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EASA Regulations & Airworthiness Directives

Browse 4995 EASA regulations with AI-powered summaries.

Aircraft:AllAirbus A320280Airbus A321276Airbus A319246Airbus A350214Airbus A330210All194Airbus A318185Airbus A380171Boeing 737170Airbus A340140Airbus A350-941125Airbus BD-500 (A220 Series)116Airbus Helicopters AS 332116Airbus Helicopters EC 225113Airbus Helicopters SA 330113Show all...

EASA AD BR-2019-11-07

Landing Gear - Pintle Pins of the Main Landing Gear Shock Struts - Inspection / Replacement

Brazilian Airworthiness Directive AD No. 2019-11-07 addresses inspection and replacement requirements for the pintle pins of the main landing gear shock struts on specific Embraer ERJ 170 and ERJ 190 series aircraft. The directive applies to certain pintle pins repaired under specific Liebherr Aerospace engineering dispositions that may have reduced life limits. It mandates inspections and replacement of affected pintle pins to ensure continued airworthiness and safety.

Nov 20, 2019
Airworthiness DirectiveMaintenanceSafety MgmtEmbraer ERJ 170Embraer ERJ 190

EASA AD 2019-0284-E

Wings — Inner Flap Fitting Bearing Bolts — Inspection

EASA Airworthiness Directive 2019-0284-E is an emergency directive addressing the inspection of inner flap fitting bearing bolts on SIAT 223 aeroplanes. It mandates repetitive inspections of specific bearing bolts with part numbers 223-20-13003 or 223-20-13053 due to reported cracks. The directive aims to ensure continued airworthiness and prevent potential loss of control caused by bolt fractures.

Nov 20, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Defence & Space Gmbh SIAT 223SIAT 223

EASA AD 2019-0280

Main Rotor — Spherical Bearing — Inspection / Time Limit

EASA Airworthiness Directive 2019-0280 is an airworthiness directive issued for Airbus Helicopters AS 350 BB models. It addresses the inspection and life limit requirements for the main rotor spherical thrust bearing, part number 579085. The directive mandates inspections and replacement of these bearings to ensure continued airworthiness.

Nov 19, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters AS 350Airbus Helicopters EC 130Airbus Helicopters AS 350 BB

EASA AD CF-2019-42

Flight Controls — Rudder Control System — Rudder Feel Unit Shaft Fracture

Canadian Airworthiness Directive CF-2019-42 addresses a safety issue in Bombardier Inc. aeroplanes including models CL-600-2B19, CL-600-2C10, CL-600-2D15, CL-600-2D24, and CL-600-2C11. The directive concerns the rudder control system, specifically the rudder feel unit shaft, which has been found to fracture due to fatigue. This fracture could lead to loss of rudder feel and affect aircraft controllability.

Nov 18, 2019
Airworthiness DirectiveMaintenanceSafety MgmtMHI RJ Aviation CL-600 (Regional Jet)Bombardier CL-600-2B19Bombardier CL-600-2C10Bombardier CL-600-2D15Bombardier CL-600-2D24Bombardier CL-600-2C11

EASA AD CF-2019-41

Ice and Rain Protection — Wing Anti-Ice System — Additional Operating Limitations

Canadian Airworthiness Directive CF-2019-41 addresses additional operating limitations for the wing anti-ice system on Bombardier Inc. CL-600-2B19 aircraft. This directive mandates changes to the Airplane Flight Manual to ensure the wing anti-ice system is activated under specific conditions to prevent ice accumulation on wing leading edges. The directive aims to enhance safety by mitigating risks associated with undetected ice during landing.

Nov 18, 2019
Airworthiness DirectiveFlight OpsSafety MgmtMHI RJ Aviation CL-600 (Regional Jet)Bombardier CL-600-2B19

EASA AD 2019-0272R1

SUPERSEDED BY EASA AD 2021-0069

EASA Airworthiness Directive 2019-0272R1 is an amendment addressing safety concerns for Airbus Helicopters EC 120 B models. It mandates inspections and potential replacement of the tail rotor hub body, part number C642A0100103, to prevent loss of tail rotor drive and yaw control. The directive includes detailed inspection and replacement procedures to ensure continued airworthiness.

