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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-2024-12-07

Fuselage - Lavatory Service Panel, Access Pan, and Attaching Structure - Inspection

The Federal Register document titled 'Fuselage - Lavatory Service Panel, Access Pan, and Attaching Structure - Inspection' is a final rule airworthiness directive (AD 2024-12-07) issued by the FAA affecting Boeing 757-200 airplanes modified by specific supplemental type certificates. It addresses reports of cracking in and around the lavatory service panel structure. The AD mandates repetitive inspections, reinforcement of the attaching structure, and repair or replacement of affected parts to ensure continued airworthiness.

Jun 28, 2024
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 757Boeing 757-200

EASA AD 2024-0123

Landing Gear — Hydraulic Line Restrictor Check Valve — Replacement

EASA Airworthiness Directive 2024-0123 is issued for Fokker Services B.V. F28 Mark 0070 and Mark 0100 aeroplanes. It addresses the replacement of hydraulic line restrictor check valves in the main landing gear hydraulic system to ensure continued airworthiness and safety. The directive applies to specific part numbers of restrictor check valves installed in the hydraulic return line of the parking brake shut-off valve.

Jun 28, 2024
Airworthiness DirectiveMaintenanceSafety MgmtFokker F28Fokker F28 Mark 0070Fokker F28 Mark 0100

EASA AD 2024-0122

SUPERSEDED BY EASA AD 2025-0233

EASA Airworthiness Directive 2024-0122 is an airworthiness directive addressing Rolls-Royce Trent 1000 series engines installed on Boeing 787 aircraft. It mandates repetitive borescope inspections of the high-pressure compressor mini-disc anti-rotation block to detect potential part release that could compromise engine safety. The directive applies to Trent 1000-A, AE, C, CE, D, E, G, and H models with specific service bulletins embodied, excluding those with a particular production modification.

Jun 28, 2024
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg TRENT 1000Boeing 787

EASA AD 2024-0119

Fire Protection — Engine Pylon Fire Detector — Replacement

EASA Airworthiness Directive 2024-0119 is an airworthiness directive addressing fire protection on Airbus A330 aeroplanes. It specifically targets the replacement of engine pylon fire detectors with part numbers 10-3001-00 or 10-3002-00 that are contaminated and may fail to detect fires reliably. The directive applies to multiple Airbus A330 variants with certain Airbus modifications embodied.

Jun 27, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A330

EASA AD 2024-0120

Stabilizers — Vertical Tail Plane Forward and Aft Fittings — Inspection

EASA Airworthiness Directive 2024-0120 is an airworthiness directive addressing ATR 42 and ATR 72 aeroplanes, specifically certain manufacturer serial numbers equipped with vertical tail plane forward and aft fittings. The directive mandates inspection of these fittings due to a potential use of improper material during production, which could compromise structural integrity. The affected parts include specific fuselage to vertical tail plane fittings identified by part numbers S5537490120400, S5537490220400, S5537490320000, and S5537490420000.

Jun 27, 2024
Airworthiness DirectiveMaintenanceSafety MgmtATR ATR42ATR ATR72ATR 42ATR 72

EASA AD 2024-0121

Time Limits / Maintenance Checks — Certification Maintenance Requirements and Airworthiness Limitations — Amendment

EASA Airworthiness Directive 2024-0121 is an amendment addressing the time limits and maintenance checks for ATR 42-200, ATR 42-300, and ATR 42-320 aeroplanes. It updates the Certification Maintenance Requirements and Airworthiness Limitations as defined in the ATR 42-200/-300/-320 Time Limits Document (TLD) Revision 13. This directive ensures continued airworthiness by mandating compliance with updated maintenance tasks and life limits for components.

Jun 27, 2024
Airworthiness DirectiveMaintenanceSafety MgmtATR ATR42ATR 42-200ATR 42-300ATR 42-320

EASA AD US-2024-11-01

Electrical Power - Nickel-Cadmium Batteries during Aeroplane Parking or Storage - Replacement

The Electrical Power - Nickel-Cadmium Batteries during Aeroplane Parking or Storage - Replacement is a Federal Aviation Administration (FAA) Airworthiness Directive (AD 2024-11-01) that applies to various Airbus SAS airplane models including A300, A310, A318, A319, A320, A321, A330, A340, A350, and A380 series equipped with certain parts manufacturer approval (PMA) nickel-cadmium (Ni-Cd) batteries. This AD addresses the issue of reduced battery endurance performance during airplane parking or storage periods. It mandates replacement of affected PMA Ni-Cd batteries with serviceable parts to ensure electrical power reliability during abnormal or emergency conditions.

