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EASA Regulations & Airworthiness Directives

Browse 4985 EASA regulations with AI-powered summaries.

Aircraft:AllAirbus A320279Airbus A321275Airbus A319246Airbus A350213Airbus A330209All193Airbus A318185Airbus A380171Boeing 737170Airbus A340140Airbus A350-941124Airbus BD-500 (A220 Series)116Airbus Helicopters AS 332115Airbus Helicopters EC 225112Airbus Helicopters SA 330112Show all...

EASA AD 2025-0020R1

Engine — Combustion Rear Inner Case Bolt — Replacement / Modification

EASA Airworthiness Directive 2025-0020R1 is an updated directive addressing the replacement and modification of combustion rear inner case (CRIC) bolts, Part Number FW82729, on Rolls-Royce RB211 Trent 900 series engines. These engines are commonly installed on Airbus A380 aircraft. The directive mandates repetitive replacement of affected bolts during qualified shop visits and requires a modification of the engine to install an improved CRIC assembly to prevent bolt fractures.

Jan 22, 2025
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg RB211 TRENT 900

EASA AD 2025-0023-E

Flight Controls - Flaperon Bellcrank Bolt - Inspection

EASA Airworthiness Directive 2025-0023-E is an emergency directive addressing the inspection and corrective actions for the flaperon bellcrank bolt on Pipistrel Vertical Solutions Virus SW 121, SW 121A, SW 121C, and Virus SW 128 aeroplanes. The directive mandates inspection and modification procedures to ensure the secure installation of the flaperon bellcrank bolt to prevent control stick malfunctions. This AD applies to all serial numbers listed in the relevant Pipistrel service bulletins.

Jan 22, 2025
Airworthiness DirectiveMaintenanceSafety MgmtPipistrel Vertical Solutions D.O.O. Virus SW

EASA AD GA8-12

Powerplant Instrumentation and Limitations - Maintenance and Operational Manual - Amendment

The Powerplant Instrumentation and Limitations - Maintenance and Operational Manual - Amendment is an Airworthiness Directive issued by the Civil Aviation Safety Authority of Australia affecting all GippsAero GA8 series aeroplanes listed in the relevant service bulletin. It addresses discrepancies in engine performance data related to take-off charts and engine RPM limits. This directive mandates updates to maintenance and operational manuals to ensure compliance with corrected engine limitations.

Jan 22, 2025
Airworthiness DirectiveMaintenanceFlight OpsGa8 Airvan Pty Ltd (Gippsaero) GA8

EASA AD 2025-0024

SUPERSEDED BY EASA AD 2025-0080

EASA Airworthiness Directive 2025-0024 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting ATR 42 and ATR 72 aeroplanes. It addresses a potential unsafe condition related to the aft cargo compartment fire extinguisher distribution piping, specifically a disconnected fire extinguishing tube found during final assembly inspections. The directive applies to various ATR 42 and ATR 72 models with specific modification and serial number applicability.

Jan 22, 2025
Airworthiness DirectiveMaintenanceSafety MgmtATR ATR42ATR ATR72

EASA AD 2025-0021R1

SUPERSEDED BY EASA AD 2025-0266

EASA Airworthiness Directive 2025-0021R1 is an updated directive addressing the inspection and maintenance of Rolls-Royce Trent 7000-72 and Trent 7000-72C engines, primarily installed on Airbus A330 (NEO) aircraft. It mandates on-wing borescope inspections of high pressure turbine (HPT) blades with part number KH64485 to detect axial cracking and requires corrective actions including engine removal and blade replacement if cracks exceed specified limits. The directive also introduces a life limit for affected HPT blades and excludes engines modified with mod 72-K336 from these requirements.

Jan 22, 2025
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg TRENT 7000

EASA AD 2025-0022

Engine Fuel & Control — Fuel Control System — Additive Application

EASA Airworthiness Directive 2025-0022 is an official safety directive addressing the fuel control system of GE Aviation Czech M601, H75, H80, and H85 series engines. These engines are commonly installed on aircraft such as the Aircraft Industries L-410 and L-420, Air Tractor AT series, Allied Ag Cat G-164, Thrush Aircraft 510G and S-2R, Viking Air DHC-3 Otter, Zlin Z-37T, and PAC FU-24. The directive mandates the periodic application of a lubricity improver additive to the fuel control unit to prevent fuel deposit-related malfunctions.

