EASA Regulations & Airworthiness Directives

Browse 5,156 EASA regulations with AI-powered summaries.

Aircraft:All Airbus A320286 Airbus A321285 Airbus A319253 Airbus A350222 Airbus A330220 Airbus A318189 Airbus A380182 Boeing 737175 Airbus A340141 Airbus A350-941132 Airbus BD-500 (A220 Series)123 Airbus Helicopters AS 332119 Airbus Helicopters EC 225116 Airbus Helicopters SA 330116 Boeing 787115 Show all...

EASA AD 2025-0094

Apr 24, 2025

Electrical Power — Overhead Panel Wires Interference — Inspection / Modification

EASA Airworthiness Directive 2025-0094 is an official regulatory document addressing electrical power system safety on Leonardo S.p.A. AB139 and AW139 helicopters. It mandates inspections and modifications to the overhead panel wiring to prevent interference between cables and connectors that could lead to cable damage, fire, and loss of helicopter control. The directive applies to all serial numbers of these helicopter models.

Airworthiness DirectiveSuperseded

Leonardo S.P.A. Helicopters AB139
Leonardo S.P.A. Helicopters AW139

EASA AD 2025-0093

Apr 24, 2025

Landing Gear — Nose Landing Gear Shock Absorber — Functional Check

EASA Airworthiness Directive 2025-0093 is an airworthiness directive affecting Airbus A350-941 and A350-1041 aeroplanes. It mandates functional checks of the nose landing gear (NLG) shock absorber sliding piston assemblies with specific part numbers to address potential mechanical noise and corrosion issues. The directive applies to certain NLG piston assemblies identified by part numbers 6407A2000-01, 6407A2000-02, 6407A2000-03, 5035A3200-01, and 5035A3200-02.

Airworthiness Directive

Airbus A350

EASA AD 2025-0080

Apr 23, 2025

[Correction] Fire Protection — Aft Cargo Compartment Fire Extinguisher Distribution Piping — Functional Check

[Correction] Fire Protection — Aft Cargo Compartment Fire Extinguisher Distribution Piping — Functional Check is a regulatory document addressing fire protection systems on ATR ATR42 and ATR72 aircraft. It focuses on the functional check of the aft cargo compartment fire extinguisher distribution piping to ensure proper operation and safety compliance. This correction clarifies or updates previous instructions related to these specific aircraft models.

Correction

ATR ATR42
ATR ATR72

EASA AD 2025-0092

Apr 23, 2025

Flight Controls — Maintenance and Avionics Interface Computer Software — Modification / Airplane Flight Manual — Amendment

EASA Airworthiness Directive 2025-0092 is an airworthiness directive affecting Dassault Aviation Falcon 7X aeroplanes that have embodied modification M1000, also known as Falcon 8X. This directive mandates modifications to the flight controls maintenance and avionics interface computer software, along with amendments to the Airplane Flight Manual. The directive aims to enhance safety by addressing issues related to the inboard slats extension system during landing.

Airworthiness Directive

Dassault Falcon 7X

EASA AD CF-2025-20

Apr 23, 2025

Pneumatic — Engine Bleed Pressure Regulating Shutoff Valve (PRSOV) Failure

Canadian Airworthiness Directive CF-2025-20 addresses failures of the Pneumatic Engine Bleed Pressure Regulating Shutoff Valve (PRSOV) on Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11 aircraft. The directive targets serial numbers 50001 through 50072 for BD-500-1A10 and 55001 through 55271 for BD-500-1A11. It mandates revisions to the Airplane Flight Manual and replacement of the PRSOV with a redesigned part to mitigate risks associated with bleed air leaks.

Airworthiness Directive

Airbus BD-500 (A220 Series)

EASA AD 2025-0091

Apr 23, 2025

Power Plant — Engine Support Frame — Inspections / Modification; Propeller — Propeller Assembly — Balancing; Engine — Fuel and Control — Powerplant Controllers Software — Modification

EASA Airworthiness Directive 2025-0091 is an airworthiness directive addressing DG-1000M powered sailplanes manufactured by DG-Flugzeugbau GmbH. It mandates inspections, repairs, and modifications related to the engine support frame, propeller assembly balancing, and powerplant controller software. The directive aims to ensure continued airworthiness by preventing engine mount structural failures and maintaining proper power transmission to the propeller.

Airworthiness Directive

Dg Aviation Gmbh DG-1000

EASA AD 2025-0090

Apr 23, 2025

Time Limits / Maintenance Checks – Airworthiness Limitations Section – Amendment

EASA Airworthiness Directive 2025-0090 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all Leonardo AW189 helicopters equipped with either General Electric CT7-2E1 or Safran Aneto-1K engines. This directive mandates compliance with updated airworthiness limitations and maintenance tasks as specified in the latest Leonardo AW189 Air Vehicle Maintenance Planning Information documents. It ensures continued airworthiness by enforcing new or more restrictive maintenance requirements.