Jun 26, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A300Airbus A300-600Airbus A300-600ST (Beluga)Airbus A310Airbus A318Airbus A319Airbus A320Airbus A321Airbus A330Airbus A340Airbus A350Airbus A380

EASA AD 2024-0117

Engine — Propeller Gear Box / Post Flight Report — Check

The document titled Engine — Propeller Gear Box / Post Flight Report — Check is an informational Airworthiness Directive record created by EASA regarding the Europrop International GmbH TP400-D6 engine. It clarifies that no Europrop TP400-D6 engines are currently in civil service, so no public AD exists. The document serves as a recommendation for military authorities responsible for aircraft equipped with these engines to issue their own applicable ADs.

Jun 25, 2024
Airworthiness DirectiveMaintenanceSafety MgmtEpi Europrop International Gmbh TP400-D6

EASA AD 2024-0115-CN

CANCELLED: Engine Fuel and Control — Check of Correct Position of Adjusted Fuel Control Unit

EASA Airworthiness Directive Cancellation Notice 2024-0115-CN cancels the previous DGAC France AD F-2005-088 which addressed the inspection of the fuel control unit position on SAFRAN Helicopter Engines ARRIUS 2F engines. These engines are commonly installed on EC 120B helicopters. The cancellation reflects that all affected engines have been inspected and corrected where necessary, and the safety risk no longer qualifies as an unsafe condition.

Jun 21, 2024
Airworthiness DirectiveMaintenanceSafety MgmtSafran ARRIUS 2Airbus Helicopters EC 120B

EASA AD 2021-0124R2

Engine — Low Pressure Turbine Stage 2 Discs — Replacement

EASA Airworthiness Directive record for Engine — Low Pressure Turbine Stage 2 Discs — Replacement provides information regarding the Europrop International GmbH TP400-D6 engine. This document clarifies that no civil service aircraft currently use the TP400-D6 engine, and therefore no public AD exists. The record serves as a recommendation for military authorities responsible for affected aircraft equipped with TP400-D6 engines.

Jun 21, 2024
Airworthiness DirectiveMaintenanceSafety MgmtEpi Europrop International Gmbh TP400-D6

EASA AD 2024-0116

SUPERSEDED BY EASA AD 2025-0119

EASA Airworthiness Directive 2024-0116 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Rolls-Royce Deutschland Ltd & Co KG Trent XWB-75, Trent XWB-79, Trent XWB-79B, and Trent XWB-84 engines. These engines are commonly installed on Airbus A350 aircraft. The directive mandates compliance with updated airworthiness limitations and maintenance instructions to ensure continued safe operation of these engines.

Jun 21, 2024
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg TRENT XWBAirbus A350

EASA AD CF-2024-24

SUPERSEDED BY TCCA AD CF-2025-38

Canadian Airworthiness Directive CF-2024-24 addresses missing or loose bolts in the anti-yaw mounting block of the horizontal stabilizer on Mitsubishi Heavy Industries RJ Aviation ULC aircraft, specifically models CL-600-2C10, CL-600-2C11, CL-600-2D15, CL-600-2D24, and CL-600-2E25 within certain serial number ranges. The directive mandates inspections and eventual replacement of these bolts to ensure structural integrity and flight safety.

Jun 21, 2024
Airworthiness DirectiveMaintenanceSafety MgmtMHI RJ Aviation CL-600 (Regional Jet)Mitsubishi Heavy Industries RJ Aviation ULC CL-600-2C10Mitsubishi Heavy Industries RJ Aviation ULC CL-600-2C11Mitsubishi Heavy Industries RJ Aviation ULC CL-600-2D15Mitsubishi Heavy Industries RJ Aviation ULC CL-600-2D24Mitsubishi Heavy Industries RJ Aviation ULC CL-600-2E25

EASA AD 2024-0114

Time Limits / Maintenance Checks — Airworthiness Limitations Section — Amendment

EASA Airworthiness Directive 2024-0114 is an amendment concerning the ARRIUS 2G1 engines manufactured by SAFRAN Helicopter Engines, commonly installed on KAMOV 226T helicopters. This directive mandates compliance with updated airworthiness limitations and maintenance tasks as specified in the latest Airworthiness Limitations Section of the SAFRAN Arrius 2G1 Maintenance Manual. It ensures continued airworthiness by enforcing replacement of life-limited parts and adherence to revised maintenance intervals.