Nov 18, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters EC 120 B

EASA AD CF-2019-43

Landing Gear — Nose Landing Gear Shock Strut Cylinder Corrosion

Canadian Airworthiness Directive CF-2019-43 addresses corrosion found on the nose landing gear (NLG) shock strut cylinders of Bombardier BD-100-1A10 aircraft, serial numbers 20003 through 20767. This directive mandates inspections and modifications to the NLG shock strut cylinders to prevent structural failure due to corrosion. It also restricts installation of certain replacement NLG shock strut assemblies unless reworked according to specified service bulletins.

Nov 15, 2019
Airworthiness DirectiveMaintenanceSafety MgmtBombardier BD-100Bombardier BD-100-1A10

EASA AD US-2019-21-08

SUPERSEDED BY FAA AD 2019-23-10

FAA Airworthiness Directive 2019-21-08 is a final rule addressing Textron Aviation Inc. airplanes, including Models E33, E33A, E33C, F33, G33, 35-C33, 35-C33A, K35, M35, N35, P35, S35, V35, V35A, 36, and certain serial-numbered Models F33A, F33C, V35B, and A36. This directive mandates inspection and replacement of damaged right aileron flight control cable end fittings to prevent potential failure. The AD aims to enhance flight safety by mitigating risks associated with cracked or fractured cable fittings.

Nov 15, 2019
Airworthiness DirectiveMaintenanceSafety MgmtTextron Aviation 33 (Bonanza)Textron Aviation 35 (Bonanza)Textron Aviation 36 (Bonanza)Textron Aviation E33Textron Aviation E33ATextron Aviation E33CTextron Aviation F33Textron Aviation G33Textron Aviation 35-C33Textron Aviation 35-C33ATextron Aviation K35Textron Aviation M35Textron Aviation N35Textron Aviation P35Textron Aviation S35Textron Aviation V35Textron Aviation V35ATextron Aviation 36Textron Aviation F33ATextron Aviation F33CTextron Aviation V35BTextron Aviation A36

EASA AD 2019-0267R1

SUPERSEDED BY EASA AD 2020-0078

EASA Airworthiness Directive 2019-0267R1 is an update addressing the inspection and replacement requirements for the double bearing installed on the tail rotor gearbox of Airbus Helicopters SA 365, AS 365, and EC155 models. This directive applies to all serial numbers of these helicopter types and focuses on preventing loss of yaw control due to bearing degradation. It mandates repetitive inspections of the tail rotor gearbox chip detector and timely replacement of affected double bearings.

Nov 13, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SAAirbus Helicopters AS 365Airbus Helicopters EC 155Airbus Helicopters SA 365Airbus Helicopters EC155

EASA AD US-2019-22-10

SUPERSEDED BY FAA AD 2021-09-06

FAA Airworthiness Directive 2019-22-10 is a final rule affecting all Boeing 737-600, -700, -700C, -800, -900, and -900ER series airplanes. It mandates expanded repetitive inspections for cracking in the left- and right-hand side outboard chords of frame fittings and failsafe straps at station 663.75, around eight fasteners adjacent to stringer S-18A straps. This directive addresses structural integrity concerns to prevent potential loss of airplane control.

Nov 13, 2019
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 737Boeing 737-600Boeing 737-700Boeing 737-700CBoeing 737-800Boeing 737-900Boeing 737-900ER

EASA AD 2019-0277-E

Air — Anti-icing Valve Assembly Gaskets — Replacement

EASA Airworthiness Directive 2019-0277-E is an emergency directive addressing SAFRAN RTM322-01/9 and RTM322-01/9A helicopter engines, commonly installed on NH Industries NH90 military helicopters. The directive mandates replacement of specific anti-icing valve assembly gaskets to prevent loss of anti-icing function. It applies to engines with affected gasket part numbers 0322710040 and 0322710050.

Nov 12, 2019
Airworthiness DirectiveMaintenanceSafety MgmtSafran RTM 322NH Industries NH90

EASA AD 2019-0278

Electronic Common Installation — Engine Nacelle Electrical Wiring — Modification; Hydraulic Power — Underwing Box Hydraulic Pipe — Inspection / Replacement

Electronic Common Installation — Engine Nacelle Electrical Wiring — Modification; Hydraulic Power — Underwing Box Hydraulic Pipe — Inspection / Replacement is a regulatory document applicable to ATR ATR42 and ATR72 aircraft. It addresses modifications to the electrical wiring within the engine nacelle and mandates inspection and potential replacement of the hydraulic pipes located in the underwing box. These measures aim to ensure continued airworthiness and operational safety of the affected aircraft models.

