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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 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SUPERSEDED BY ANAC BRAZIL AD 2021-02-01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SUPERSEDED BY EASA AD 2023-0013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

EASA SIB NE-19-16

Avidyne SkyTrax6XXA Software - Traffic Advisory System - Failure to Display Traffic

The Special Airworthiness Information Bulletin SAIB: NE-19-16 is an FAA informational bulletin addressing a software issue in certain Avidyne SkyTrax6XXA (TAS6XXA) traffic advisory systems used in general aviation aircraft. The affected units, identified by part number 700-00185-() with flight software P/N 510-00296-000 Revisions 00, 01, and 02 (Releases 2.0.0, 2.0.1, and 2.0.2), may intermittently fail to display traffic on interfaced RS-232 display systems. This issue is resolved in flight software Revision 03 (Release 2.0.3).

Dec 9, 2019
Safety Information BulletinSafety MgmtMaintenance

EASA AD 2019-0296

Engine Fuel & Control — Fuel Filter Pre-Blockage Pressure Switch — Replacement

EASA Airworthiness Directive 2019-0296 is an airworthiness directive addressing SAFRAN Helicopter Engines ARRIUS 2G1 engines, commonly installed on Kamov Ka-226T helicopters. The directive mandates the replacement of certain fuel filter pre-blockage pressure switches identified by specific part and serial numbers due to potential non-conformities. This AD aims to ensure continued safe operation by preventing uncommanded engine shutdowns caused by fuel filter contamination.

Dec 9, 2019
Airworthiness DirectiveMaintenanceSafety MgmtSafran ARRIUS 2Kamov Ka-226T

EASA AD US-2019-22-06

Fuel - Fuel Quantity Indicating System Tank Unit - Inspection

Federal Register Volume 84, Number 227 (November 25, 2019) - Airworthiness Directive 2019-22-06 is a final rule issued by the FAA affecting certain Boeing 737-800 series airplanes modified with split winglets per STC ST00830SE. This directive addresses inadequate clearance between the fuel quantity indicating system (FQIS) tank unit and a reinforcement angle added during the split winglet modification, which could pose a fire risk.

Dec 9, 2019
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 737Boeing 737-800

EASA AD 2018-0142R1

SUPERSEDED BY EASA AD 2024-0100

EASA Airworthiness Directive 2018-0142R1 is an amendment addressing Airbus Helicopters AS 332 C, C1, L, and L1 models equipped with dual hoist installations and de-icing systems. This directive focuses on mitigating a vibration issue around 12 Hz caused by specific helicopter configurations that could lead to structural failure or loss of control. It provides requirements for removal of certain dual hoist parts or the de-icing system, or alternatively, operational flight envelope limitations for AS 332 L and L1 helicopters.

Dec 9, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SA 330Airbus Helicopters AS 332Airbus Helicopters EC 225Airbus Helicopters AS 332 CAirbus Helicopters AS 332 C1Airbus Helicopters AS 332 LAirbus Helicopters AS 332 L1

EASA AD 2019-FATA-01020A-07

SUPERSEDED BY FATA AD 2021-FATA-01020A-07

Airworthiness Directive 2019-FATA-01020A-07 issued by the Federal Air Transport Agency of the Russian Federation addresses mandatory inspections and corrective actions for RRJ-95 aircraft. It corrects references related to the one-time inspection of bearings in the links of tracks of slat section 1 on the left-hand and right-hand outer wings. The directive provides updated inspection procedures and replacement requirements to ensure continued airworthiness.

Dec 9, 2019
Airworthiness DirectiveMaintenanceSafety MgmtIrkut Corporation Jsc RRJ-95RRJ-95

EASA AD 2019-FATA-01020A-06

SUPERSEDED BY FATA AD 2021-FATA-01020A-07

Airworthiness Directive 2019-FATA-01020A-06 issued by the Federal Air Transport Agency of the Russian Federation addresses cracks found on the inner ring of bearings of the link of track of slat sections on RRJ-95 aircraft. This directive mandates inspections and replacements of affected track link assemblies on specific RRJ-95 aircraft with manufacturer serial numbers ranging from 95007 to 95220. The directive aims to ensure continued airworthiness and safety of the RRJ-95 fleet by timely detecting and correcting these structural issues.

Dec 9, 2019
Airworthiness DirectiveMaintenanceSafety MgmtIrkut Corporation Jsc RRJ-95RRJ-95

EASA AD 2019-FATA-01020A-09

SUPERSEDED BY FATA AD 2021-FATA-01020A-07

Airworthiness Directive 2019-FATA-01020A-09 issued by the Federal Air Transport Agency of the Russian Federation applies to RRJ-95 aircraft manufactured in the Russian Federation. This directive extends the validity of the previous Airworthiness Directive 2019-FATA-01020F-05 to continue mandatory inspections and corrective actions related to cracks detected in the slat hinge plates of RRJ-95 aircraft. The directive mandates ongoing inspections and replacements to ensure continued airworthiness.

Dec 9, 2019
Airworthiness DirectiveMaintenanceSafety MgmtIrkut Corporation Jsc RRJ-95RRJ-95