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EASA Regulations & Airworthiness Directives

Browse 4771 EASA regulations with AI-powered summaries.

Aircraft:AllAirbus A320262Airbus A321257Airbus A319229Airbus A350206Airbus A330197All177Airbus A318172Boeing 737164Airbus A380162Airbus A340136Airbus A350-941119Airbus Helicopters AS 332110Airbus Helicopters EC 225107Airbus Helicopters SA 330107Boeing 787106Show all...

EASA AD 2025-0179

Wings — Sloping Rib and Slat 1 Inboard Seal — Inspection

The document titled Wings — Sloping Rib and Slat 1 Inboard Seal — Inspection is an airworthiness directive applicable to the AIRBUS S.A.S. A330 aircraft. It addresses the inspection requirements for the sloping rib and Slat 1 inboard seal on the wings of these aircraft. The directive aims to ensure the continued airworthiness and safety of the affected aircraft by mandating specific inspection procedures.

Aug 13, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A330

EASA AD US-2025-15-08

Equipment / Furnishings - Flight Crew Seats - Inspection / Check

Airworthiness Directive 2025-15-08 is a final rule issued by the Federal Aviation Administration (FAA) addressing The Boeing Company Model 767-200, -300, -300F, and -400ER series airplanes. It focuses on inspection and checks of the flight crew seats, specifically the Captain's and First Officer's seats, to ensure the horizontal movement system (HMS) functions safely. This directive corrects previous errors related to crediting compliance actions and clarifies inspection requirements.

Aug 11, 2025
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 767

EASA AD 2025-0175

Aircraft Flight Manual — Sections Limitations and Normal Procedures — Amendment Master Minimum Equipment List — Amendment

EASA Airworthiness Directive 2025-0175 is an amendment affecting Airbus A330 and A340 aeroplanes, covering updates to the Aircraft Flight Manual (AFM) sections on limitations and normal procedures, as well as the Master Minimum Equipment List (MMEL). The directive addresses specific models including A330-201 through A330-343 and A340-211 through A340-643, requiring changes related to flight with landing gear down operations and associated system alerts.

Aug 8, 2025
Airworthiness DirectiveFlight OpsMaintenanceSafety MgmtAirbus A330Airbus A340

EASA AD CF-2025-38

Horizontal Stabilizer (H-Stab) — Anti Yaw Steady Fitting Block — Missing or Loose Bolts

Canadian Airworthiness Directive CF-2025-38 addresses missing or loose bolts on the horizontal stabilizer (H-Stab) anti-yaw steady fitting block in MHI RJ Aviation ULC aircraft models CL-600-2C10, CL-600-2C11, CL-600-2D15, CL-600-2D24, and CL-600-2E25 within specified serial number ranges. The directive mandates inspections and torque checks of the fitting block bolts to ensure they are secure until replacement hardware with secondary locking features is installed. This AD aims to prevent potential loss of the horizontal stabilizer due to bolt failure under certain loading conditions.

Aug 8, 2025
Airworthiness DirectiveMaintenanceSafety MgmtMHI RJ Aviation CL-600 (Regional Jet)

EASA AD CF-2025-39

Wings — Oversized Holes in Rib 6

Canadian Airworthiness Directive CF-2025-39 addresses an issue with oversized holes in rib 6 of the wings on Bombardier Inc. model BD-700-2A12 aeroplanes, specifically serial numbers 70042 through 70074, 70079, and 70080. The directive mandates inspection and potential rework of fasteners and fastener holes to ensure structural integrity. This AD aims to prevent fuel leakage and potential structural failure due to cracks in the wing rib shear-ties.

Aug 8, 2025
Airworthiness DirectiveMaintenanceSafety MgmtBombardier BD-700

EASA AD 2025-0154R1

Aircraft Flight Manual - Limitation / Wings — Front and Rear Spar — Inspections

The document titled Aircraft Flight Manual - Limitation / Wings — Front and Rear Spar — Inspections is an EASA Airworthiness Directive 2025-0154R1 issued on 7 August 2025. It applies to LAVIA ARGENTINA S.A. PA-25, PA-25-235, and PA-25-260 aeroplanes and mandates inspections of specific front and rear wing spars identified by part numbers. The directive addresses corrosion and crack findings in wing spars and related fittings to ensure continued airworthiness.

