EASA Regulations & Airworthiness Directives

Browse 4771 EASA regulations with AI-powered summaries.

EASA AD 2020-0127

Ice and Rain Protection — Wing Anti-Ice Outboard Flexible Hoses — Inspection

EASA Airworthiness Directive 2020-0127 is an airworthiness directive addressing the inspection of wing anti-ice outboard flexible hoses on Dassault Aviation Falcon 10 aeroplanes. It applies to all serial numbers of Falcon 10 aircraft and focuses on inspecting and replacing damaged wing anti-ice flexible hoses with part number 115S018A315. The directive also introduces a new serviceable hose part number 115S118A319 with a defined life limit.

Jun 4, 2020
Airworthiness DirectiveMaintenanceSafety MgmtDassault Falcon 10

EASA AD 2020-0128

Tail Rotor — Tail Rotor Duplex Bearing and Plug — Inspection

EASA Airworthiness Directive 2020-0128 is an airworthiness directive addressing inspection requirements for the tail rotor duplex bearing and plug on Leonardo S.p.A. A119 and AW119MKII helicopters. It applies to helicopters with manufacturer serial numbers up to 14972, excluding certain serial numbers, and focuses on inspecting and correcting issues related to the tail rotor pitch change mechanism components.

Jun 4, 2020
Airworthiness DirectiveMaintenanceSafety MgmtLeonardo S.P.A. Helicopters A109Leonardo S.P.A. Helicopters A119Leonardo A119Leonardo AW119MKII

EASA SIB AIR-20-10

FAA AD 2020-03-16 Alternative Methods of Compliance and FAQ

FAA AD 2020-03-16 Alternative Methods of Compliance and FAQ is a Special Airworthiness Information Bulletin providing information on four alternative methods of compliance (AMOCs) related to FAA Airworthiness Directive 2020-03-16. This directive affects Textron Aviation Inc. Models 210G, T210G, 210H, T210H, 210J, T210J, 210K, T210K, 210L, T210L, 210M, and T210M airplanes and addresses inspections and corrosion issues on the carry-thru spar lower cap. The bulletin also answers frequently asked questions about the AD and compliance options.

Jun 3, 2020
Safety Information BulletinMaintenanceSafety Mgmt

EASA AD 2020-0126

Flight Controls — Flap Drive Struts and Lever Bearing Assemblies — Inspection

EASA Airworthiness Directive 2020-0126 is an airworthiness directive issued for Airbus A350-1041 aeroplanes. It mandates inspections of the flap drive struts and lever bearing assemblies at flap station 3 on both right-hand and left-hand sides to detect wear and corrosion. This directive aims to prevent potential flap detachment during flight by ensuring the structural integrity of these components.

Jun 3, 2020
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A350Airbus A350-1041

EASA AD BR-2020-05-03

Aircraft Flight Manual - Operational Envelope Temperature / Minimum Airspeed Limitation - Amendment

The Aircraft Flight Manual - Operational Envelope Temperature / Minimum Airspeed Limitation - Amendment is a Brazilian Airworthiness Directive (AD No. 2020-05-03) issued by ANAC that applies to Embraer EMB-500 and EMB-505 aircraft equipped with PW617F-E, PW617F1-E, or PW535E engines. It addresses operational limitations related to static air temperatures below -54°C to ensure safe aircraft operation within the approved flight envelope.

Jun 2, 2020
Airworthiness DirectiveFlight OpsSafety MgmtEmbraer EMB-500 (Phenom 100)Embraer EMB-505 (Phenom 300)Embraer EMB-500Embraer EMB-505

EASA AD 2020-0125

Aircraft Flight Manual Section Limitations — Amendment

EASA Airworthiness Directive 2020-0125 is an amendment addressing flight control law limitations on Airbus A320neo aircraft models A320-251N, A320-252N, A320-253N, A320-271N, A320-272N, and A320-273N. It mandates updates to the Aircraft Flight Manual (AFM) to incorporate temporary revisions or later AFM revisions that include new center of gravity (CG) envelopes enabled by Airbus modification 163923. This directive aims to ensure safe operation by limiting flight configurations that could reduce angle of attack protection efficiency.

