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EASA Regulations & Airworthiness Directives

Browse 4771 EASA regulations with AI-powered summaries.

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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SUPERSEDED BY ANAC BRAZIL EMERGENCY AD 2019-11-08

SUPERSEDED BY ANAC BRAZIL EMERGENCY AD 2019-11-08 is a regulatory document indicating that the current directive has been replaced by the ANAC Brazil Emergency Airworthiness Directive issued on November 8, 2019.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

EASA AD 2019-0274

Landing Gear — Main Landing Gear Leg — Inspection

EASA Airworthiness Directive 2019-0274 is an airworthiness directive issued by EASA concerning the inspection of the main landing gear legs on DAHER Aerospace TB 20 and TB 21 aeroplanes. It mandates repetitive detailed inspections using magnetic particle methods to detect cracks in the main landing gear leg areas. This directive applies to all serial numbers of these aircraft models to ensure continued airworthiness and safety.

Nov 6, 2019
Airworthiness DirectiveMaintenanceSafety MgmtDaher Aerospace TBDAHER Aerospace TB 20DAHER Aerospace TB 21

EASA AD CF-2019-40

Navigation System — Flight Management System, Inertial Reference System and Attitude and Heading Reference System — Outdated Magnetic Variation Tables

Navigation System — Flight Management System, Inertial Reference System and Attitude and Heading Reference System — Outdated Magnetic Variation Tables is a Canadian Airworthiness Directive (CF-2019-40) issued by Transport Canada. It applies to Bombardier Inc. aircraft models CL-600-2B19, CL-600-2C10, CL-600-2C11, CL-600-2D15, CL-600-2D24, and CL-600-2E25. The directive addresses outdated magnetic variation tables used in navigation systems that may cause inaccurate magnetic heading displays and positioning errors.

Nov 6, 2019
Airworthiness DirectiveMaintenanceSafety MgmtMHI RJ Aviation CL-600 (Regional Jet)Bombardier CL-600-2B19Bombardier CL-600-2C10Bombardier CL-600-2C11Bombardier CL-600-2D15Bombardier CL-600-2D24Bombardier CL-600-2E25

EASA AD CF-2019-19R1

Fuel Distribution - Fuel Feed Tube Damage at Bonding Clamp Location Inside the Fuel Tank

Airworthiness Directive CF-2019-19R1 addresses fuel feed tube damage at the bonding clamp location inside the fuel tanks of Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11 aircraft. This directive mandates inspections and modifications to prevent fuel tube failure that could cause fuel imbalance or engine shutdown. It applies to specific serial numbers of these aircraft models.

Nov 4, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus BD-500 (A220 Series)Airbus Canada Limited Partnership BD-500-1A10Airbus Canada Limited Partnership BD-500-1A11

EASA AD 2010-0054-CN

CANCELLED: Flight Controls — Tab-to-Actuator Linkage — Inspection

EASA Airworthiness Directive Cancellation Notice 2010-0054-CN cancels the previous EASA AD 2010-0054, which applied to Dornier 328-100 and 328-300 aeroplanes. The cancellation reflects that the inspection requirements for the flight controls' tab-to-actuator linkage are now incorporated into updated Airworthiness Limitations Sections (ALS) approved by EASA. This notice affects all manufacturer serial numbers of Dornier 328-100 and 328-300 aircraft.

Oct 30, 2019
Agency DecisionMaintenanceSafety MgmtDeutsche Aircraft Gmbh Dornier 328Dornier 328-100Dornier 328-300

EASA AD 2006-0197-CN

CANCELLED: Fuel — Fuel Airworthiness Limitations — Implementation [Fuel Tank Safety]

CANCELLED: Fuel — Fuel Airworthiness Limitations — Implementation [Fuel Tank Safety] is a document related to the DEUTSCHE AIRCRAFT GmbH Dornier 328 aircraft. This document addressed fuel airworthiness limitations focusing on fuel tank safety for the Dornier 328. However, the document has been cancelled and is no longer in effect.

Oct 30, 2019
OtherMaintenanceSafety MgmtDeutsche Aircraft Gmbh Dornier 328DEUTSCHE AIRCRAFT Dornier 328

EASA AD BR-2019-10-02

Instruments - Honeywell Primus EPIC Software - Installation

Brazilian Airworthiness Directive AD No. 2019-10-02 issued by the Agência Nacional de Aviação Civil (ANAC) mandates updates to the Honeywell Primus EPIC software installed on Embraer S.A. ERJ 170 series aircraft. This directive applies to all serial numbers of ERJ 170-100 and ERJ 170-200 variants equipped with specific versions of the Primus EPIC software. The directive addresses unsafe conditions related to erroneous engine parameter indications and autopilot anomalies during flight.

