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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 US-2019-08-03

Fuselage - Section 43 Lower Lobe Frames - Inspection

Federal Aviation Administration Airworthiness Directive 2019-08-03 is a final rule addressing certain Boeing 737-100, -200, -200C, -300, -400, and -500 series airplanes. It mandates repetitive detailed, general visual, and high frequency eddy current inspections of the section 43 lower lobe frames between station 380 and station 520, as well as inspections to identify certain repairs and applicable on-condition actions. This directive aims to detect and mitigate frame web and integral inboard chord cracking below the passenger floor.

Jun 4, 2019
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 737Boeing 737-100Boeing 737-200Boeing 737-200CBoeing 737-300Boeing 737-400Boeing 737-500

EASA AD 2019-0122

Fuselage — Side Box Beam Flange in Frame 43 Area — Inspection / Repair / Modification

EASA Airworthiness Directive 2019-0122 is an airworthiness directive addressing inspection, repair, and modification of the fuselage side box beam flange in the Frame 43 area on Airbus A318, A319, A320, and A321 aeroplanes. It applies to aircraft with Airbus modification 21202 embodied in production, excluding those with modification 152569. The directive mandates repetitive inspections and corrective actions to detect and repair cracks that could compromise structural integrity.

Jun 4, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2018-0254R1

Wings — Roll Spoiler Bearing Arms — Inspection

EASA Airworthiness Directive 2018-0254R1 is an updated safety directive addressing the inspection of roll spoiler bearing arms on Dornier 328-100 aeroplanes. It mandates a one-time non-destructive eddy current inspection of specific roll spoiler bearing arm parts to detect cracks that could impair roll spoiler functionality. The directive applies to all serial numbers of Dornier 328-100 aircraft and aims to prevent potential loss of control due to unresponsive roll spoilers.

Jun 4, 2019
Airworthiness DirectiveMaintenanceSafety MgmtDeutsche Aircraft Gmbh Dornier 328Dornier 328-100

EASA AD CF-2019-20R1

Decompression Panel — Flight Compartment Door — Upper Panel

Airworthiness Directive CF-2019-20R1 is issued by Transport Canada and applies to Bombardier Inc. model CL-600-2C10, CL-600-2D15, CL-600-2D24, and CL-600-2E25 aircraft. This directive addresses the incorrect installation of cockpit door edge protection plates on the upper decompression panel, which could prevent the panel from opening during rapid decompression. The directive mandates maintenance schedule updates to ensure the decompression panel functions correctly.

Jun 3, 2019
Airworthiness DirectiveMaintenanceSafety MgmtMHI RJ Aviation CL-600 (Regional Jet)Bombardier CL-600-2C10Bombardier CL-600-2D15Bombardier CL-600-2D24Bombardier CL-600-2E25

EASA AD 2019-0120

Electrical Power — Power Transfer Contactors — Replacement

EASA Airworthiness Directive 2019-0120 is an official regulatory document addressing electrical power transfer contactors on Fokker Services B.V. F28 Mark 0100 aeroplanes. It mandates the replacement of specific generator, essential bus, and auxiliary power transfer contactors with new parts to prevent smoke and electrical power loss in the cockpit.

May 29, 2019
Airworthiness DirectiveMaintenanceSafety MgmtFokker F28Fokker F28 Mark 0100

EASA AD 2019-0118

Equipment / Furnishings — Emergency Flotation Unit — Replacement Rotorcraft Flight Manual / Master Minimum Equipment List — Revision

EASA Airworthiness Directive 2019-0118 is an airworthiness directive affecting Airbus Helicopters EC175 B models. It addresses issues related to the Emergency Flotation Unit (EFU), specifically parts with manufacturer part numbers SE13876 and SE24251, requiring updates to the Rotorcraft Flight Manual and Master Minimum Equipment List.

May 29, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters EC175Airbus Helicopters EC175 B

EASA AD 2019-0119-E

Flight Controls — Flap Actuator — Inspection / Replacement

EASA Airworthiness Directive 2019-0119-E is an emergency directive addressing flap actuator inspections and replacements for Leonardo S.p.A. F260 series aeroplanes, including F260, F260B, F260C, F260D, F260E, F260F, and SF260TP models. The directive targets flap actuators with specific part numbers SF260-12-215-01, SF260-12-215-101, and SF260-12-215-09 due to detected cracks. It mandates inspections and potential replacement to ensure continued airworthiness.

