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EASA Regulations & Airworthiness Directives

Browse 4771 EASA regulations with AI-powered summaries.

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EASA AD CF-2024-34R1

Electrical Power — Variable Frequency Generator Power-Feeder Harness Chafing Against Wheel Bins and Main Landing Gear

The Electrical Power — Variable Frequency Generator Power-Feeder Harness Chafing Against Wheel Bins and Main Landing Gear is an Emergency Airworthiness Directive CF-2024-34R1 issued by Transport Canada. It applies to Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11 aircraft, addressing chafing issues of the Variable Frequency Generator (VFG) power-feeder harnesses against wheel bins and main landing gear. The directive mandates inspections, repairs, and modifications to prevent damage that could lead to generator failures and critical system losses.

Oct 16, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus BD-500 (A220 Series)Airbus Canada BD-500-1A10Airbus Canada BD-500-1A11

EASA AD ISR-I-32-24-10-01R1

Nose Landing Gear Actuator to Strut Attachment Pin Inspection / Life Limit AMM Revision

Airworthiness Directive AD ISR I-32-24-10-01R1 issued by the Civil Aviation Authority of Israel addresses the inspection and life limit revision for the nose landing gear actuator to strut attachment pin on all Gulfstream G150 model aircraft. This directive mandates updates to the Aircraft Maintenance Manual (AMM) to include a life limit for the affected pin part number 2247-0500-008. The directive aims to enhance safety by preventing failures related to this critical landing gear component.

Oct 16, 2024
Airworthiness DirectiveMaintenanceSafety MgmtGulfstream (Galp) G150Gulfstream G150

EASA AD BR-2020-04-01R3

Windows - Cockpit Side Windows - Inspection / Replacement

Brazilian Airworthiness Directive AD No. 2020-04-01R03 is issued by the Agência Nacional de Aviação Civil (ANAC) and applies to Embraer S.A. EMB-545 and EMB-550 airplanes equipped with specific cockpit side window part numbers. The directive mandates inspection and replacement of cockpit side windows to address safety concerns related to cracks, delamination, and potential window failure. It requires compliance with detailed inspection procedures and replacement with modified windows bearing new part numbers.

Oct 16, 2024
Airworthiness DirectiveMaintenanceSafety MgmtEmbraer EMB-545Embraer EMB-550

EASA AD 2024-0194

Engine — Centrifugal Compressor Case — Inspections

EASA Airworthiness Directive 2024-0194 is an airworthiness directive addressing inspections of the centrifugal compressor case on GE Aviation Czech M601 series engines. It applies to M601D, M601E, M601E-11, M601E-11A, M601E-11AS, M601E-11S, M601E-21, M601F, and M601FS engines installed on various aircraft including the Aircraft Industries L-410 series, Air Tractor AT series, Allied Ag Cat G-164 series, PZL-106 Kruk, Do 28 series, Thrush S-2R series, Viking DHC-3 Otter, Zlin Z 37 T and Z 137 T, and Pacific Aerospace FU-24. The directive mandates repetitive inspections of the affected centrifugal compressor case parts to detect cracks and prevent potential engine separation.

Oct 15, 2024
Airworthiness DirectiveMaintenanceSafety MgmtGe Aviation Czech M601Aircraft Industries L-410Air Tractor ATAllied Ag Cat G-164PZL-106 KrukDornier Do 28Thrush S-2RViking DHC-3 OtterZlin Z 37 TZlin Z 137 TPacific Aerospace FU-24

EASA AD US-2024-20-02

Fuselage - Aft Fuselage Cant Bulkhead at Certain Stations and Vertical Stabilizer Rear Spar Structure - Inspection

The document titled 'Fuselage - Aft Fuselage Cant Bulkhead at Certain Stations and Vertical Stabilizer Rear Spar Structure - Inspection' is a regulatory inspection directive concerning specific structural components of an aircraft's aft fuselage and vertical stabilizer. It addresses the need for inspection of the aft fuselage cant bulkhead at designated stations and the vertical stabilizer rear spar structure to ensure structural integrity and airworthiness. The directive applies to affected aircraft models as specified within the full regulatory text.