Oct 30, 2019
Airworthiness DirectiveMaintenanceSafety MgmtEmbraer ERJ 170

EASA AD 2014-0140R2

Main Rotor — Hydraulic Drag Damper Lug — Replacement

EASA Airworthiness Directive 2014-0140R2 is a regulatory update addressing the replacement of hydraulic drag damper lugs on PZL SW-4 helicopters. It applies to helicopters fitted with main rotor hydraulic drag dampers Part Number TLH48-1 and targets specific lug parts with potential fatigue life issues. The directive mandates replacement of affected lugs to prevent failure that could lead to ground resonance and safety hazards.

Oct 30, 2019
Airworthiness DirectiveMaintenanceSafety MgmtWsk Pzl-Swidnik SW4PZL SW-4

EASA AD 2019-0270

Time Limits / Maintenance Checks — Certification Maintenance Requirements / Airworthiness Limitations Section — Amendment

EASA Airworthiness Directive 2019-0270 is an amendment addressing time limits and maintenance checks for Dornier 328-100 aeroplanes. It mandates compliance with updated Certification Maintenance Requirements and Airworthiness Limitations as specified by 328 Support Services GmbH. This directive applies to all serial numbers of Dornier 328-100 aircraft and consolidates previous airworthiness directives into a single updated requirement.

Oct 30, 2019
Airworthiness DirectiveMaintenanceSafety MgmtDeutsche Aircraft Gmbh Dornier 328Dornier 328-100

EASA AD 2019-0271

Time Limits / Maintenance Checks — Certification Maintenance Requirements /Airworthiness Limitations Section — Amendment

EASA Airworthiness Directive 2019-0271 is an amendment addressing the time limits and maintenance checks for Dornier 328-300 aeroplanes. It mandates compliance with updated Certification Maintenance Requirements and Airworthiness Limitations Sections as specified by 328 Support Services GmbH. This directive ensures continued airworthiness by enforcing mandatory maintenance tasks and life limits for components on all Dornier 328-300 aircraft.

Oct 30, 2019
Airworthiness DirectiveMaintenanceSafety MgmtDeutsche Aircraft Gmbh Dornier 328Dornier 328-300

EASA AD 2019-0269

Aircraft Flight Manual — Amendment; Navigation — Flight Environment Data / Altimetry System for RVSM Operations — Modification

EASA Airworthiness Directive 2019-0269 is an amendment concerning Piaggio P.180 Avanti II aeroplanes, specifically serial numbers 1002 and 1105 to 3010. It addresses issues with the altimetry system and flight environment data related to Reduced Vertical Separation Minimum (RVSM) operations. The directive mandates modifications to the Aircraft Flight Manual and installation of improved Air Data Computers and Detachable Configuration Modules.

Oct 29, 2019
Airworthiness DirectiveMaintenanceSafety MgmtPiaggio P180Piaggio P.180 Avanti II

EASA AD 2019-0268

Equipment and Furnishings — Emergency Locator Transmitter Sealing Gasket — Inspection / Installation

EASA Airworthiness Directive 2019-0268 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus Helicopters EC 175 B models equipped with CPI 503 ADELT emergency locator transmitters (ELT) with part number 503-16-25. The directive addresses the inspection and installation of the ELT sealing gasket to prevent water ingress that could impair emergency transmission functionality.

Oct 29, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters EC175Airbus Helicopters EC 175 B

EASA AD US-2019-19-02

Fuselage - Underwing Longerons - Inspection

Federal Register Volume 84, Number 205 (October 23, 2019) Final Rule titled 'Fuselage - Underwing Longerons - Inspection' is an FAA Airworthiness Directive (AD 2019-19-02) applicable to certain Boeing 747-400 and 747-400F series airplanes. It mandates repetitive inspections of the underwing longerons and adjacent fuselage skins to detect fatigue cracks and requires corrective actions if cracks are found.

Oct 29, 2019
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 747Boeing 747-400Boeing 747-400F

EASA AD US-2019-21-11

SUPERSEDED BY FAA AD 2021-14-06

FAA Airworthiness Directive 2019-21-11 is a final rule addressing certain Pratt & Whitney PW1519G, PW1521G, PW1521GA, PW1524G, PW1525G, PW1521G-3, PW1524G-3, PW1525G-3, PW1919G, PW1921G, PW1922G, PW1923G, and PW1923G-A turbofan engines. This directive mandates inspections of the low-pressure compressor rotor 1 (LPC R1) for cracks or damage to prevent in-flight failures. It removes the previous requirement to inspect the LPC inlet guide vane (IGV) for alignment and expands applicability to additional engine models.

Oct 29, 2019
Airworthiness DirectiveMaintenanceSafety MgmtPratt & Whitney PW1500GPratt & Whitney PW1900G