May 29, 2019
Airworthiness DirectiveMaintenanceSafety MgmtLeonardo S.P.A. Aircraft F260Leonardo F260Leonardo F260BLeonardo F260CLeonardo F260DLeonardo F260ELeonardo F260FLeonardo SF260TP

EASA AD 2019-0117

Main Rotor — Blades — Inspection / Replacement

EASA Airworthiness Directive 2019-0117 is an airworthiness directive addressing inspection and replacement requirements for main rotor blades on MECAER AVIATION GROUP S.P.A. NH-500D and AMD500N helicopters. The directive applies specifically to main rotor blades with part numbers 369D21100-(), 369D21120-(), and 369D21102-() manufactured by Helicopter Technology Company, LLC and Breda-Nardi S.p.A. It mandates repetitive inspections to detect cracks near the trim tab area to prevent potential in-flight failures.

May 29, 2019
Airworthiness DirectiveMaintenanceSafety MgmtMecaer Aviation Group Spa AMD-500NMecaer Aviation Group Spa NH-500DMECAER AVIATION GROUP S.P.A. NH-500DMECAER AVIATION GROUP S.P.A. AMD500N

EASA AD 2019-0115

Equipment / Furnishings — Baby Bassinet Inserts — Inspection / Modification

EASA Airworthiness Directive 2019-0115 is an official regulatory document addressing the inspection and modification of baby bassinet inserts installed on Airbus A350-941 aeroplanes, specifically those with manufacturer serial numbers ranging from 0005 to 0255 as listed. The directive mandates repetitive inspections and corrective actions to ensure the secure attachment of baby bassinet inserts on stowages and partitions to prevent potential detachment and injury. It applies to Airbus A350 aircraft and involves specific part numbers and service bulletins for compliance.

May 28, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A350

EASA AD 2019-0116

SUPERSEDED BY EASA ADR 2021-0268

The document titled SUPERSEDED BY EASA ADR 2021-0268 is an explanatory statement regarding the absence of an Airworthiness Directive (AD) for the Airbus A400M aeroplane in civil service. It clarifies that no publicly available AD exists because the Airbus A400M is not operated in civil aviation. The document serves as an informational record provided by EASA to military authorities and design approval holders.

May 28, 2019
OtherSafety MgmtAirbus Military A400MAirbus A400M

EASA AD 2019-0113

Engine Fuel & Control — Engine Electronic Control Software — Update

EASA Airworthiness Directive 2019-0113 is an official directive addressing Rolls-Royce RB211 Trent 970-84, 972-84, and 972E-84 engines, commonly installed on Airbus A380 aircraft. The directive mandates an update to the engine electronic controller (EEC) software to version 12.3 or later to enhance safety. This update targets the intermediate pressure turbine over-speed system to prevent potential engine failures.

May 24, 2019
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg RB211 TRENT 900Airbus A380

EASA AD 2019-0114

SUPERSEDED BY EASA AD 2019-0297

EASA Airworthiness Directive 2019-0114 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A340-541, A340-542, A340-642, and A340-643 aeroplanes. It addresses cracks found on the wing lower skin covers at rib bay 3/4 on both left-hand and right-hand sides, which could lead to fuel leaks and reduced structural strength. The directive mandates inspections to detect these cracks and ensure continued airworthiness.

May 24, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A340Airbus A340-541Airbus A340-542Airbus A340-642Airbus A340-643

EASA AD CF-2018-26R1

Landing Gear — Main Landing Gear Side Stay Actuators Contain Non-Conforming Split Ball Bearing

The Canadian Airworthiness Directive CF-2018-26R1 addresses an issue with Bombardier Inc. CL-600-2B16 aircraft, serial numbers 5301 through 5665, 5701 through 5988, and 6050 through 6091, equipped with split ball bearing Part Number 104467672 in the main landing gear side stay actuators. This directive mandates verification and possible replacement of non-conforming split ball bearings to prevent asymmetric landing gear extension or retraction that could lead to gear collapse during landing.

May 23, 2019
Airworthiness DirectiveMaintenanceSafety MgmtBombardier CL-600 (Challenger)Bombardier CL-600-2B16

EASA SIB SAFO19002

McCauley Constant Speed Propellers - Improper Overhaul and Repair by Sensenich Propeller Services, Inc., North Windham, Connecticut

SAFO 19002 is a Safety Alert for Operators issued by the FAA regarding improper overhaul and repair of McCauley Constant Speed Propellers by Sensenich Propeller Services, Inc., located in North Windham, Connecticut. The alert affects all McCauley Constant Speed Propellers overhauled by this maintenance provider, which failed to follow the manufacturer's recommended overhaul procedures. This includes failure to test or replace critical components such as propeller return springs and other key parts.