Aug 7, 2025
Airworthiness DirectiveMaintenanceSafety MgmtLavia PA-25 (Chincul)Lavia PA-25 (Pawnee)Lavia PA-25 (Puelche)

EASA AD 2025-0176

Air — Intermediate / High Pressure Air Tubes / Connectors — Inspection

The document titled Air — Intermediate / High Pressure Air Tubes / Connectors — Inspection is a regulatory directive concerning the inspection requirements for intermediate and high pressure air tubes and connectors on Rolls-Royce Deutschland Ltd & Co KG Trent 1000 engines. It specifies inspection protocols to ensure the integrity and safety of these components in affected aircraft powered by Trent 1000 engines.

Aug 7, 2025
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg TRENT 1000

EASA AD CF-2025-37

Fuel — Fuel Boost Pump — Loose Fasteners and Missing Brush Seal

Airworthiness Directive CF-2025-37 is issued by Transport Canada and applies to Airbus Canada Limited Partnership model BD-500-1A10 and BD-500-1A11 aircraft. It addresses loose fasteners and missing brush seals on the fuel boost pump canister to wing rib 6 interface, which may cause fuel leaks and corrosion. The directive mandates inspections and corrective actions to ensure continued airworthiness.

Aug 6, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus BD-500 (A220 Series)

EASA AD 2025-0173

Aircraft Flight Manual — Normal Procedures — Amendment

EASA Airworthiness Directive 2025-0173 is an amendment addressing the Aircraft Flight Manual normal procedures for ATR 42-400, ATR 42-500, ATR 72-212, and ATR 72-212A aeroplanes. The directive mandates updates to smoke detector check procedures in the flight manuals to enhance safety during cargo operations. It applies to all manufacturer serial numbers of the specified ATR models.

Aug 5, 2025
Airworthiness DirectiveFlight OpsSafety MgmtATR ATR42ATR ATR72

EASA AD 2025-0172

Hydraulic Power — Hydraulic Pump Motor — Replacement

EASA Airworthiness Directive 2025-0172 is an official safety directive addressing hydraulic pump motor replacement on General Atomics AeroTec Systems GmbH Dornier 228 aeroplanes, including models Dornier 228-100 through Dornier 228-212. The directive targets hydraulic pump motor Part Number 1259A, requiring replacement with an improved motor Part Number A-752511A00B to prevent overheating issues. This directive applies to all serial numbers of the affected Dornier 228 aircraft.

Aug 4, 2025
Airworthiness DirectiveMaintenanceSafety MgmtGeneral Atomics Aerotec Systems Gmbh 228

EASA AD 2025-0170

Main Landing Gear — Replacement

The document titled 'Main Landing Gear — Replacement' is a regulatory communication concerning the Airbus A300, A300-600, and A300-600ST (Beluga) aircraft models. It addresses the replacement procedures or requirements related to the main landing gear components of these specific Airbus aircraft types. The document serves as a guideline or directive for maintenance and operational compliance.

Aug 4, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A300Airbus A300-600Airbus A300-600ST (Beluga)

EASA AD BR-E2025-07-03R1

SUPERSEDED BY ANAC BRAZIL AD 2025-10-01

Brazilian Emergency Airworthiness Directive E2025-07-03R1 is issued by the Agência Nacional de Aviação Civil (ANAC) and applies to Embraer ERJ190-300 and ERJ190-400 aircraft equipped with Engine Feed Check Valve Part Number L85E38-003. This directive mandates inspections and functional tests of the engine feed check valves to address potential valve failures that could lead to engine flameout or fuel starvation during flight.

