EASA Regulations & Airworthiness Directives

Browse 220 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 787114Show all...
Filtered by: Airbus A350Clear filter

EASA AD 2025-0120

May 26, 2025

Cabin Systems — Antenna Adapter Plate — Inspection

EASA Airworthiness Directive 2025-0120 is an airworthiness directive addressing inspection requirements for the antenna adapter plate and related parts installed on Airbus A319, A320, A321, A330, A350, and A380 aircraft models. The directive mandates repetitive general visual inspections of affected broadband antenna adapter plates to detect corrosion and cracks that could compromise aircraft safety. It applies to all manufacturer serial numbers of the specified Airbus models.

Airworthiness Directive
  • Airbus A319
  • Airbus A320
  • Airbus A321
  • Airbus A330
  • Airbus A350
  • Airbus A380

EASA AD 2025-0117

May 19, 2025

Fuselage — Bracket Supporting Flap Shaft Catcher — Inspection

EASA Airworthiness Directive 2025-0117 is an airworthiness directive addressing the Airbus A350-1041 aeroplanes with specific manufacturer serial numbers. It mandates inspection of the fuselage bracket supporting the flap shaft catcher to detect incorrect installation that could cause misalignment and potential flap surface detachment. The directive applies to affected left-hand and right-hand side brackets identified by part numbers V5393528020000 and V5393528020100.

Airworthiness Directive
  • Airbus A350

EASA AD 2025-0109

May 16, 2025

Superseded by EASA AD 2025-0117

EASA Airworthiness Directive 2025-0109 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A350-1041 aeroplanes with specific manufacturer serial numbers. The directive mandates inspection of the fuselage bracket supporting the flap shaft catcher to detect incorrect installation that could lead to flap surface detachment. This AD applies to certain left-hand and right-hand side brackets identified by part numbers V5393528020000 and V5393528020100.

Airworthiness DirectiveSuperseded
  • Airbus A350

EASA AD 2025-0105

May 7, 2025

Aircraft Flight Manual — Derated Take-Off/Limitations — Amendment

EASA Airworthiness Directive 2025-0105 is an amendment concerning Airbus A350-941 and A350-1041 aeroplanes. It addresses limitations related to derated take-off operations by requiring updates to the Airbus A350 Airplane Flight Manual (AFM) through specific Temporary Revisions. The directive ensures safe operation by mitigating potential thrust asymmetry issues during critical flight phases.

Airworthiness Directive
  • Airbus A350

EASA AD 2025-0100

Apr 30, 2025

Engine Fuel and Control — Hydro-Mechanical Unit — Replacement / Modification

EASA Airworthiness Directive 2025-0100 is an airworthiness directive affecting Airbus A350-1041 aeroplanes equipped with Rolls-Royce Trent XWB-97 engines. It addresses the replacement and modification of hydro-mechanical units (HMU) with specific part numbers to prevent engine transient N1 shaft speed exceedance caused by worn Combining Spill Valve (CSV) pistons. The directive mandates compliance with Airbus and Rolls-Royce service instructions to ensure continued safe operation.

Airworthiness Directive
  • Airbus A350

EASA AD 2025-0099

Apr 30, 2025

Superseded by EASA AD 2025-0129

EASA Airworthiness Directive 2025-0099 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A350-941 and A350-1041 aeroplanes. It addresses the replacement and maintenance requirements of Flight Control Remote Modules (FCRM) due to hydraulic fluid contamination risks. The directive applies to specific FCRM part numbers and aims to prevent potential loss of control of rudder, elevator, or aileron surfaces.

Airworthiness DirectiveSuperseded
  • Airbus A350

EASA AD 2025-0095

Apr 25, 2025

Superseded by EASA AD 2025-0150

EASA Airworthiness Directive 2025-0095 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A350-941 aeroplanes with specific manufacturer serial numbers. It mandates inspections of the main landing gear brake rod center pin and nut sub-assemblies to detect corrosion and potential detachment risks. The directive aims to ensure continued airworthiness and prevent landing gear extension failures.

