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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 US-2019-16-01

Engine - Turbine Exhaust Case - Inspection

The Federal Aviation Administration's Airworthiness Directive 2019-16-01 addresses all International Aero Engines AG V2525-D5 and V2528-D5 turbofan engines. This directive mandates inspections of turbine exhaust cases due to reports of cracks, aiming to prevent engine failure and potential loss of the airplane. It requires initial and repetitive inspections and replacement of affected parts if cracks are found.

Aug 20, 2019
Airworthiness DirectiveMaintenanceSafety MgmtInternational Aero Engines Ag V2500-( )5

EASA AD 2019-0205

SUPERSEDED BY EASA AD 2019-0251

EASA Airworthiness Directive 2019-0205 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A380-841, A380-842, and A380-861 aeroplanes. It addresses the engine bleed air system, specifically the Certification Maintenance Requirements task related to the pneumatic system. The directive mandates inspections and functional tests to ensure continued airworthiness of the affected aircraft.

Aug 20, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380Airbus A380-841Airbus A380-842Airbus A380-861

EASA AD 2019-0206

SUPERSEDED BY EASA AD 2021-0141

EASA Airworthiness Directive 2019-0206 is an airworthiness directive issued for Airbus A350-941 and A350-1041 aeroplanes, excluding those with certain production modifications. It addresses inspection and maintenance requirements for the trimmable horizontal stabilizer fittings and bearing assembly attachment interface to prevent potential corrosion and structural issues.

Aug 20, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A350Airbus A350-941Airbus A350-1041

EASA AD 2019-0201

SUPERSEDED BY EASA AD 2023-0062

EASA Airworthiness Directive 2023-0062 is an airworthiness directive concerning the Dassault Aviation Mystère-Falcon 20 aircraft. This directive replaces previous regulatory requirements to ensure continued safety and compliance for the specified aircraft type. It addresses necessary inspections, modifications, or operational limitations to maintain airworthiness standards.

Aug 20, 2019
Airworthiness DirectiveMaintenanceSafety MgmtDassault Mystère-Falcon 20Dassault Aviation Mystère-Falcon 20

EASA AD US-2019-16-04

SUPERSEDED BY FAA AD 2019-18-08

FAA Airworthiness Directive 2019-16-04 is a final rule affecting Engine Alliance GP7270 and GP7277 model turbofan engines equipped with a specific engine fan hub assembly. It mandates inspections and possible replacement of the engine fan hub blade lock assembly to address potential uncontained failures. This directive updates previous requirements to enhance safety measures for these engine models.

Aug 20, 2019
Airworthiness DirectiveMaintenanceSafety MgmtEngine Alliance GP7200

EASA AD US-2019-14-13

SUPERSEDED BY FAA AD 2025-01-06

FAA Airworthiness Directive 2019-14-13 is a final rule affecting all Boeing 767-200, -300, -300F, and -400ER series airplanes. It addresses uncommanded fore/aft movements of the Captain's and First Officer's seats by requiring identification of seat part and serial numbers, detailed inspections, repetitive checks of the horizontal movement system, and applicable corrective actions. An optional terminating action is provided for certain airplanes to end repetitive checks.

Aug 20, 2019
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 767Boeing 767-200Boeing 767-300Boeing 767-300FBoeing 767-400ER

EASA AD 2019-0202

Main Rotor — Blade Droop Stops — Removal from Service

EASA Airworthiness Directive 2019-0202 is an airworthiness directive addressing the removal from service of main rotor blade droop stops, Part Number 37.21.800.00.00, installed on PZL W-3A and W-3AS helicopters. The directive applies to all manufacturer serial numbers of these helicopter models and mandates removal of affected parts to prevent unsafe conditions.

