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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 2019-0247-E

Engine — Module 01 26-Teeth Bevel Gear — Replacement

EASA Airworthiness Directive 2019-0247-E is an emergency directive addressing SAFRAN HELICOPTER ENGINES MAKILA 2A and 2A1 engines installed on helicopters such as the Airbus Helicopters EC 225 LP. It mandates the replacement of Module 01 26-tooth bevel gears with specific part numbers and serial numbers due to a manufacturing quality issue causing gear tooth rupture. The directive aims to prevent engine in-flight shutdowns and potential loss of helicopter power.

Oct 4, 2019
Airworthiness DirectiveMaintenanceSafety MgmtSafran MAKILA 2Airbus Helicopters EC 225 LP

EASA AD US-2019-18-08

SUPERSEDED BY FAA AD 2021-26-04

Airworthiness Directive 2019-18-08 is a final rule issued by the FAA affecting all Engine Alliance GP7270 and GP7277 model turbofan engines. This directive addresses an unsafe condition related to potential cracks and damage in the engine fan hub assembly, which could lead to uncontained engine failure. It mandates inspections and possible part replacements to ensure continued airworthiness.

Oct 4, 2019
Airworthiness DirectiveMaintenanceSafety MgmtEngine Alliance GP7200

EASA AD US-2019-20-02

SUPERSEDED BY FAA AD 2019-22-10

FAA Airworthiness Directive 2019-20-02 is a final rule addressing all Boeing 737-600, -700, -700C, -800, -900, and -900ER series airplanes. It mandates repetitive inspections for cracking in the left and right side outboard chords of the station 663.75 frame fittings and failsafe straps adjacent to stringer S-18A straps, with required repairs if cracking is found. This directive aims to maintain structural integrity and prevent potential loss of airplane control.

Oct 3, 2019
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 737Boeing 737-600Boeing 737-700Boeing 737-700CBoeing 737-800Boeing 737-900Boeing 737-900ER

EASA AD 2019-0245

Burner — Modification

Burner — Modification is a regulatory document addressing modifications to burners used in various hot air balloon models, including AEROSTATS MA Series, BALLONS CHAIZE CS, JZ, and JZX Series, BALLONS LIBERT, BALLONSERVICE & TECHNIK Schoen, CAMERON Special Shape, Gas and Helium Hot Air Balloons, Sky Hot Air Balloons, KUBICEK FACTORY AB 2 and AB 8, AEROTECHNIK AB, BB, Special Shape Hot Air Balloons, LINDSTRAND TECHNOLOGIES 203T HiFlyer, SCHROEDER FIRE BALLOONS G and S, and ULTRAMAGIC Hot Air Balloons. The document specifies modifications applicable to burners installed on these hot air balloon types.

Oct 1, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAerostats MA Series Hot Air BalloonsBallons Chaize CS SERIES HOT AIR BALLOONSBallons Chaize JZ SERIES HOT AIR BALLOONSBallons Chaize JZX SERIES HOT AIR BALLOONSBallons Libert Libert Hot Air BalloonsBallonservice & Technik Schoen Hot Air BalloonsCameron Balloons Cameron Special Shape Hot Air BalloonsCameron Balloons Gas BalloonsCameron Balloons Helium-Hot Air BalloonsCameron Balloons Hot Air BalloonsCameron Balloons Sky Hot Air BalloonsKubicek Factory S.R.O AB 2 Hot Air BalloonsKubicek Factory S.R.O AB 8 Hot Air BalloonsKubicek Factory S.R.O AEROTECHNIK AB Hot Air BalloonsKubicek Factory S.R.O BB Hot Air BalloonsKubicek Factory S.R.O Special Shape Hot Air BalloonsLindstrand Technologies 203T HiFlyerSchroeder Fire Balloons fire balloons GSchroeder Fire Balloons fire balloons S - Special Shape BalloonsUltramagic Hot Air BalloonsUltramagic Special Shape Hot Air BalloonsAEROSTATS MA SeriesBALLONS CHAIZE CS SeriesBALLONS CHAIZE JZ SeriesBALLONS CHAIZE JZX SeriesBALLONS LIBERTBALLONSERVICE & TECHNIK SchoenCAMERON Special ShapeGas and Helium Hot Air BalloonsSky Hot Air BalloonsKUBICEK FACTORY AB 2KUBICEK FACTORY AB 8AEROTECHNIK ABAEROTECHNIK BBSpecial Shape Hot Air BalloonsSCHROEDER FIRE BALLOONS GSCHROEDER FIRE BALLOONS S