Jan 21, 2025
Airworthiness DirectiveMaintenanceSafety MgmtGe Aviation Czech H75, H80, H85Ge Aviation Czech M601

EASA AD BR-2025-01-01

Computerized Aeroplane Flight Manual Takeoff Calculation Module - Revision

Brazilian Airworthiness Directive AD No. 2025-01-01 is a regulatory document issued by the Agência Nacional de Aviação Civil (ANAC) that applies to Embraer ERJ 190-300 and ERJ 190-400 airplane models. It addresses an inconsistency in the Computerized Airplane Flight Manual (CAFM) Takeoff Calculation Module affecting these aircraft. The directive mandates updates to the Airplane Flight Manual to ensure accurate takeoff performance calculations.

Jan 20, 2025
Airworthiness DirectiveFlight OpsSafety MgmtEmbraer ERJ 190

EASA SIB BEA-2024-07R1

Landing Gear - Shock Absorber Servicing

BEA 2024-07R1 is a Special Airworthiness Bulletin issued to inform the civil aviation community about best practices for servicing the Main Landing Gear (MLG) shock absorbers on EMBRAER S.A. EMB-545 and EMB-550 aircraft. The bulletin highlights issues related to improper servicing that can affect landing gear operation and aircraft control laws. It provides recommendations to ensure correct servicing procedures are followed to maintain safe aircraft operation.

Jan 20, 2025
Safety Information BulletinMaintenanceSafety MgmtEmbraer EMB-545Embraer EMB-550

EASA AD CF-2025-04

SUPERSEDED BY TCCA AD CF-2025-45

The Canadian Airworthiness Directive CF-2025-04 is a regulatory document addressing electrical wiring issues in the toilet A maintenance panel of Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11 aircraft models. It mandates inspections and corrective actions to ensure proper securing and clearance of electrical harnesses near oxygen supply lines to prevent potential fire hazards.

Jan 20, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus BD-500 (A220 Series)

EASA AD 2024-0242R1

Flight Controls — Horizontal Tailplane Drive Lower Bearing — Modification

EASA Airworthiness Directive 2024-0242R1 is a regulatory document addressing the horizontal tailplane drive lower bearing on Standard Cirrus sailplanes manufactured by SCHEMPP-HIRTH Flugzeugbau GmbH. It applies specifically to Standard Cirrus sailplanes with certain serial numbers and mandates inspection and possible replacement of affected lower ball bearings to ensure continued airworthiness.

Jan 17, 2025
Airworthiness DirectiveMaintenanceSafety MgmtSchempp Hirth Flugzeugbau Standard Cirrus

EASA AD 2025-0017R1

Fuselage — Tail Rotor Pylon — Inspection

EASA Airworthiness Directive 2025-0017R1 is an updated safety directive addressing inspection requirements for the tail rotor pylon fuselage on Airbus Helicopters EC 175 B models. It mandates repetitive visual inspections to detect loose rivets and cracks that could compromise the structural integrity of the tail rotor pylon. The directive applies to all serial numbers of the EC 175 B helicopter and provides guidance on corrective repairs if discrepancies are found.

Jan 17, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters EC175

EASA SIB SAIB-2025-01

Hydraulic Power System - Fatigue Failure of Hydraulic Flexible Hoses

The Special Airworthiness Information Bulletin (SAIB) 2025-01 issued by the FAA addresses fatigue failure of hydraulic flexible hoses in the wheel wells of the main and nose landing gear on Boeing 757 series airplanes. The bulletin provides information on the issue and recommends maintenance actions to prevent loss of the left hydraulic system. This SAIB is informational and does not mandate regulatory action under 14 CFR part 39.

Jan 17, 2025
Safety Information BulletinMaintenanceSafety MgmtBoeing 757

EASA AD 2025-0019-E

Engine / Electrical Power — Internal Generator — Inspection / Replacement of Oil Spray Nozzle

EASA Airworthiness Directive 2025-0019-E is an emergency directive addressing BRP-Rotax 912i, 915i, and 916i series engines installed on various general aviation aeroplanes and powered sailplanes. It mandates inspection and possible replacement of the oil spray nozzle assembly, Part Number 456540, and generator stator assemblies to prevent potential engine failures. The directive applies to all serial numbers of the affected engines and aims to ensure continued airworthiness and safety.