Jun 2, 2020
Airworthiness DirectiveFlight OpsSafety MgmtAirbus A320Airbus A320neo

EASA AD 2019-0171R2

Aircraft Flight Manual Section Limitations — Amendment

EASA Airworthiness Directive 2019-0171R2 is an amendment addressing Airbus A321neo aircraft equipped with specific Elevator Aileron Computer (ELAC) units. It mandates changes to the Aircraft Flight Manual (AFM) limitations to mitigate reduced angle of attack protection caused by certain ELAC software versions. The directive applies to various A321neo models except those with Airbus modification 163923 installed in production.

Jun 2, 2020
Airworthiness DirectiveFlight OpsSafety MgmtAirbus A321Airbus A321neo

EASA SIB 2020-09

CEAPR DR 400 Aeroplanes - Defective Seat Belt Attachment Rivet Assembly

EASA Safety Information Bulletin 2020-09 is a safety information bulletin addressing a defective seat belt attachment rivet assembly in CEAPR DR 400 aeroplanes. The affected models include DR 400/100, DR 400/120, DR 400/140 B, DR 400/160, DR 400/180, and DR 400/180 R with specific serial numbers from 2703 to 2734. The bulletin provides guidance on inspection and corrective actions related to the rivet assembly holding the front seat belt retractor.

May 29, 2020
Safety Information BulletinMaintenanceSafety Mgmt

EASA SIB 2020-10

CEAPR DR 400 Aeroplanes - Defective Warning Lights Panel

EASA Safety Information Bulletin 2020-10 is an airworthiness bulletin addressing defective warning lights panels on CEAPR DR 400 series aeroplanes, specifically models DR 400/100, DR 400/120, DR 400/140 B, DR 400/160, DR 400/180, and DR 400/180 R with certain serial numbers. The bulletin informs operators about a wiring defect that may cause a short circuit during the warning lights test when the pitot heater is on. It provides guidance on inspection and corrective actions via CEAPR Service Bulletin 190902.

May 29, 2020
Safety Information BulletinMaintenanceSafety Mgmt

EASA AD 2020-0122

Equipment / Furnishings — Overhead Stowage Compartment Fixation Brackets — Inspection

EASA Airworthiness Directive 2020-0122 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A320-271N, A321-211, and A321-271N aeroplanes with specific manufacturer serial numbers. The directive addresses the inspection of overhead stowage compartment X-fixation brackets to ensure their correct installation and presence. It mandates a one-time detailed inspection to prevent potential overhead stowage compartment failure that could cause passenger injury.

May 29, 2020
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A320Airbus A321

EASA AD 2020-0124

SUPERSEDED BY EASA AD 2020-0154

EASA Airworthiness Directive 2020-0124 is an airworthiness directive issued by the European Union Aviation Safety Agency concerning Rolls-Royce Trent 1000-D2, Trent 1000-J2, and Trent 1000-K2 engines, commonly installed on Boeing 787 aircraft. The directive addresses fuel pump life limitations due to wear-related performance degradation. It mandates replacement of affected fuel pumps to maintain engine performance and safety.

May 29, 2020
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg TRENT 1000Boeing 787

EASA AD 2020-0123

SUPERSEDED BY EASA AD 2023-0068

EASA Airworthiness Directive 2020-0123 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A350-941 aeroplanes, except those with Airbus modification 109799 incorporated in production. The directive addresses an unsafe condition related to the rotation of certain fasteners in the centre wing box, which could lead to fuel vapour leakage inside the cabin. This directive mandates the replacement of affected fasteners with improved friction material fasteners to ensure continued airworthiness.

May 29, 2020
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A350Airbus A350-941

EASA AD 2020-0121

SUPERSEDED BY EASA AD 2020-0138

EASA Airworthiness Directive 2020-0121 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting various Grob sailplanes including ASTIR CS series, CLUB ASTIR II, TWIN ASTIR models, and G 103 series powered and unpowered sailplanes. The directive addresses the inspection and potential replacement of the elevator control pushrod in the vertical fin to prevent corrosion-related failures. This AD applies to all serial numbers of the specified models and mandates inspection procedures defined by Fiberglas-Technik R. Lindner GmbH & Co. KG.