EASA AD 2019-0219

[Correction] Fuselage — Fuselage Bulk Cargo Door Frames — Inspection / Repair

The document titled '[Correction] Fuselage — Fuselage Bulk Cargo Door Frames — Inspection / Repair' is an airworthiness directive correction applicable to Airbus Defence & Space S.A. EASA STC 10034690 and Airbus S.A.S. A330 aircraft. It addresses inspection and repair requirements specifically for the fuselage bulk cargo door frames on these aircraft models. The directive aims to ensure continued structural integrity and safety of the affected fuselage components.

Oct 1, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A330Airbus Defence & Space A330

EASA AD CF-2017-05R2

Fuel System — Motive Flow Line Fouling, Motive Flow Line and Pressure Relief Line Broken P-Clamps, and Vent Line TeflonTM Sleeve Installation

The Canadian Airworthiness Directive CF-2017-05R2 titled 'Fuel System — Motive Flow Line Fouling, Motive Flow Line and Pressure Relief Line Broken P-Clamps, and Vent Line TeflonTM Sleeve Installation' applies to De Havilland DHC-8-400 series aircraft with serial numbers 4001, 4003, and subsequent. It addresses issues related to broken P-clamps on fuel system lines, interference causing wear on the motive flow line, and improper installation of Teflon sleeves on vent lines that could lead to fuel tank ignition risks during lightning strikes.

Oct 1, 2019
Airworthiness DirectiveMaintenanceSafety MgmtDe Havilland Canada DHC-8De Havilland DHC-8-400

EASA AD US-2019-17-01

Fuselage - Upper Fuselage Skin - Inspection / Repair

Federal Register Airworthiness Directive 2019-17-01 is a final rule issued by the FAA addressing certain Learjet, Inc. Model 60 airplanes. It mandates inspections and repairs of the upper fuselage skin to detect and correct corrosion that could compromise structural integrity. This directive updates previous requirements by clarifying inspection areas and compliance times.

Oct 1, 2019
Airworthiness DirectiveMaintenanceSafety MgmtLearjet, 60Learjet 60

EASA AD 2019-0246

Rotors Flight Control — Collective Controls / Protective Cover — Modification

EASA Airworthiness Directive 2019-0246 is an airworthiness directive addressing Airbus Helicopters EC 155 B and EC 155 B1 models. It focuses on the modification of the protective cover for the "SHEAR" control pushbutton on pilot and copilot collective sticks to prevent mechanical deformation and potential unintended shearing of the hoist cable.

Oct 1, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SAAirbus Helicopters AS 365Airbus Helicopters EC 155Airbus Helicopters EC 155 BAirbus Helicopters EC 155 B1

EASA AD 2019-0243

Fuselage — Structure Frames and Joints — Modification / Reinforcement

EASA Airworthiness Directive 2019-0243 is a regulatory document addressing structural modifications and reinforcements for Airbus A340-211, A340-212, A340-213, A340-311, A340-312, and A340-313 aeroplanes. It mandates specific modifications to fuselage structure frames and joints to ensure continued airworthiness and structural integrity. The directive applies to all manufacturer serial numbers of the affected Airbus A340 models.

Sep 30, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A340Airbus A340-211Airbus A340-212Airbus A340-213Airbus A340-311Airbus A340-312Airbus A340-313

EASA AD 2019-0244

SUPERSEDED BY EASA AD 2020-0143

EASA Airworthiness Directive 2019-0244 is an airworthiness directive addressing safety issues in GE Aviation Czech H80-200 and H85-200 engines installed on Aircraft Industries L 410 UVP-E20, L 410 UVP-E20 CARGO, and L 410 NG aeroplanes. It mandates inspections, adjustments, and modifications of the engine push-pull control and beta switch components to prevent uncommanded propeller reverse and potential loss of aircraft control. The directive applies to specific engine configurations and propeller combinations.

