EASA Regulations & Airworthiness Directives

Browse 5,158 EASA regulations with AI-powered summaries.

Aircraft:AllAirbus A320286Airbus A321285Airbus A319253Airbus A350222Airbus A330220Airbus A318189Airbus A380182Boeing 737175Airbus A340141Airbus A350-941132Airbus BD-500 (A220 Series)123Airbus Helicopters AS 332119Airbus Helicopters EC 225116Airbus Helicopters SA 330116Boeing 787115Show all...

EASA AD US-2024-15-09

Oct 14, 2024

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.

Airworthiness Directive
  • Textron Aviation 525 (CitationJet)

EASA AD US-2024-19-14

Oct 14, 2024

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.

Safety Directive
  • Boeing 777

EASA AD US-2024-16-09

Oct 14, 2024

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.

Airworthiness Directive
  • Boeing 777

EASA AD 2024-0190

Oct 11, 2024

[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.

CRD
  • Airbus A350
  • Airbus A380

EASA AD 2024-0193

Oct 11, 2024

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.

Airworthiness Directive
  • Leonardo S.P.A. Helicopters A109
  • Leonardo S.P.A. Helicopters A119
  • Leonardo A109
  • Leonardo AW109

EASA AD 2024-0192

Oct 10, 2024

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.

Airworthiness Directive
  • Fokker F28
  • Fokker F28 Mark 0070
  • Fokker F28 Mark 0100

EASA AD 2024-0191

Oct 10, 2024

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.

Airworthiness Directive
  • Airbus A380841842861

EASA AD 2024-0182R1

Oct 9, 2024

Engine – Main Fuel Hose Assembly / Fuel Hoses – Inspection

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.

Airworthiness DirectiveSuperseded
  • Rolls-Royce Deutschland Ltd & Co Kg TRENT XWB
  • Airbus A350

EASA SIB SAFO24006

Oct 8, 2024

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.

Safety Information Bulletin
  • Boeing 737

EASA AD US-2024-15-07

Oct 2, 2024

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.

Airworthiness Directive
  • Boeing 777

EASA AD 2024-0189

Oct 1, 2024

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.

Airworthiness Directive
  • Airbus A3509411041

EASA AD US-2024-19-17

Sep 30, 2024

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.

Safety Directive
  • Bell Textron Inc. (Bti) 204B
  • Bell Textron Inc. (Bti) 205
  • Bell Textron Inc. (Bti) 210
  • Bell Textron Inc. (Bti) 212

EASA CZIB 2024-01 R7

Sep 28, 2024

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.

Safety Information BulletinSuperseded
All aircraft

EASA AD 2024-0188

Sep 27, 2024

Landing Gear – Nose Landing Gear Shock Absorber – Functional Check

EASA Airworthiness Directive 2024-0188 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A350-941 and A350-1041 aeroplanes. It addresses potential mechanical noise and structural issues related to the nose landing gear shock absorber, specifically parts with Part Numbers 6406Axxxx and 4816Axxxx. The directive mandates repetitive functional steering checks to detect and correct increased friction and possible corrosion that could lead to nose landing gear failure.

Airworthiness DirectiveSuperseded
  • Airbus A3509411041

EASA AD US-2024-16-03

Sep 27, 2024

Wings - Fastener Collars inside the Fuel Tanks - Application of Cap Seals

The document titled 'Wings - Fastener Collars inside the Fuel Tanks - Application of Cap Seals' is a regulatory communication addressing the installation of cap seals on fastener collars located inside aircraft fuel tanks. It is intended for aviation maintenance and engineering professionals involved with aircraft fuel system integrity. The document does not specify particular aircraft models or engine types affected.

Safety Information Bulletin
  • Boeing 747

EASA AD 2023-0003R1

Sep 26, 2024

Navigation — EASy Avionics Architecture / Modification; Aircraft Flight Manual — Amendment; Master Minimum Equipment List — Implementation; Operational Suitability Manual — Flight Crew — Implementation

EASA Airworthiness Directive 2023-0003R1 is an updated regulatory document addressing the Falcon 7X aeroplanes equipped with the EASy avionics architecture. It mandates modifications to the aircraft flight manual, implementation of the Master Minimum Equipment List, and updates to the Operational Suitability Manual for flight crews to enhance avionics reliability and safety. The directive applies to all Falcon 7X aircraft except those with certain later avionics modifications embodied in production.

Airworthiness Directive
  • Dassault Falcon 7X

EASA AD 2024-0187

Sep 25, 2024

Doors — Overwing Exit Door Latch Bracket Bushes — Inspection

EASA Airworthiness Directive 2024-0187 is an airworthiness directive addressing inspection requirements for the overwing exit door latch bracket bushes on Airbus A321-251NX, A321-252NX, A321-253NX, A321-271NX, and A321-272NX aeroplanes. The directive mandates repetitive detailed inspections and corrective modifications to prevent potential structural integrity issues caused by bush migration on the latch shaft of the emergency overwing exit door. It applies to specific bracket assembly latch and door assembly overwing part numbers identified by Airbus.

Airworthiness Directive
  • Airbus A321251NX252NX253NX271NX272NX

EASA AD 2024-0181R1

Sep 24, 2024

Flight Controls — Rudder Trim Tab Installation / Threaded Bolts — Replacement

EASA Airworthiness Directive 2024-0181R1 is an updated regulatory requirement addressing the installation and replacement of rudder trim tab threaded bolts on Pilatus PC-24 aeroplanes, specifically those with manufacturer serial numbers 101 and above. The directive mandates replacing affected short rudder-trim control rod assemblies with serviceable parts to prevent potential failure of titanium bolts. This directive applies to the rudder trim tab installation and threaded bolts identified by specific part numbers.

Airworthiness Directive
  • Pilatus Aircraft PC-24
  • Pilatus PC-24

EASA AD 2024-0186

Sep 24, 2024

Oxygen — Crew Oxygen Cylinder Assembly — Inspection / Replacement

EASA Airworthiness Directive 2024-0186 is an airworthiness directive addressing oxygen crew cylinder assemblies on Airbus A350-941 and A350-1041 aeroplanes. It mandates inspection and replacement of specific oxygen cylinder assemblies with part numbers 4441227-058-000 and 4441227-058-001 due to a design defect causing loss of retention of the regulator inlet filter retainer. The directive applies to all manufacturer serial numbers of these aircraft models.

Airworthiness Directive
  • Airbus A3509411041