Airworthiness DirectiveSuperseded

Leonardo S.P.A. Helicopters AW189

EASA AD BR-2025-04-02

Apr 22, 2025

Aircraft Flight Manual - Amendment

The Brazilian Airworthiness Directive AD No. 2025-04-02 is an amendment issued by the Agência Nacional de Aviação Civil (ANAC) that applies to all Embraer S.A. ERJ 190-300 and ERJ 190-400 aircraft. This directive mandates updates to the Aircraft Flight Manual (AFM) procedures related to AVIONICS MAU 1A and MAU 3B failures and requires a software update to the Brake Control Module (BCM).

Airworthiness Directive

Embraer ERJ 190

EASA AD 2025-0087

Apr 16, 2025

Flight Controls — Flap Asymmetry Detection Mechanism — Inspection

EASA Airworthiness Directive 2025-0087 is an airworthiness directive issued by EASA that applies to ATR 42-200, ATR 42-300, and ATR 42-320 aeroplanes of all manufacturer serial numbers. It mandates inspection of the flap asymmetry detection mechanism to ensure continued safe operation of these aircraft. The directive addresses a potential safety issue related to worn splines in the flap asymmetry detector and flap interconnection shaft.

Airworthiness Directive

ATR ATR42

EASA SD SD-2025-01

Apr 16, 2025

Replacement of certain Rockwell Collins SBAS receivers on aeroplanes conducting LPV200 approaches in EGNOS SoL service area

EASA Safety Directive 2025-01 mandates the replacement of certain Rockwell Collins Satellite Based Augmentation Systems (SBAS) receivers installed on various aircraft conducting LPV-200 approaches within the EGNOS Safety of Life service area. Affected aircraft include models from Airbus such as the A318, A319, A320, A321, A330, A350, and A380, as well as Bombardier, Dassault Falcon series, Embraer EMB-550, Gulfstream G150, G280, G200, and others equipped with GPS-4000S, GLU-2100, GLUS-2100, and GLUS-2100A receivers. This directive addresses a safety concern related to the integrity monitoring of GNSS signals used for precision approaches.

Safety Directive

EASA AD 2025-0088

Apr 16, 2025

ROCKWELL COLLINS: Satellite Based Augmentation Systems / Global Positioning System Receiver — Replacement

EASA Airworthiness Directive 2025-0088 addresses the replacement of certain Rockwell Collins Satellite Based Augmentation Systems (SBAS) and Global Positioning System (GPS) receivers, specifically models GPS-4000S, GLU-2100, GLUS-2100, and GLUS-2100A. These receivers are installed on various aircraft including Airbus A318/A319/A320/A321, Airbus Canada BD-500 (A220 series), Airbus Defence and Space CN-235/C-295, among others. The directive mandates replacement of affected parts to ensure compliance with operational performance standards for satellite navigation systems used in aviation.

Airworthiness Directive

EASA AD 2025-0086

Apr 16, 2025

Time Limits / Maintenance Checks — Engine Time Limits Manual — Amendment

EASA Airworthiness Directive 2025-0086 is an amendment addressing time limits and maintenance checks for Rolls-Royce Deutschland BR700-715 engines, specifically models BR700-715A1-30, BR700-715B1-30, and BR700-715C1-30, commonly installed on Boeing 717 aircraft. This directive mandates compliance with the updated BR715 Time Limits Manual Revision 68 to ensure continued airworthiness. It replaces previous emergency directives and updates maintenance requirements for these engines.

Airworthiness Directive

Rolls-Royce Deutschland Ltd & Co Kg BR700-715

EASA SIB InFO-25003

Apr 16, 2025

Use of Liquid Water Equivalent System (LWES)

InFO 25003 is an informational document from the FAA Flight Standards Service reminding pilots and operators about the proper use of the Liquid Water Equivalent System (LWES) when operating in snow and ice conditions. It emphasizes that while LWES can provide precise weather data, pilots should also consider Meteorological Aerodrome Reports (METAR) and visual observations to ensure safe takeoff decisions. This guidance applies broadly to all aircraft operating in freezing contaminant conditions.