Sep 30, 2019
Airworthiness DirectiveMaintenanceSafety MgmtGe Aviation Czech H75, H80, H85Aircraft Industries L 410 UVP-E20Aircraft Industries L 410 UVP-E20 CARGOAircraft Industries L 410 NG

EASA AD US-2019-18-03

Exhaust - Thrust Reverser Upper Locking Actuators - Maintenance Instructions Amendment / Integrity Testing

The Exhaust - Thrust Reverser Upper Locking Actuators - Maintenance Instructions Amendment / Integrity Testing is a Federal Aviation Administration (FAA) airworthiness directive (AD 2019-18-03) applicable to all Boeing 737 series airplanes except models 737-100, -200, -200C, -300, -400, and -500. This directive addresses unsafe conditions related to the thrust reverser upper locking actuator by requiring revisions to maintenance programs and, for certain models, repetitive integrity testing. The AD aims to prevent undetected failures of the locking mechanism that could lead to in-flight thrust reverser deployment and loss of airplane control.

Sep 27, 2019
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 737

EASA AD CF-2019-34

SUPERSEDED BY CANADIAN AD CF-2020-15

Canadian Airworthiness Directive CF-2019-34 addresses the failure risk of bolted fittings in the tail rotor drive shaft couplings on Bell Helicopter Textron Canada Limited models 206, 206A, 206A-1, 206B, 206B-1, 206L, 206L-1, 206L-3, and 206L-4. The directive mandates replacing MS21042 series nuts with NAS9926 series nuts to prevent potential tail rotor drive loss. This AD aims to enhance flight safety by mitigating the risk of tail rotor control failure due to nut cracking or loss.

Sep 27, 2019
Airworthiness DirectiveMaintenanceSafety MgmtBell 206Bell Helicopter Textron Canada Limited 206Bell Helicopter Textron Canada Limited 206ABell Helicopter Textron Canada Limited 206A-1Bell Helicopter Textron Canada Limited 206BBell Helicopter Textron Canada Limited 206B-1Bell Helicopter Textron Canada Limited 206LBell Helicopter Textron Canada Limited 206L-1Bell Helicopter Textron Canada Limited 206L-3Bell Helicopter Textron Canada Limited 206L-4

EASA AD US-2019-18-09

SUPERSEDED BY FAA AD US-2023-09-13

FAA Airworthiness Directive 2019-18-09 is a final rule affecting all Lockheed Martin Corporation/Lockheed Martin Aeronautics Company Model 382 series airplanes and Model C-130A, HP-C-130A, EC-130Q, and C-130B airplanes. It mandates inspections of the center wing upper and lower rainbow fittings for cracks and requires replacement if cracks are found. This directive addresses a critical safety issue involving cracked inner tangs of the center wing lower rainbow fittings.

Sep 27, 2019
Airworthiness DirectiveMaintenanceSafety MgmtLockheed Martin Corporation 382 (Hercules)Lockheed Martin Model 382Lockheed Martin C-130ALockheed Martin HP-C-130ALockheed Martin EC-130QLockheed Martin C-130B

EASA AD 2019-0242

Aircraft Flight Manual — Use of the Disc Braking System — Amendment

EASA Airworthiness Directive 2019-0242 is an amendment concerning the use of the disc braking system on CEAPR DR 400 aeroplanes, including various DR 400 models up to serial number 2668. This directive addresses safety issues related to brake and wing fires caused by incorrect use of the disc braking system. It applies to aircraft equipped with disc brakes and not modified by CEAPR modification DET150102.