Oct 15, 2024
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 717Boeing DC-9

EASA AD BR-1999-02-01R7

Aileron PCA Rod Ends and Fittings - Inspections

Brazilian Airworthiness Directive AD No. 1999-02-01R7 issued by ANAC addresses inspection and reinforcement requirements for aileron PCA rod ends and fittings on Embraer S.A. EMB-145 aircraft models, excluding EMB-135 models. The directive mandates repetitive visual inspections and installation of new reinforced parts to ensure structural integrity and flight safety. It includes specific part numbers for affected PCAs and fittings and references Embraer Service Bulletins for compliance procedures.

Oct 14, 2024
Airworthiness DirectiveMaintenanceSafety MgmtEmbraer EMB-145

EASA AD US-2024-15-09

Flight Controls - Tamarack Active Technology Load Alleviation System (ATLAS) Winglets - Placard Installation / AFM Revision

The Flight Controls - Tamarack Active Technology Load Alleviation System (ATLAS) Winglets - Placard Installation / AFM Revision is a regulatory document addressing the installation of placards and revisions to the Aircraft Flight Manual (AFM) related to Tamarack ATLAS winglets. It applies to aircraft equipped with these winglets to ensure proper operational awareness and compliance with updated flight control requirements.

Oct 14, 2024
Airworthiness DirectiveFlight OpsMaintenanceSafety MgmtTextron Aviation 525 (CitationJet)

EASA AD US-2024-19-14

Fuel - Lightning Protection for the Engine Fuel Feed System - Inspections

The document titled 'Fuel - Lightning Protection for the Engine Fuel Feed System - Inspections' is a regulatory directive focused on ensuring the safety and integrity of the engine fuel feed system against lightning strikes. It addresses inspection requirements to verify the effectiveness of lightning protection measures. The document does not specify particular aircraft types or engine models.

Oct 14, 2024
Safety DirectiveMaintenanceSafety MgmtBoeing 777

EASA AD US-2024-16-09

Fuselage - Underwing Longeron (UWL) - Inspections

The document titled "Fuselage - Underwing Longeron (UWL) - Inspections" is a regulatory directive concerning the inspection requirements for the underwing longeron structure of aircraft fuselages. It aims to ensure the structural integrity and airworthiness of affected aircraft by mandating specific inspection procedures. The document does not explicitly mention particular aircraft models, engine types, or part numbers.

Oct 14, 2024
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 777

EASA AD 2024-0190

[Correction] Aircraft Flight Manual — Normal Procedures — Amendment

[Correction] Aircraft Flight Manual — Normal Procedures — Amendment is a regulatory document addressing updates to the flight manual procedures for Airbus S.A.S. aircraft models A350 and A380. This amendment corrects previously issued information to ensure accurate and safe operational guidance for these specific aircraft types. The document focuses on normal procedures relevant to flight crews operating the Airbus A350 and A380.

Oct 11, 2024
CRDFlight OpsSafety MgmtAirbus A350Airbus A380

EASA AD 2024-0193

Fire Protection — Engine Fire Extinguisher Bottle Connections — Inspection

EASA Airworthiness Directive 2024-0193 is an airworthiness directive addressing the inspection of engine fire extinguisher bottle connections on Leonardo S.p.A. A109 series helicopters, including A109E, A109LUH, A109S, and AW109SP models. The directive mandates inspection of motor cables and bonding braids related to the engine fire extinguishing system to ensure correct installation and functionality.

Oct 11, 2024
Airworthiness DirectiveMaintenanceSafety MgmtLeonardo S.P.A. Helicopters A109Leonardo S.P.A. Helicopters A119Leonardo A109Leonardo AW109

EASA AD 2024-0192

Landing Gear — Main Landing Gear Piston — Inspection

EASA Airworthiness Directive 2024-0192 is issued for Fokker F28 Mark 0070 and Mark 0100 aeroplanes equipped with Collins Aerospace main landing gear pistons having part numbers 41050-7 to -16 or 41060-3 to -6, except those already modified by Fokker Services Service Bulletin SBF100-32-172. This directive mandates inspections of the main landing gear piston, specifically targeting pistons modified by Aerospace NDI Pty Ltd with part number 41141-5, to detect cracks caused by stress corrosion. The directive aims to prevent structural failure and potential collapse of the main landing gear during operation.

Oct 10, 2024
Airworthiness DirectiveMaintenanceSafety MgmtFokker F28Fokker F28 Mark 0070Fokker F28 Mark 0100

EASA AD 2024-0191

Wings — Wing Front and Rear Spars — Inspection

EASA Airworthiness Directive 2024-0191 is an airworthiness directive addressing inspection requirements for the wing front and rear spars of Airbus A380-841, A380-842, and A380-861 aeroplanes. It mandates special detailed inspections of specific wing spar areas to detect cracks that could compromise structural integrity. This directive applies to all manufacturer serial numbers of these Airbus A380 models.