Airworthiness DirectiveSuperseded
  • Airbus A350

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 2025-0073

Apr 3, 2025

Stabilizers — Horizontal Tail Plane Lateral Load Fitting Bushings — Inspection

EASA Airworthiness Directive 2025-0073 is an airworthiness directive addressing inspection requirements for the horizontal tail plane lateral load fitting bushings on Airbus A350-941 and A350-1041 aeroplanes, excluding those with Airbus modification 114806. The directive mandates repetitive detailed inspections of affected bushings to detect migration and potential damage. It applies to all manufacturer serial numbers of the specified models and provides instructions for corrective actions and optional modification as terminating action.

Airworthiness Directive
  • Airbus A350

EASA AD 2025-0035

Feb 12, 2025

Superseded by EASA AD 2025-0139

EASA Airworthiness Directive 2025-0035 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A350-941 and A350-1041 aeroplanes, excluding those with Airbus modification 116830 incorporated in production. The directive addresses issues related to hydraulic engine driven pumps and requires a software update to the Hydraulic Monitoring and Control Application (HMCA) to enhance protection against overheating. This directive is effective from 26 February 2025.

Airworthiness DirectiveSuperseded
  • Airbus A350

EASA AD 2019-0207R2

Jan 13, 2025

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.

Airworthiness Directive
  • Airbus A350

EASA AD 2025-0008

Jan 9, 2025

Flight Controls — Flight Control Remote Module — Replacement / Life Limitation

EASA Airworthiness Directive 2025-0008 is an airworthiness directive applicable to Airbus A350-941 and A350-1041 aeroplanes. It addresses the replacement and life limitation of Flight Control Remote Modules (FCRM) with specific part numbers CA71323-013, CA71323-014, CA71323-015, and CA71323-016. The directive mandates compliance with Airbus Service Bulletin A350-27-P066 to ensure continued airworthiness.

Airworthiness Directive
  • Airbus A350

EASA AD 2023-0189R1

Nov 26, 2024

Superseded by EASA AD 2025-0259

EASA Airworthiness Directive 2023-0189R1 is a revision addressing the Airbus A350-941 and A350-1041 aeroplanes equipped with Trent XWB engines. It focuses on the replacement and inspection of the Engine Bleed Air System (EBAS) T-Duct, part number RR03-11011-001, due to a manufacturing quality issue that could lead to cracking and potential engine failure. The directive mandates compliance with Airbus and Rolls-Royce service bulletins to ensure continued airworthiness.

Airworthiness DirectiveSuperseded
  • Airbus A350

EASA AD 2024-0220

Nov 20, 2024

Oxygen — Cabin Oxygen Containers — Inspection

The document titled 'Oxygen — Cabin Oxygen Containers — Inspection' is an AIRBUS S.A.S. directive specifically addressing the inspection requirements for cabin oxygen containers installed on the Airbus A350 aircraft. It outlines necessary procedures to ensure the safety and reliability of oxygen supply systems on this aircraft type. The directive aims to maintain compliance with airworthiness standards for the Airbus A350 fleet.

Safety Directive
  • Airbus A350

EASA AD 2024-0199

Oct 18, 2024

Superseded by EASA AD 2025-0120

EASA Airworthiness Directive 2024-0199 is an update addressing corrosion and cracks found in broadband antenna adapter plates and related parts on Airbus A319, A320, A321, A330, A350, and A380 aircraft models. The directive mandates inspections and corrective actions to ensure the continued airworthiness of these aircraft. It applies to all serial numbers of the affected Airbus models and includes new provisions for the recently certified A321-253NY variant.

Airworthiness DirectiveSuperseded
  • Airbus A319
  • Airbus A320
  • Airbus A321
  • Airbus A330
  • Airbus A350
  • Airbus A380

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 2024-0182R1

Oct 9, 2024

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.

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