Jan 16, 2025
Airworthiness DirectiveMaintenanceSafety MgmtBrp-Rotax Gmbh & Co Kg 912 iScBrp-Rotax Gmbh & Co Kg 915Brp-Rotax Gmbh & Co Kg 916 iSc

EASA AD ISR-I-32-25-01-7

Nose Landing Gear Actuator to Strut Attachment Pin - Inspection / Replacement

Airworthiness Directive AD ISR I-32-25-01-7 issued by the Civil Aviation Authority of Israel mandates inspection and replacement of the nose landing gear actuator to strut attachment pin on all G100, ASTRA SPX, and ASTRA model aircraft. This directive addresses a safety concern related to the failure of this specific attachment pin. It requires operators to update their Aircraft Maintenance Manuals (AMM) to include pin life limits.

Jan 16, 2025
Airworthiness DirectiveMaintenanceSafety MgmtGulfstream (Galp) ASTRAGulfstream (Galp) G100

EASA AD CF-2025-03

Indicating / Recording Systems — Unsecured Maintenance Ports

The Canadian Airworthiness Directive CF-2025-03 addresses unsecured maintenance ports on Bombardier Inc. model BD-700-1A10 and BD-700-1A11 aircraft, including Global 5000, Global 5500, Global 6000, and Global 6500 variants. This directive mandates the installation of locking features on network interfaces to prevent unauthorized physical access. It applies to specific serial numbers as identified in Bombardier Service Bulletins.

Jan 15, 2025
Airworthiness DirectiveMaintenanceSafety MgmtBombardier BD-700

EASA AD CF-2025-02

Oxygen — Therapeutic Oxygen Hoses — Inadequate clearance from Electrical Harness

Airworthiness Directive CF-2025-02 addresses inadequate clearance between therapeutic oxygen hoses and electrical harnesses on Bombardier Inc. model BD-700-1A10 aeroplanes. This directive mandates inspections and corrective actions to prevent potential damage that could impair the firewall hydraulic shutoff valve. The affected aircraft include various serial numbers of the BD-700-1A10 Global Express, Global XRS, Global 6000, and Global 6500 models.

Jan 15, 2025
Airworthiness DirectiveMaintenanceSafety MgmtBombardier BD-700

EASA AD CF-2025-01

Time Limits/Maintenance Checks (TLMC) — Mid-Life - Airworthiness Limitations (AWL)

The Airworthiness Directive CF-2025-01 issued by Transport Canada mandates updated time limits and maintenance checks for Bombardier BD-700-1A10 and BD-700-1A11 aircraft models, including Global Express, Global Express XRS, Global 6000, Global 5000, and Global 5000 featuring GVFD. This directive addresses mid-life airworthiness limitations as specified in the updated TLMC manual revisions. It ensures continued airworthiness by enforcing compliance with revised inspection intervals and maintenance tasks.

Jan 15, 2025
Airworthiness DirectiveMaintenanceSafety MgmtBombardier BD-700

EASA AD US-2024-25-07

Engine - Stages 6-10 Compressor Rotor Spools - Inspection

The document titled 'Engine - Stages 6-10 Compressor Rotor Spools - Inspection' is a regulatory directive concerning the inspection requirements for compressor rotor spools in engine stages 6 through 10. It addresses specific inspection protocols to ensure the integrity and safety of these engine components. The directive is relevant to aviation professionals involved in engine maintenance and airworthiness compliance.

Jan 14, 2025
Airworthiness DirectiveMaintenanceSafety MgmtGeneral Electric GEnx

EASA AD 2025-0018

SUPERSEDED BY EASA AD 2025-0040

EASA Airworthiness Directive 2025-0018 is issued for Airbus Helicopters H160-B models concerning the inspection of rotating scissors spherical bearings, part number U623A40T1007. This directive mandates repetitive inspections to detect excessive axial play in these bearings to ensure continued safe operation. It applies to all serial numbers of the H160-B helicopter and provides detailed inspection intervals and corrective actions.

Jan 14, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters H160

EASA AD 2019-0207R2

Doors — Passenger / Crew Door Girt Bar Fitting Assemblies - Inspection

EASA Airworthiness Directive 2019-0207R2 is an updated safety directive addressing inspection requirements for the passenger and crew door girt bar fitting assemblies on Airbus A350-941 and A350-1041 aeroplanes, excluding those with Airbus modification 115327. The directive mandates repetitive detailed inspections of affected girt bar fitting assemblies with part numbers V5217170000000 or V5217170000100 to detect potential safety hook jamming issues. It aims to prevent possible failure of passenger door slide deployment during emergencies.

Jan 13, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A350