RegNotify

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 2019-0242

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SUPERSEDED BY FAA AD 2019-21-11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

EASA AD 2019-0238

Pneumatic — Bleed Control Computer — Check

The Pneumatic — Bleed Control Computer — Check document is an explanatory statement issued by EASA regarding the absence of an Airworthiness Directive (AD) for the Airbus A400M aircraft in civil service. It clarifies that no publicly available AD exists because the Airbus A400M is currently not operated in civil aviation. The document serves as an informational record for military authorities and design approval holders, recommending that military authorities issue their own applicable ADs.

Sep 24, 2019
OtherMaintenanceSafety MgmtAirbus Military A400MAirbus A400M

EASA AD 2019-0230

[Correction] Engine — Oil Service Pipe Sealing Rings — Inspection / Replacement / Modification / Rework

EASA Airworthiness Directive 2019-0230 is a regulatory document addressing inspection, replacement, modification, and rework of oil service pipe sealing rings on Rolls-Royce Deutschland RB211 Trent 900 engines, commonly installed on Airbus A380 aircraft. The directive targets high pressure/intermediate pressure support structure oil service tube buffer sealing rings with Part Number FW64487 to prevent potential engine failures. It mandates life limits, inspections, and modifications to ensure continued airworthiness and safety.

Sep 20, 2019
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg RB211 TRENT 900Airbus A380

EASA AD 2012-0108R1

Fuselage — Frame No.9 — Inspection / Repair

The document titled 'Fuselage — Frame No.9 — Inspection / Repair' pertains to AIRBUS HELICOPTERS models SA/AS 365 and EC 155. It addresses inspection and repair procedures specifically for Frame No.9 of the fuselage structure on these helicopter types. The document provides guidance to ensure structural integrity and airworthiness of the affected aircraft.

Sep 19, 2019
OtherMaintenanceSafety MgmtAirbus Helicopters SAAirbus Helicopters AS 365Airbus Helicopters EC 155Airbus Helicopters SA 365

EASA AD 2019-0233

SUPERSEDED BY EASA AD 2022-0111

EASA Airworthiness Directive 2019-0233 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting certain Airbus A319, A320, and A321 aircraft models. It addresses incomplete installations of overwing panel lug attachments that could compromise wing structural integrity. The directive mandates inspections and corrective actions to ensure continued airworthiness of the affected aircraft.

Sep 19, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A319Airbus A320Airbus A321

EASA AD 2019-0234

SUPERSEDED BY EASA AD 2022-0129

EASA Airworthiness Directive 2019-0234 is an airworthiness directive issued by the European Union Aviation Safety Agency concerning Rolls-Royce Trent XWB series engines installed on Airbus A350 aircraft. The directive mandates inspections of the front engine mount support structure, specifically the low pressure compressor outlet guide vane outer mount ring assembly, to detect potential failures that could lead to engine separation.

Sep 19, 2019
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg TRENT XWBAirbus A350

EASA AD 2019-0229R1

Exhaust — Thrust Reverser Cascades and Aft Frame Attachment — Inspection / Modification

EASA Airworthiness Directive 2019-0229R1 is an updated regulatory requirement addressing inspection and modification of the thrust reverser cascades and aft frame attachments on Airbus A380-861 aeroplanes equipped with GP7200 engines. It mandates detailed inspections and modifications of specific thrust reverser parts identified by part and serial numbers to prevent potential part failure and detachment. The directive references Airbus and SAFRAN Nacelles service bulletins for compliance procedures.

Sep 18, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380

EASA AD US-2019-18-01

Turbine - Low-Pressure Turbine Stage 6 Disks - Replacement

The Federal Aviation Administration Airworthiness Directive 2019-18-01 is a final rule addressing certain International Aero Engines AG V2500 model turbofan engines. It targets specific low-pressure turbine (LPT) stage 6 disks identified with material anomalies that could compromise engine safety. This directive mandates the removal and replacement of affected LPT stage 6 disks to prevent potential engine failure and damage to the aircraft.

