospace Corporation Model G-IV and Model GIV-X airplanes. It mandates revisions to the airworthiness limitations section of the aircraft maintenance manual to incorporate updated inspections and life limits addressing fatigue cracking of principal structural elements. This directive affects specific serial numbers of the G-IV and GIV-X series airplanes.

Dec 13, 2019
Airworthiness DirectiveMaintenanceSafety MgmtGulfstream Aerospace Corporation GIVGulfstream G-IVGulfstream GIV-X

EASA SIB CE-19-21

Air Tractor, Inc., Models AT-602, AT-802, and AT-802A Airplanes - Flap Motor Mounting Studs

The FAA Special Airworthiness Information Bulletin SAIB: CE-19-21 addresses an airworthiness concern for Air Tractor, Inc. Models AT-602, AT-802, and AT-802A airplanes related to flap motor mounting studs. The bulletin excludes AT-802/AT-802A models equipped with part number 71112-1 flap actuators. It informs owners and operators about inspection and replacement procedures for certain flap motor mounting studs to prevent potential loss of flap control.

Dec 12, 2019
Safety Information BulletinMaintenanceSafety Mgmt

EASA AD 2019-0301

Flight Controls — Aileron and Elevator Electro-Hydrostatic Actuators — Modification Aircraft Flight Manual — Amendment

EASA Airworthiness Directive 2019-0301 is an amendment addressing flight control issues on Airbus A350-941 and A350-1041 aeroplanes. It focuses on the modification of electro-hydrostatic actuators (EHA) for inboard ailerons and elevators, specifically parts with P/N CA67001-025, CB36001-003, and CA67006-025. The directive mandates updates to the Aircraft Flight Manual and installation of modifications to ensure continued airworthiness.

Dec 12, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A350Airbus A350-941Airbus A350-1041

EASA AD 2019-0300

Main Rotor — Lower and Upper Torque Scissors — Inspection

EASA Airworthiness Directive 2019-0300 is an airworthiness directive addressing the inspection of Lower and Upper Torque Scissors on PZL SW-4 helicopters. It applies to all serial numbers of this helicopter model and focuses on specific parts including Lower Torque Scissors P/N 60.02.250.00.01 and Upper Torque Scissors P/N 60.02.260.00.02. The directive mandates inspections to ensure correct installation and orientation of these parts to maintain safe helicopter control.

Dec 12, 2019
Airworthiness DirectiveMaintenanceSafety MgmtWsk Pzl-Swidnik SW4PZL SW-4

EASA AD CF-2019-44

Maintenance Requirements Manual — Introduction of New Appendix A2-00 — Candidate Certification Maintenance Requirements Interval Limitations

Maintenance Requirements Manual — Introduction of New Appendix A2-00 — Candidate Certification Maintenance Requirements Interval Limitations is a Canadian Airworthiness Directive (AD CF-2019-44) that applies to Bombardier Inc. models CL-600-2C10, CL-600-2C11, CL-600-2D15, CL-600-2D24, and CL-600-2E25 aeroplanes. This directive mandates the incorporation of a new appendix into the Maintenance Requirements Manual to establish Candidate Certification Maintenance Requirements (CCMR) interval limitations as Airworthiness Limitations. It ensures operators maintain compliance with updated maintenance intervals to uphold aircraft safety.

Dec 12, 2019
Airworthiness DirectiveMaintenanceSafety MgmtMHI RJ Aviation CL-600 (Regional Jet)Bombardier CL-600-2C10Bombardier CL-600-2C11Bombardier CL-600-2D15Bombardier CL-600-2D24Bombardier CL-600-2E25

EASA AD 2018-0043R1

Power Plant — Rear Engine Mount Assembly — Inspection

EASA Airworthiness Directive 2018-0043R1 is a regulatory document addressing inspection requirements for the rear engine mount assembly on Airbus A380-841 and A380-842 aeroplanes. It mandates inspections of specific rear engine mount beams and assemblies, particularly those with part numbers L7121076120000 and related assemblies, to detect cracks caused by manufacturing defects. The directive ensures continued airworthiness by requiring detailed or high-frequency eddy current inspections and, if necessary, replacement of affected parts.

Dec 12, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380Airbus A380-841Airbus A380-842

EASA AD 2016-0232R1

Rotor Drive(s) — Main Gear Box / Emergency Spraying System — Modification / Functional Test

EASA Airworthiness Directive 2016-0232R1 is an updated regulatory requirement affecting Airbus Helicopters EC 225 LP models. It addresses issues related to oil leaks from the main gearbox caused by inadvertent opening of the emergency lubrication system valve during engine start-up. The directive mandates modifications and functional testing to ensure continued safe operation of the main gearbox lubrication system.

Dec 12, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SA 330Airbus Helicopters AS 332Airbus Helicopters EC 225Airbus Helicopters EC 225 LP

EASA AD 2019-0299

Engine — High Pressure Turbine Stage 1 Discs — Life Limit Reduction / Replacement

EASA Airworthiness Directive 2019-0299 is an airworthiness directive addressing Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20, and BR700-710C4-11 engines installed on aircraft such as Bombardier BD-700-1A10, BD-700-1A11, Gulfstream G500, and G550. The directive focuses on reducing the life limit and requiring replacement of certain high pressure turbine stage 1 discs due to a manufacturing quality issue. It mandates identification and removal of affected parts to ensure continued airworthiness and safety.

Dec 10, 2019
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg BR700-710Bombardier BD-700-1A10Bombardier BD-700-1A11Gulfstream G500Gulfstream G550

EASA SIB CE-19-20

Gulfstream Aerospace Corporation G-1159A (G-III), G-IV, GIV-X, GV, GV-SP, and GVI Aeroplanes - Flight Compartment Windows

The Gulfstream Aerospace Corporation G-1159A (G-III), G-IV, GIV-X, GV, GV-SP, and GVI Aeroplanes - Flight Compartment Windows Special Airworthiness Information Bulletin (SAIB: CE-19-20) informs operators about windshield failures on these Gulfstream models. It highlights incidents involving arcing, cracking, smoke, and small fires related to the flight compartment windows and introduces a new windshield design with an improved heater terminal block for replacements.

Dec 10, 2019
Safety Information BulletinMaintenanceSafety Mgmt

EASA SIB CE-19-19

Rockwell Collins TDR-94 and TDR-94D ATC/Mode S Transponders - Update of the Transponder System

The Special Airworthiness Information Bulletin SAIB: CE-19-19 informs owners and operators about detection and tracking issues with aircraft equipped with Rockwell Collins TDR-94 and TDR-94D ATC/Mode S Transponders modified by Service Bulletin TDR-94()-34-30. This bulletin addresses problems experienced by certain ground stations outside the United States, including Multilateration (MLAT) and Air Traffic Control Radar Beacon System (ATCRBS) stations. The issue does not currently warrant an airworthiness directive under 14 CFR part 39.

Dec 10, 2019
Safety Information BulletinMaintenanceSafety Mgmt

EASA AD 2019-0273R1

Airplane Flight Manual — Section Normal Procedures — Amendment

EASA Airworthiness Directive 2019-0273R1 is an amendment addressing the Falcon 900EX and Falcon 2000EX aeroplanes equipped with Dassault's EASy configurations. It mandates changes to the Airplane Flight Manual normal procedures to prevent icing of angle of attack and pitot probes during take-off. This directive ensures safer operation by requiring flight crews to manually activate probe heating during line up.

Dec 9, 2019
Airworthiness DirectiveFlight OpsSafety MgmtDassault Falcon 2000Dassault Falcon 900EXDassault Falcon 2000EX