May 28, 2020
Airworthiness DirectiveMaintenanceSafety MgmtE Aerospace Fischer Gmbh ASTIR CS TOPFiberglas Technik R. Lindner Grob SailplanesGrob ASTIR CSGrob CLUB ASTIR IIGrob TWIN ASTIRGrob G 103

EASA AD 2020-0097R1

SUPERSEDED BY EASA AD 2025-0205

EASA Airworthiness Directive 2020-0097R1 is an updated directive addressing inspection and potential repair or replacement of passenger seat tracks on ATR 42 and ATR 72 aeroplanes. It applies to specific seat track part numbers manufactured between 2012 and 2017 and targets certain serial number ranges of ATR 42 and ATR 72 aircraft. The directive aims to ensure the structural integrity of seat tracks to prevent failure during emergency landings.

May 28, 2020
Airworthiness DirectiveMaintenanceSafety MgmtATR ATR42ATR ATR72ATR 42ATR 72

EASA AD CF-2020-19

Oxygen — Crew — Inspection and Removal of a Protective End Cap Obstructing an Extraction Duct

Canadian Airworthiness Directive CF-2020-19 mandates inspection and removal of a protective end cap obstructing an extraction duct on certain Airbus Canada Limited Partnership aircraft models BD-500-1A10 and BD-500-1A11. This directive addresses a safety issue related to crew oxygen systems and ventilation under the flight deck floor. The affected aircraft include specific serial numbers of the BD-500-1A10 and BD-500-1A11 models.

May 27, 2020
Airworthiness DirectiveMaintenanceSafety MgmtAirbus BD-500 (A220 Series)Airbus Canada BD-500-1A10Airbus Canada BD-500-1A11

EASA AD 2020-0120

SUPERSEDED BY EASA AD 2020-0278

EASA Airworthiness Directive 2020-0120 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all Pilatus PC-6 aeroplanes. It mandates compliance with updated airworthiness limitations and maintenance tasks as specified in the latest Pilatus PC-6 Aircraft Maintenance Manual and Airworthiness Limitations Section documents. The directive ensures continued airworthiness by requiring specific inspections and maintenance actions for these aircraft.

May 27, 2020
Airworthiness DirectiveMaintenanceSafety MgmtPilatus Aircraft PC-6Pilatus PC-6

EASA AD 2020-0110R1

SUPERSEDED BY EASA AD 2024-0008

EASA Airworthiness Directive 2020-0110R1 is an updated directive addressing structural inspections on Airbus A300 aeroplanes of all certified models and manufacturer serial numbers. It mandates repetitive special detailed inspections of specific fuselage areas including the windshield frame, skin lap joint, and centre wing bottom skin to detect cracks that could compromise structural integrity. This directive applies to various groups of A300 aircraft differentiated by embodied Airbus modifications and service bulletins.

May 27, 2020
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A300

EASA AD 2020-0112R1

SUPERSEDED BY EASA AD 2024-0010

EASA Airworthiness Directive 2020-0112R1 is an updated directive addressing structural inspections on Airbus A310 aeroplanes. It mandates repetitive special detailed inspections of specific fuselage areas, including the windshield frame and circumferential junctions, to detect cracks that could compromise structural integrity. This directive applies to all certified Airbus A310 models and serial numbers.

May 27, 2020
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A310

EASA AD 2020-0119

Equipment / Furnishings — Emergency Locator Transmitter — Inhibition / Replacement

The document titled Equipment / Furnishings — Emergency Locator Transmitter — Inhibition / Replacement is an airworthiness directive concerning AIRBUS HELICOPTERS: EC175. It addresses requirements related to the emergency locator transmitter (ELT) system, specifically its inhibition and replacement procedures for this helicopter model.

May 26, 2020
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters EC175

EASA AD BR-2020-05-02

Flight Controls - Horizontal Stabilizer Control Yoke Assemblies - Modification

Brazilian Airworthiness Directive 2020-05-02 is a regulatory document issued by the Agência Nacional de Aviação Civil (ANAC) that applies to Yaborã Indústria Aeronáutica S.A. ERJ 190 series airplanes equipped with specific Embraer Control Yoke Assemblies. It addresses a safety issue related to the incorrect installation of horizontal stabilizer pitch trim switches on the control yokes. The directive mandates modifications to prevent reversed pitch trim commands.

May 26, 2020
Airworthiness DirectiveMaintenanceSafety MgmtEmbraer ERJ 190