May 23, 2019
Safety AlertMaintenanceSafety Mgmt

EASA AD 2017-0020R1

Tail Rotor — Pitch Rod — Inspection

EASA Airworthiness Directive 2017-0020R1 is an updated safety directive addressing inspection requirements for the tail rotor pitch rod on Airbus Helicopters AS 350 and AS 355 models. It mandates repetitive visual inspections of the elastomeric ball-joint of the tail rotor pitch rod to detect damage that could lead to loss of helicopter control. The directive applies to all serial numbers of AS 350 B, BA, BB, B1, B2, B3 and AS 355 E, F, F1, F2, N, and NP helicopters incorporating specific modifications.

May 22, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters AS 350Airbus Helicopters EC 130Airbus Helicopters AS 355Airbus Helicopters AS 350 BAirbus Helicopters AS 350 BAAirbus Helicopters AS 350 BBAirbus Helicopters AS 350 B1Airbus Helicopters AS 350 B2Airbus Helicopters AS 350 B3Airbus Helicopters AS 355 EAirbus Helicopters AS 355 FAirbus Helicopters AS 355 F1Airbus Helicopters AS 355 F2Airbus Helicopters AS 355 NAirbus Helicopters AS 355 NP

EASA AD CF-2019-21

Wing Structure — Lower Wing Plank — Cracking at Stringer Run-out

The Canadian Airworthiness Directive CF-2019-21 addresses fatigue cracking detected in the lower wing plank at the stringer run-out area on Bombardier Inc. CL-600-2B19 aircraft, serial number 7003 and later. This directive mandates updated inspection procedures to detect potential cracks in the right lower wing plank to ensure structural integrity. It applies specifically to the wing structure of these Bombardier regional jets.

May 22, 2019
Airworthiness DirectiveMaintenanceSafety MgmtMHI RJ Aviation CL-600 (Regional Jet)Bombardier CL-600-2B19

EASA AD 2019-0112

Engine Fuel & Control — Engine Electronic Controller Software — Update

EASA Airworthiness Directive 2019-0112 is an official directive addressing Rolls-Royce Trent XWB-75, XWB-79, XWB-79B, and XWB-84 engines installed on Airbus A350 aircraft. It mandates an update to the engine electronic controller software to correct fuel flow limits and low pressure shaft speed parameters. This directive ensures continued airworthiness and safe operation of affected engines.

May 21, 2019
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg TRENT XWBAirbus A350

EASA AD 2019-0110

Engine — Torque Conformation Box — Check

The document titled 'Engine — Torque Conformation Box — Check' is a technical directive concerning the SAFRAN HELICOPTER ENGINES: ARRIEL 2 engine model. It addresses inspection and verification procedures for the torque conformation box component to ensure engine reliability and safety. This directive is relevant for operators and maintenance organizations managing helicopters equipped with the ARRIEL 2 engine.

May 21, 2019
Airworthiness DirectiveMaintenanceSafety MgmtSafran ARRIEL 2Safran Helicopter Engines Arriel 2

EASA AD 2019-0111

SUPERSEDED BY EASA AD 2021-0218

EASA Airworthiness Directive 2019-0111 is an airworthiness directive issued by the European Union Aviation Safety Agency concerning ATR 42 and ATR 72 aeroplanes. It addresses oxygen cylinders with Part Number 89794077 that may have a manufacturing defect leading to oxygen leakage. The directive mandates inspection and possible replacement of affected oxygen cylinders to ensure safety.

May 21, 2019
Airworthiness DirectiveMaintenanceSafety MgmtATR ATR42ATR ATR72ATR 42ATR 72

EASA AD CF-2019-18

Oxygen System — Insufficient Accessibility to the Portable Oxygen Bottle

Canadian Airworthiness Directive CF-2019-18 addresses an oxygen system issue affecting Bombardier Inc. aeroplanes Model BD-700-1A10 and BD-700-1A11 with specified serial numbers. The directive mandates modifications to the portable oxygen bottle brackets to improve accessibility for cabin crew during emergencies. This AD ensures compliance with Canadian Aviation Regulations related to airworthiness directives.

May 20, 2019
Airworthiness DirectiveMaintenanceSafety MgmtBombardier BD-700Bombardier BD-700-1A10Bombardier BD-700-1A11