Sep 17, 2019
Airworthiness DirectiveMaintenanceSafety MgmtInternational Aero Engines Ag V2500-( )5

EASA AD 2019-0232

Hydraulic Power — Hydraulic Reservoir Pressurisation Lines — Modification

Hydraulic Power — Hydraulic Reservoir Pressurisation Lines — Modification is a regulatory document applicable to Airbus S.A.S. aircraft models A319, A320, and A321. It addresses modifications related to the hydraulic reservoir pressurisation lines to ensure continued airworthiness and system reliability. The document provides guidance on required changes to maintain hydraulic system integrity on these aircraft types.

Sep 16, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A319Airbus A320Airbus A321

EASA AD US-2019-15-07

[Correction] Fuselage - Fuselage Lower Lobe Frames - Inspection

Correction to Airworthiness Directive 2019-15-07 issued by the Federal Aviation Administration (FAA) concerning certain Boeing 737-100, 737-200, 737-200C, 737-300, 737-400, and 737-500 series airplanes. This correction addresses an incorrect paragraph reference in the original directive related to inspections of fuselage lower lobe frames. The directive mandates repetitive inspections and applicable repairs to prevent structural failure due to cracking in the fuselage frames.

Sep 13, 2019
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 737

EASA AD 2019-0231

Flight Controls — Flap Drive System / Flap Fairings and Front Inboard Tension Rods — Inspection / Modification / Replacement

EASA Airworthiness Directive 2019-0231 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Pilatus Aircraft Ltd PC-12/47E aeroplanes with manufacturer serial numbers 1576 and higher. It addresses inspection, modification, and replacement requirements for the flap drive system, specifically the inboard flap fairings aft (IFFA) and front inboard tension rods. The directive aims to ensure continued airworthiness by preventing potential flap drive arm failure due to chafing and corrosion.

Sep 13, 2019
Airworthiness DirectiveMaintenanceSafety MgmtPilatus Aircraft PC-12Pilatus PC-12/47E

EASA AD CF-2016-13R1

Main Rotor Drive — Loss of Lubrication to the Freewheel Assembly

The Canadian Airworthiness Directive CF-2016-13R1 titled 'Main Rotor Drive — Loss of Lubrication to the Freewheel Assembly' applies to Bell Helicopter Textron Canada Limited models 206A, 206B, 206L series, and 407 helicopters. It addresses the risk of main rotor mast failure caused by blocked oil restrictors in the freewheel lubrication circuit, which can lead to loss of helicopter control. The directive mandates inspections, cleaning, and possible replacement of components to ensure proper lubrication flow.

Sep 13, 2019
Airworthiness DirectiveMaintenanceSafety MgmtBell 206Bell 407Bell Helicopter Textron Canada 206ABell Helicopter Textron Canada 206BBell Helicopter Textron Canada 206L seriesBell Helicopter Textron Canada 407

EASA AD US-2019-16-16

Engine Air Intake System - Rotorcraft Flight Manual Supplement - Revision

The Federal Aviation Administration (FAA) Airworthiness Directive 2019-16-16 is a final rule superseding AD 2018-18-12 concerning Airbus Helicopters Model AS350B, AS350B1, AS350B2, AS350B3, and AS350BA equipped with certain Pall Aerospace Inlet Barrier Filter (IBF) elements. This directive addresses unsafe conditions related to water ingestion by the engine due to affected IBF elements, which can cause engine flameout and loss of helicopter control. The AD expands applicability to additional IBF part numbers and prohibits reinstalling removed filters or installing affected filters on any helicopter.

Sep 12, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters AS 350Airbus Helicopters EC 130Airbus Helicopters AS350BAirbus Helicopters AS350B1Airbus Helicopters AS350B2Airbus Helicopters AS350B3Airbus Helicopters AS350BA