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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 2019-0238

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SUPERSEDED BY EASA AD 2022-0111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

EASA AD 2019-0228

Equipment / Furnishings — Electric Hoist Installation — Modification

EASA Airworthiness Directive 2019-0228 addresses the electric hoist installation modification on Airbus Helicopters AS 350 and AS 355 models. It targets electric hoists manufactured by BREEZE, TRW, LUCAS, or AIR EQUIPEMENT installed with specific hoist boxes, ensuring proper electrical modifications are applied to guarantee emergency release functionality. The directive mandates verification and correction of the hoist electrical system to prevent failure in emergency cable release.

Sep 12, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters AS 350Airbus Helicopters EC 130Airbus Helicopters AS 355

EASA AD US-2019-10-51

Fuselage - Fuselage Frame - Inspection

Federal Register Volume 84, Number 171 (September 4, 2019) Final Rule Airworthiness Directive 2019-10-51 addresses all Airbus Helicopters Deutschland GmbH Model MBB-BK 117 C-2 helicopters. This directive mandates inspection of the fuselage frame for fatigue cracks and prohibits installation of certain recessed medical wall components installed under Supplemental Type Certificate SR00592DE. The directive aims to mitigate risks of structural failure due to reported cracks in the fuselage frame.

Sep 12, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters MBB-BK 117Airbus Helicopters MBB-BK 117 C-2

EASA AD CF-2019-14R1

SUPERSEDED BY TRANSPORT CANADA AD CF-2020-25

The Canadian Airworthiness Directive CF-2019-14R1 is an amendment to the previous directive CF-2019-14, applicable to Airbus Canada Limited Partnership aircraft models BD-500-1A10 and BD-500-1A11. This directive mandates the incorporation of updated airworthiness limitations and maintenance tasks as specified in the June 6, 2019 edition 009.00 of the CSALP airworthiness limitations publication. It ensures that operators maintain compliance with Transport Canada's approved maintenance schedules for these aircraft models.

Sep 12, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus BD-500 (A220 Series)Airbus Canada BD-500-1A10Airbus Canada BD-500-1A11

EASA AD 2019-0227

Electric and Electronic Common Installation — Electrical Wiring — Modification

EASA Airworthiness Directive 2019-0227 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A319 and A320 aeroplanes, specifically models A319-112, A319-115, A319-132, A320-214, A320-216, A320-232, and A320-233. The directive addresses a potential interference issue between electrical wiring harnesses and tapping units in the aircraft's lavatory smoke detection and passenger oxygen systems. This interference could compromise the delivery of passenger oxygen during emergencies.

Sep 11, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A319Airbus A320

EASA SIB 2019-09R1

Emergency Locator Transmitters and Personal Locator Beacon - Annual Testing

EASA Safety Information Bulletin 2019-09R1 is an airworthiness bulletin addressing the annual testing and inspection of Emergency Locator Transmitters (ELT) and Personal Locator Beacons (PLB) installed on aircraft. It applies to all operators of aircraft equipped with Automatic Fixed or Automatic Portable ELTs, as well as operators carrying PLBs under Regulation (EU) 965/2012. The bulletin emphasizes proper testing procedures to ensure beacon reliability and prevent false alerts that could divert Search and Rescue resources.

Sep 11, 2019
Safety Information BulletinMaintenanceSafety Mgmt

EASA AD 2019-0226

Landing Gear — Centre Landing Gear Wheel Axle — Replacement

EASA Airworthiness Directive 2019-0226 is an airworthiness directive addressing the replacement of centre landing gear wheel axles on Airbus A340-541, A340-542, A340-642, and A340-643 aeroplanes. The directive targets specific wheel axles with part numbers 55-1107065-00 and 55-1107069-00 that have been identified as affected due to corrosion found during overhaul. It mandates replacement of these affected parts to ensure continued airworthiness.

Sep 11, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A340Airbus A340-541Airbus A340-542Airbus A340-642Airbus A340-643

EASA AD 2019-0225-E

Main Rotor Drive - Main Gearbox Drive Shaft / Engine Coupling - Inspection

EASA Airworthiness Directive 2019-0225-E is an emergency directive addressing the inspection of the main gearbox drive shaft and engine coupling on Airbus Helicopters AS 350 B3 and EC 130 T2 models equipped with SAFRAN ARRIEL 2D engines. It mandates a one-time visual inspection of the affected parts on helicopters with less than 300 flight hours since first flight. The directive aims to ensure continued airworthiness following an accident involving an AS 350 B3 helicopter.

Sep 11, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters AS 350Airbus Helicopters EC 130Airbus Helicopters AS 350 B3Airbus Helicopters EC 130 T2