Aug 4, 2025
Airworthiness DirectiveMaintenanceSafety MgmtEmbraer ERJ 190

EASA AD G-2025-0004-E

Hot Air Balloons — Cylinders fitted with PRV adaptor CB8426— Inspect for Cracking and Replace

The Civil Aviation Authority Emergency Airworthiness Directive G-2025-0004-E addresses safety concerns for hot air balloons equipped with fuel cylinders fitted with Pressure Relief Valve (PRV) adaptor CB8426, including models such as Thunder & Colt, Sky Lindstrand, and various Cameron Balloons Limited cylinders. This directive mandates inspection for cracks in the CB8426 adaptors and replacement with the new CB7922 adaptor to prevent uncontrolled LPG fuel leaks.

Aug 1, 2025
Airworthiness DirectiveMaintenanceSafety MgmtCameron Balloons A TypeCameron Balloons A Type CloudhopperCameron Balloons B TypeCameron Balloons C TypeCameron Balloons Cameron Special Shape Hot Air BalloonsCameron Balloons Gas BalloonsCameron Balloons Helium-Hot Air BalloonsCameron Balloons Hot Air BalloonsCameron Balloons L TypeCameron Balloons Lindstrand Special Shape Hot Air BalloonsCameron Balloons S TypeCameron Balloons Sky Hot Air BalloonsCameron Balloons X TypeKubicek Factory S.R.O AB 2 Hot Air BalloonsKubicek Factory S.R.O AB 8 Hot Air BalloonsKubicek Factory S.R.O AEROTECHNIK AB Hot Air BalloonsKubicek Factory S.R.O BB Hot Air BalloonsKubicek Factory S.R.O Special Shape Hot Air BalloonsLindstrand Technologies 203T HiFlyerLindstrand Technologies Series 1Lindstrand Technologies Series 2Lindstrand Technologies Series RLindstrand Technologies Series Special ShapesLindstrand Technologies TGBUltramagic Hot Air BalloonsUltramagic Special Shape Hot Air Balloons

EASA AD US-2025-15-07

Equipment / Furnishings - Captain's and First Officer's Seats - Inspection / Check

Airworthiness Directive 2025-15-07 is a final rule issued by the Federal Aviation Administration addressing The Boeing Company Model 747 series airplanes, including 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, 747-8F, and 747-8. It focuses on inspection and checks of the Captain's and First Officer's seats, specifically the horizontal movement system (HMS), to ensure safety and prevent uncommanded seat movement during critical flight phases.

Jul 31, 2025
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 747

EASA AD 2025-0169

Flight Controls — Trimmable Horizontal Stabilizer Actuator / Electric Load Sensing Device — Modification

EASA Airworthiness Directive 2025-0169 is an official regulatory document addressing modifications to the flight controls, specifically the Trimmable Horizontal Stabilizer Actuator (THSA) and Electric Load Sensing Device (ELSD) on Airbus A330 and A340 aeroplanes. This directive applies to various Airbus A330 models up to manufacturer serial number 1919 (excluding MSN 1915) and all Airbus A340-211, -212, -213, -311, -312, and -313 models. The AD mandates modifications to improve safety related to the THSA's secondary load path and the installation and activation of the ELSD.

Jul 31, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A330Airbus A340

EASA AD 2025-0043R1

SUPERSEDED BY EASA AD 2025-0286

EASA Airworthiness Directive 2025-0043R1 is an amendment addressing Airbus A330-243, A330-243F, A330-841, and A330-941 aeroplanes equipped with Airbus modification 207423 but not modification 211442. The directive mandates updates to the Aircraft Flight Manual and Master Minimum Equipment List to mitigate issues related to loss of data synchronization between Radio Management Panels and the Audio Management Unit. This AD aims to prevent loss of radio communication control, transponder and TCAS setting changes, and standby navigation activation.

Jul 31, 2025
Airworthiness DirectiveFlight OpsSafety MgmtAirbus A330

EASA AD 2025-0168

Wings — Frame 40 Lower Junction Fastener Holes — Inspection

The document titled 'Wings — Frame 40 Lower Junction Fastener Holes — Inspection' is an inspection directive applicable to the AIRBUS S.A.S. A300-600ST (Beluga) aircraft. It addresses the condition and integrity of the fastener holes located at the lower junction of Frame 40 on the wings. The directive aims to ensure continued airworthiness by mandating specific inspection procedures for these critical structural elements.

Jul 31, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A300-600ST (Beluga)