Aug 19, 2019
Airworthiness DirectiveMaintenanceSafety MgmtWsk Pzl-Swidnik PZL W-3APZL W-3APZL W-3AS

EASA AD 2019-0199

Tail Rotor Drive - Ti-Bolt - Inspection / Replacement

EASA Airworthiness Directive 2019-0199 is an airworthiness directive addressing the inspection and replacement of titanium (Ti) bolts, part number L535M2001203, installed on the forward tail rotor drive shaft of Airbus Helicopters Deutschland GmbH EC135 and EC635 helicopter models. The directive applies to all variants and serial numbers of these helicopters. It mandates inspection and, if necessary, replacement of affected Ti-bolts to ensure continued airworthiness.

Aug 16, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters EC135Airbus Helicopters 635Airbus Helicopters EC635

EASA AD 2019-0198

Flight Controls — Wiring Harness — Modification

EASA Airworthiness Directive 2019-0198 is an airworthiness directive addressing wiring harness modifications for Airbus Helicopters Deutschland GmbH MBB-BK117 D-2 helicopters. It targets specific wire harness trim connector backshells with part number M85049/90-13W02 manufactured by AMPHENOL or of unknown manufacturer. The directive aims to prevent potential short circuits in yaw and pitch trim actuators that could lead to loss of helicopter control.

Aug 15, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters MBB-BK 117Airbus Helicopters MBB-BK117 D-2

EASA AD 2019-0196

Fuselage — Cabin, Cargo Compartment and Airframe Parts — Inspection / Replacement [Improper Heat Treatment]

EASA Airworthiness Directive 2019-0196 is an airworthiness directive addressing improper heat treatment of certain structural parts in Airbus A318, A319, A320, and A321 aircraft. It mandates inspections and possible replacement of affected cabin, cargo compartment, and airframe parts to ensure structural integrity. The directive applies to specific manufacturer serial numbers and references Airbus Service Bulletins for inspection procedures.

Aug 14, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD CF-2019-29

Flight Controls — Multi-Function Spoiler Jam

Canadian Airworthiness Directive CF-2019-29 addresses a flight control issue involving the multi-function spoiler (MFS) jam on Bombardier Inc. model BD-100-1A10 aircraft, serial numbers 20003 through 20788. The directive mandates updates to the Airplane Flight Manual procedures to manage uncommanded spoiler deployment that can cause high crew workload during roll control. This AD aims to enhance flight safety by providing revised non-normal procedures for affected aircraft.

Aug 13, 2019
Airworthiness DirectiveFlight OpsSafety MgmtBombardier BD-100Bombardier BD-100-1A10

EASA AD 2019-0195

SUPERSEDED BY EASA AD 2020-0086

EASA Airworthiness Directive 2019-0195 is an airworthiness directive issued by the European Union Aviation Safety Agency concerning Airbus Helicopters AS 332 and SA 330 models. It addresses inspection and replacement requirements for tail rotor hub assembly components, specifically flapping hinge components and spindle bolts, to prevent potential failures that could lead to loss of helicopter control.

Aug 13, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SA 330Airbus Helicopters AS 332Airbus Helicopters EC 225

EASA AD US-2019-16-02

Engine Fuel Control - Fuel Pump Metering Unit - Replacement

The Federal Register Volume 84, Number 154 (August 9, 2019) final rule titled "Engine Fuel Control - Fuel Pump Metering Unit - Replacement" is an Airworthiness Directive issued by the FAA for all GE Honda Aero Engines HF120 model turbofan engines equipped with fuel pump metering unit (FPMU) assembly part number 24100-Q0A-F000. This directive addresses damage found on the permanent magnetic alternator drive gear within the FPMU assembly that could lead to engine failure. The AD mandates replacement of the affected FPMU assembly with approved parts to ensure continued airworthiness and safety.