Oct 10, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380Airbus A380-841Airbus A380-842Airbus A380-861

EASA AD 2024-0182R1

SUPERSEDED BY EASA AD 2025-0128

EASA Airworthiness Directive 2024-0182R1 is a regulatory update addressing inspection and maintenance requirements for Rolls-Royce Trent XWB series engines, specifically models Trent XWB-75, -79, -79B, -84, and -97, installed on Airbus A350 aircraft. The directive focuses on inspecting and replacing certain main fuel hose assemblies identified by specific part numbers to prevent potential engine fires. It mandates repetitive inspections and corrective actions to ensure continued airworthiness of affected engines.

Oct 9, 2024
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg TRENT XWBAirbus A350

EASA SIB SAFO24006

Potential for Jammed or Restricted Rudder on Boeing Model 737 Series Airplanes Equipped with Optional Collins Aerospace SVO-730 Rudder Rollout Guidance Actuators (RRGA).

The Safety Alert for Operators SAFO 24006 notifies operators of Boeing 737 series airplanes, including the 737-600/-700/-800/-900/-900ER (737NG) and 737-8/-8200/-9 (737 MAX) models, equipped with optional Collins Aerospace SVO-730 Rudder Rollout Guidance Actuators (RRGA) about the potential for jammed or restricted rudder movement. This condition may occur due to moisture freezing inside the actuator, which can limit rudder control during flight or landing rollout. The alert provides important safety information and recommended procedures to address this issue.

Oct 8, 2024
Safety Information BulletinFlight OpsMaintenanceSafety MgmtBoeing 737

EASA AD US-2024-15-07

Fuel - Nitrogen Enriched Air Distribution System (NEADS) Cover Plate Assembly - Installation / Revision of Maintenance and Inspection Program

The Fuel - Nitrogen Enriched Air Distribution System (NEADS) Cover Plate Assembly - Installation / Revision of Maintenance and Inspection Program is a regulatory document addressing the installation and maintenance requirements for the NEADS cover plate assembly. It applies to aircraft equipped with this specific fuel system component, ensuring proper inspection and upkeep to maintain airworthiness and safety standards.

Oct 2, 2024
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 777

EASA AD 2024-0189

Time Limits / Maintenance Checks — Airworthiness Limitations Section Part 1 — Safe Life Airworthiness Limitations Items — Amendment

EASA Airworthiness Directive 2024-0189 is an amendment addressing the Safe Life Airworthiness Limitations Items for Airbus A350-941 and A350-1041 aeroplanes. It updates the Airbus A350 Airworthiness Limitations Section Part 1 to Revision 08, Issue 2, ensuring mandatory compliance with new and more restrictive maintenance limits. This directive applies to all manufacturer serial numbers of the affected Airbus A350 models.

Oct 1, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A350Airbus A350-941Airbus A350-1041

EASA AD US-2024-19-17

Rotors Flight Control - Tension Torsion (TT) Straps - Removal / Installation Prohibition

The document titled 'Rotors Flight Control - Tension Torsion (TT) Straps - Removal / Installation Prohibition' is a regulatory directive addressing the handling of tension torsion straps in rotor flight control systems. It applies to specific rotorcraft models equipped with these components, prohibiting their removal or installation to ensure flight safety and structural integrity.

Sep 30, 2024
Safety DirectiveMaintenanceSafety MgmtBell Textron Inc. (Bti) 204BBell Textron Inc. (Bti) 205Bell Textron Inc. (Bti) 210Bell Textron Inc. (Bti) 212

EASA CZIB 2024-01 R7

Airspace of Lebanon

The document titled Airspace of Lebanon is a safety information bulletin issued by EASA concerning the airspace over Lebanon, specifically the Beirut FIR (OLBB). It highlights ongoing high risks due to regional tensions and recent Israeli airstrikes near Beirut International Airport, affecting all flight levels in Lebanese airspace. The bulletin applies to air operators subject to EU Regulation 965/2012 and third country operators authorized by EASA under TCO authorizations.

Sep 28, 2024
Safety Information BulletinFlight OpsSafety Mgmt