Jun 21, 2024
Airworthiness DirectiveMaintenanceSafety MgmtSafran ARRIUS 2Kamov 226T

EASA AD US-2024-11-03

Engine - 1st-Stage Hubs and 2nd-Stage Hubs - Inspection / Replacement

The Federal Aviation Administration's Airworthiness Directive 2024-11-03 addresses certain International Aero Engines, AG Model V2500 engines installed on aircraft such as the Airbus A320neo and A321-231. This directive requires angled ultrasonic inspections and accelerated replacement of specific high-pressure turbine 1st-stage and 2nd-stage hubs due to a risk of failure caused by a nickel powdered metal anomaly. The AD aims to prevent unsafe conditions resulting from hub failures that could lead to engine shutdowns or uncontained engine debris.

Jun 20, 2024
Airworthiness DirectiveMaintenanceSafety MgmtInternational Aero Engines Ag V2500-( )5Airbus A320neoAirbus A321-231

EASA AD CF-2024-23

Fire Protection — Fire Extinguisher — Defective Cargo Fire Extinguisher Bottles

Canadian Airworthiness Directive CF-2024-23 addresses defective cargo fire extinguisher bottles on Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11 aircraft. The directive targets specific Low Rate Discharge (LRD) bottles with part numbers 475086-1, 475124-1, and 475087-1 that may have a manufacturing defect causing loss of extinguishing agent. This AD mandates inspection, replacement, and installation restrictions to ensure fire protection system reliability.

Jun 20, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus BD-500 (A220 Series)Airbus Canada BD-500-1A10Airbus Canada BD-500-1A11

EASA AD US-2024-10-05

Equipment / Furnishings - Decompression Panels and Pressure Equalization Valves in the Forward and Aft Lower Lobe Cargo Compartments - Inspections / Replacement / Installation

The Federal Aviation Administration's Airworthiness Directive 2024-10-05 addresses certain Boeing Company Model 757 airplanes. It mandates inspections and corrective actions for decompression panels and pressure equalization valves in the forward and aft lower lobe cargo compartments to prevent damage that could compromise cargo fire protection and airplane structural integrity.

Jun 18, 2024
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 757

EASA AD US-2024-10-07

Fuselage - Fuselage Skin Door Cutout - Inspection / Maintenance Records Check

Fuselage - Fuselage Skin Door Cutout - Inspection / Maintenance Records Check is a final rule airworthiness directive issued by the FAA affecting all Boeing Company Model 757 airplanes. It addresses potential cracks in hidden areas beneath scuff plates in the fuselage skin and bear strap of certain doors, including passenger entry, crew entry, cargo doors, and main deck cargo doors on cargo-modified aircraft.

Jun 18, 2024
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 757

EASA AD 2024-0074-CN

CANCELLED: SUSPENSION OF FLIGHT OPERATIONS

EASA Airworthiness Directive Cancellation Notice 2024-0074-CN cancels the previous Emergency AD 2024-0074-E which suspended flight operations of Blackshape S.p.A. BS 115 aeroplanes, including BK 160, BK 160-200, and BK 160TR models. The cancellation follows new data indicating that the second accident involving a BS 115 aeroplane may have resulted from operation beyond certified limits rather than a structural failure. This notice removes the suspension on all BS 115 flight operations.

Jun 13, 2024
Airworthiness DirectiveFlight OpsSafety MgmtBlackshape BS 115

EASA AD 2024-0113

Tail Rotor — Tail Rotor Hub Tension-Torsion Bars — Inspection

EASA Airworthiness Directive 2024-0113 is an airworthiness directive addressing Airbus Helicopters EC 130 B4 and EC 130 T2 models. It mandates inspection of the tail rotor hub tension-torsion bars, specifically parts with P/N 350A33318000 or P/N 350A33318001, due to a reported failure that could lead to loss of tail rotor function. The directive includes inspection procedures and corrective actions to ensure continued safe operation.

Jun 13, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters AS 350Airbus Helicopters EC 130Airbus Helicopters EC 130 B4Airbus Helicopters EC 130 T2

EASA AD 2023-0048-CN

CANCELLED: Wings — Main Wing Spar; Placards and Markings — Interior Placards — Installation; Aircraft Flight Manual / Operational Limitations — Amendment

EASA Airworthiness Directive Cancellation Notice 2023-0048-CN cancels the previous Emergency AD 2023-0048-E concerning the main wing spars, interior placards, and aircraft flight manual amendments for CEAPR DR 400 series aeroplanes. This cancellation applies to all serial numbers of the DR 400 variants and addresses the previously identified potential structural issue with main wing spars. The notice confirms that the bonding of the affected main wing spars is now considered acceptable and no longer poses an unsafe condition.

Jun 12, 2024
Airworthiness DirectiveMaintenanceSafety MgmtCeapr DR 400