Aug 12, 2019
Airworthiness DirectiveMaintenanceSafety MgmtGe Honda Aero Engines, HF120

EASA AD 2019-0086R1

Flight Controls — Active Technology Load Alleviating System — Deactivation / Modification ; Airplane Flight Manual Supplement — Amendment

The document titled 'Flight Controls — Active Technology Load Alleviating System — Deactivation / Modification ; Airplane Flight Manual Supplement — Amendment' is an EASA Supplemental Type Certificate (STC) amendment issued for the CRANFIELD AEROSPACE SOLUTIONS Ltd. and TEXTRON AVIATION INC. CitationJet model 525 aircraft. It addresses modifications related to the deactivation or alteration of the Active Technology Load Alleviating System (ATLAS) flight control system. This amendment includes updates to the Airplane Flight Manual Supplement to reflect these changes.

Aug 9, 2019
Agency DecisionFlight OpsMaintenanceTextron Aviation 525 (CitationJet)Textron Aviation CitationJet 525

EASA AD 2019-0194-E

SUPERSEDED BY EASA AD 2020-0128

EASA Airworthiness Directive 2019-0194-E is an emergency directive addressing safety concerns for Leonardo S.p.A. A119 and AW119MKII helicopters, specifically those with manufacturer serial numbers up to 14966, excluding certain serial numbers. The directive mandates inspections and corrective actions related to the tail rotor duplex bearing and plug to prevent potential loss of helicopter control.

Aug 9, 2019
Airworthiness DirectiveMaintenanceSafety MgmtLeonardo S.P.A. Helicopters A109Leonardo S.P.A. Helicopters A119Leonardo A119Leonardo AW119MKII

EASA AD 2019-0193

SUPERSEDED BY EASA AD 2020-0048

EASA Airworthiness Directive 2019-0193 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all serial numbers of Leonardo S.p.A. AW169 and AW189 helicopters. The directive addresses inspections and monitoring of the tail rotor servo actuator and duplex bearing to prevent potential loss of yaw control. It mandates repetitive inspections, thermal strip installations, and reporting requirements to ensure continued airworthiness and safety of these helicopter models.

Aug 7, 2019
Airworthiness DirectiveMaintenanceSafety MgmtLeonardo S.P.A. Helicopters AW169Leonardo S.P.A. Helicopters AW189Leonardo AW169Leonardo AW189

EASA AD 2019-0192

Electrical Power — Ram Air Turbine Free Rotation — Manual Check

EASA Airworthiness Directive 2019-0192 is an airworthiness directive addressing the Airbus A380 aeroplanes equipped with specific Ram Air Turbine (RAT) parts, identified by part numbers 1704287G and 1704287H with serial numbers AAB4000001 to AAB4000333. This directive mandates a manual free rotation check of the RAT to detect water ingress and corrosion that could impair RAT operation and electrical power generation. It applies to Airbus A380 models -841, -842, and -861 with specified manufacturer serial numbers.

Aug 5, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380

EASA AD 2019-0187

[Correction] Powerplant — Engine Cooling Fan — Replacement

EASA Airworthiness Directive 2019-0187 is a corrective directive addressing the replacement of engine cooling fans on Hélicoptères Guimbal Cabri G2 helicopters. It applies to specific aluminium cooling fan part numbers G52-00-000, G52-00-001, and G52-04-100, requiring replacement with a serviceable composite front flange cooling fan P/N G52-04-101. The directive aims to prevent engine in-flight shutdowns caused by cooling fan failures.

Aug 2, 2019
Airworthiness DirectiveMaintenanceSafety MgmtGuimbal, Helicopteres CABRIHélicoptères Guimbal Cabri G2

EASA AD 2018-0249R1

[Correction] Wings — Centre Wing Box Fastener Holes at Frame 40 Vertical Web — Inspection / Modification

EASA Airworthiness Directive 2018-0249R1 is a regulatory update addressing inspection and modification requirements for the centre wing box fastener holes at Frame 40 vertical web on Airbus A330 and A340 aeroplanes. It applies to multiple A330 and A340 variants, excluding those with specific Airbus Repair Instructions embodied. The directive mandates repetitive special detailed inspections and corrective actions to ensure structural integrity of the centre fuselage.

Aug 2, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A330Airbus A340