Safety Information Bulletin

EASA AD US-2025-05-10

Apr 15, 2025

Principal Structural Elements (PSEs) - Inspection / Revision of Maintenance Program

The Principal Structural Elements (PSEs) - Inspection / Revision of Maintenance Program is a Federal Aviation Administration (FAA) Airworthiness Directive (AD 2025-05-10) that applies to certain Boeing 777-200, -200LR, -300, -300ER, and 777F series airplanes. This final rule updates and supersedes the previous AD 2012-07-06 by requiring revisions to the maintenance program to incorporate new or more restrictive airworthiness limitations aimed at detecting fatigue cracking in principal structural elements. The directive ensures continued structural integrity and safety of the affected Boeing 777 aircraft.

Airworthiness Directive

Boeing 777

EASA AD 2025-0084

Apr 14, 2025

Engine — Propeller Gearbox Module Propeller Shaft — Replacement

The document titled 'Engine — Propeller Gearbox Module Propeller Shaft — Replacement' 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, and therefore no public AD document exists. The document serves as a recommendation for military authorities responsible for aircraft equipped with TP400-D6 engines to issue their own applicable ADs.

Airworthiness Directive

Epi Europrop International Gmbh TP400-D6

EASA AD 2025-0083

Apr 14, 2025

Equipment/Furnishings — Cargo Bulkhead Frame 24A Vertical Members — Inspection

EASA Airworthiness Directive 2025-0083 is an official regulatory document addressing inspection requirements for the cargo bulkhead frame 24A vertical members on Airbus A318, A319, A320, and A321 aeroplanes. It mandates repetitive detailed inspections of the affected cargo bulkhead vertical member upper parts and fittings located behind the 80VU rack to ensure continued airworthiness. The directive applies to all manufacturer serial numbers of the specified Airbus models.

Airworthiness Directive

Airbus A318
Airbus A319
Airbus A320
Airbus A321

EASA AD BR-2025-04-01

Apr 14, 2025

Stabilizers - Horizontal Stabilizer Backlash - Inspection / Replacement

Brazilian Airworthiness Directive AD No. 2025-04-01 issued by the Agência Nacional de Aviação Civil (ANAC) mandates inspection and possible replacement of horizontal stabilizer components on Embraer EMB-505 aircraft. The directive addresses potential invalid horizontal stabilizer backlash test results that could compromise flight safety. It requires compliance with Embraer Service Bulletin 505-27-0034, revision 02, dated December 6, 2024.

Airworthiness Directive

Embraer EMB-505 (Phenom 300)

EASA AD G-2025-0001R1-E

Apr 14, 2025

Superseded by G-2025-0004-E

Civil Aviation Authority Emergency Airworthiness Directive G-2025-0001R1-E addresses safety concerns for hot air balloons equipped with cylinders fitted with Pressure Relief Valve (PRV) adaptor CB8426, including specific models from Cameron Balloons Limited. The directive mandates inspections for cracks in the PRV adaptors to prevent potential uncontrolled leaks of LPG fuel. This directive applies to various cylinder models such as Thunder & Colt Sky Lindstrand V20-100-00/CB8420 and others listed in the document.

Airworthiness DirectiveSuperseded

Cameron Balloons A Type
Cameron Balloons A Type Cloudhopper
Cameron Balloons B Type
Cameron Balloons C Type
Cameron Balloons Cameron Special Shape Hot Air Balloons
Cameron Balloons Gas Balloons
Cameron Balloons Helium-Hot Air Balloons
Cameron Balloons Hot Air Balloons
Cameron Balloons L Type
Cameron Balloons Lindstrand Special Shape Hot Air Balloons
Cameron Balloons S Type
Cameron Balloons Sky Hot Air Balloons
Cameron Balloons X Type

EASA AD 2025-0085

Apr 14, 2025

Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 2, Airworthiness Limitation Items and Safe Life Items – Amendment

EASA Airworthiness Directive 2025-0085 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Fokker F27 Mark 050, Mark 0502, and Mark 0604 aeroplanes. It mandates compliance with updated airworthiness limitations and maintenance tasks as specified in Fokker Services' Airworthiness Limitations Section Part 2, Report SE-622, Issue 16. This directive ensures continued airworthiness by enforcing replacement of life-limited parts and adherence to maintenance intervals.

Airworthiness DirectiveSuperseded

Fokker F27

EASA AD 2025-0082

Apr 11, 2025

Engine — Intermediate Pressure Compressor Rotor 1 Blades — Inspection / Modification

The document titled 'Engine — Intermediate Pressure Compressor Rotor 1 Blades — Inspection / Modification' is an airworthiness directive concerning the Rolls-Royce Deutschland Ltd & Co KG Trent XWB engine. It mandates inspection and potential modification of the intermediate pressure compressor rotor 1 blades to ensure continued engine safety and performance. This directive applies specifically to aircraft powered by the Trent XWB engine model.

Airworthiness Directive

Rolls-Royce Deutschland Ltd & Co Kg TRENT XWB