Sep 26, 2019
Airworthiness DirectiveFlight OpsSafety MgmtCeapr DR 400

EASA AD US-2019-19-11

SUPERSEDED BY FAA AD 2019-21-11

FAA Airworthiness Directive 2019-19-11 is a final rule addressing certain Pratt & Whitney PW1500G and PW1900G model turbofan engines. It mandates initial and repetitive inspections of the low-pressure compressor inlet guide vane and rotor 1, with potential replacement of the low-pressure compressor based on inspection results. This directive aims to prevent failures that have caused recent in-flight shutdowns.

Sep 26, 2019
Airworthiness DirectiveMaintenanceSafety MgmtPratt & Whitney PW1500GPratt & Whitney PW1900G

EASA AD CF-2019-32

Engine — High Pressure Turbine Rear Cover Life Limitation Reduction

Canadian Airworthiness Directive CF-2019-32 addresses the life limitation reduction of the High Pressure Turbine (HPT) rear cover on Pratt & Whitney Canada model PW127G engines. This directive mandates compliance with updated low cycle fatigue life values for specific HPT rear cover parts, identified as P/Ns 3039639 and 3078516-01. The directive aims to ensure continued airworthiness by preventing engine and potential aircraft damage due to part failure.

Sep 25, 2019
Airworthiness DirectiveMaintenanceSafety MgmtPratt & Whitney Canada PW100

EASA AD 2019-0240

Fuel — Saddle Clamps / Motive-Flow Fuel Pipes — Replacement / Alignment

EASA Airworthiness Directive 2019-0240 is an airworthiness directive issued by EASA affecting all Pilatus PC-24 aeroplanes. It addresses the replacement and alignment of flexible saddle clamps and motive-flow fuel pipes installed between frame 34 and 36 to prevent potential fuel leaks. The directive mandates the replacement of specific flexible saddle clamps with fixed saddle clamps to ensure continued airworthiness and safety.

Sep 25, 2019
Airworthiness DirectiveMaintenanceSafety MgmtPilatus Aircraft PC-24Pilatus PC-24

EASA AD 2019-0237R1

Cabin Systems — Canopy Lock / Rear Locking Rods — Inspection / Check / Repair Aircraft Flight Manual — Amendment

EASA Airworthiness Directive 2019-0237R1 is an amendment addressing inspection, check, and repair requirements for the canopy lock and rear locking rods on DG-Flugzeugbau GmbH DG-500 and DG-1000 sailplanes and powered sailplanes. This directive applies to all serial numbers of DG-500 variants and DG-1000S and DG-1000T sailplanes up to serial number 10-144 inclusive. It mandates inspections and repairs to ensure the canopy locking mechanisms function correctly to prevent blockage of the emergency canopy release system.

Sep 24, 2019
Airworthiness DirectiveMaintenanceSafety MgmtDg Aviation Gmbh DG-1000Dg Aviation Gmbh DG-500DG-Flugzeugbau DG-500DG-Flugzeugbau DG-1000

EASA SIB 2019-12

Cable Terminals used on Small Aeroplanes with a Mechanical Flight Control Cable System

EASA Safety Information Bulletin 2019-12 is an airworthiness bulletin addressing cable terminals used on small aeroplanes with mechanical flight control cable systems. It highlights a safety concern regarding cracking and fracturing of flight control cable terminal attachment fittings connected to turnbuckle barrels. This bulletin applies to aeroplanes certified under CS-23, JAR-23, FAR-23, or equivalent regulations.

Sep 24, 2019
Safety Information BulletinMaintenanceSafety Mgmt

EASA AD 2019-0235

[Correction] ACR ELECTRONICS, Inc. — Emergency Locator Transmitter — Inspection / Modification / Replacement

EASA Airworthiness Directive 2019-0235 is a regulatory document addressing emergency locator transmitters (ELTs) manufactured by ACR Electronics, Inc., specifically models G406-4, C406-1, C406-1HM, C406-2, C406-2HM, C406-N, and C406-NHM. These ELTs are installed on various Part 23 and Part 25 aeroplanes and helicopters. The directive mandates inspection, testing, modification, and replacement procedures to ensure the proper functioning of the ELTs' longitudinal G-switch.

Sep 24, 2019
Airworthiness DirectiveMaintenanceSafety Mgmt