Nov 12, 2019
Airworthiness DirectiveMaintenanceSafety MgmtATR ATR42ATR ATR72

EASA AD 2019-0181R1

Fuselage — Forward and Aft Cargo Door Latch Fitting External Lugs — Inspection / Modification

EASA Airworthiness Directive 2019-0181R1 is an updated regulatory requirement affecting Airbus A350-941 aeroplanes, specifically addressing the forward and aft cargo door latch fitting external lugs. The directive mandates inspections and potential modifications to aluminium latch fittings to ensure structural integrity. It applies to all serial numbers except those with Airbus modifications 107020 and 107049 incorporated during production.

Nov 12, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A350Airbus A350-941

EASA SIB CASA-2019-06

Bell Helicopter 429 and 430 Helicopters - External Hoist Hook Bumper

The Transport Canada Civil Aviation Safety Alert CASA 2019-06 addresses a safety concern affecting Bell Helicopter models 429 and 430 equipped with the optional Goodrich 600-pound capacity external hoist. The alert highlights a potential incorrect assembly of the external hoist hook bumper, which could lead to loosening of the assembly and possible loss of the hoist load. This document provides safety information and recommended corrective actions to ensure proper assembly and mitigate failure risks.

Nov 11, 2019
Safety Information BulletinMaintenanceSafety Mgmt

EASA AD BR-2019-11-06

SUPERSEDED BY ANAC BRAZIL EMERGENCY AD 2019-11-08

SUPERSEDED BY ANAC BRAZIL EMERGENCY AD 2019-11-08 is a regulatory document indicating that the current directive has been replaced by the ANAC Brazil Emergency Airworthiness Directive issued on November 8, 2019. The document does not provide specific details about affected aircraft, engines, or parts due to corrupted content. It serves as a notice of supersession rather than a standalone directive.

Nov 11, 2019
Airworthiness DirectiveSafety MgmtEmbraer EMB-505 (Phenom 300)

EASA AD 2019-0088R1

Placards and Markings — Inspection / Installation

The document titled "Placards and Markings — Inspection / Installation" applies to Airbus Helicopters models SA 330, AS 332, EC 225, SA/AS 365, and EC 155. It provides guidance on the inspection and proper installation of placards and markings on these helicopter types to ensure compliance with safety and regulatory standards. The document aims to maintain the visibility and legibility of critical information displayed on the aircraft.

Nov 8, 2019
OtherMaintenanceSafety MgmtAirbus Helicopters SA 330Airbus Helicopters AS 332Airbus Helicopters EC 225Airbus Helicopters SAAirbus Helicopters AS 365Airbus Helicopters EC 155Airbus Helicopters SA 365

EASA AD 2019-0276

SUPERSEDED BY EASA ADR 2021-0157

The document titled SUPERSEDED BY EASA ADR 2021-0157 is an explanatory statement regarding the absence of an Airworthiness Directive (AD) document for the Airbus A400M aircraft. It clarifies that no Airbus A400M aeroplanes are currently in civil service, and therefore, no public AD exists. The document serves as an informational record for design approval holders and military airworthiness authorities, recommending that military authorities issue their own ADs as applicable.

Nov 8, 2019
OtherMaintenanceSafety MgmtAirbus Military A400MAirbus A400M

EASA AD CF-2019-38

Electrical Power — Ram Air Turbine Deployment Actuator Galling

Canadian Airworthiness Directive CF-2019-38 addresses an issue with the Ram Air Turbine (RAT) Deployment Actuator on Bombardier BD-700-1A10 and BD-700-1A11 aircraft. The directive targets actuators with part number BZ02001-01 that may have an incorrectly applied anti-fretting coating, potentially causing galling and failure to deploy the RAT. This failure could compromise the aircraft's ability to power essential systems during total power loss.

Nov 7, 2019
Airworthiness DirectiveMaintenanceSafety MgmtBombardier BD-700Bombardier BD-700-1A10Bombardier BD-700-1A11

EASA AD 2019-0275

Power Plant — Engine Mount Bushings — Inspection / Replacement

EASA Airworthiness Directive 2019-0275 is an official regulatory document addressing inspection and replacement requirements for engine mount bushings on Airbus Helicopters Deutschland GmbH MBB-BK117 D-2 helicopters. It applies to all serial numbers of this helicopter model and focuses on both elastomeric and metal engine mount bushings identified by specific part numbers. The directive mandates repetitive inspections and corrective actions to prevent potential engine mount failures.

Nov 7, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters MBB-BK 117Airbus Helicopters MBB-BK117 D-2