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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 2019-0067R1

SUPERSEDED BY EASA AD 2022-0151

EASA Airworthiness Directive 2019-0067R1 is a regulatory document addressing inspection requirements for the horizontal upper stiffeners of the lateral cockpit window frame on Airbus A318, A319, A320, and A321 aircraft. It mandates repetitive special detailed inspections using high frequency eddy current methods to detect cracks that could compromise fuselage structural integrity. This directive applies to specific serial numbers and configurations of these Airbus models, excluding certain modified aircraft.

Sep 11, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA SIB CASA-2019-05-Issue-2

Bell 206L Helicopters - Cracks in Fuselage

Transport Canada Civil Aviation Safety Alert CASA 2019-05 is a safety alert addressing the discovery of cracks in the fuselage frame and bulkhead of Bell 206L series helicopters, specifically around fuselage stations FS142.7 to FS155.00. The alert highlights multiple occurrences of cracks and rivet issues in the upper fuselage area, including stiffener part number 206-033-107-055. It aims to raise awareness among owners, operators, and maintainers of Bell 206L helicopters about this structural concern.

Sep 9, 2019
Safety Information BulletinMaintenanceSafety Mgmt

EASA AD 2019-0224

Landing Gear — Main Landing Gear / Piston — Inspection / Replacement / Modification

EASA Airworthiness Directive 2019-0224 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Fokker F28 Mark 0070 and Mark 0100 aeroplanes. It addresses inspection, replacement, and modification requirements for main landing gear (MLG) pistons, specifically parts with P/N 41141-3, 41141-5, and 41141-7, to prevent cracking and potential landing gear failure. The directive mandates actions to ensure the continued airworthiness of affected landing gear components.

Sep 6, 2019
Airworthiness DirectiveMaintenanceSafety MgmtFokker F28Fokker F28 Mark 0070Fokker F28 Mark 0100

EASA AD 2019-0223

SUPERSEDED BY EASA AD 2022-0019

EASA Airworthiness Directive 2019-0223 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A380-841, A380-842, and A380-861 aeroplanes with specific manufacturer serial numbers. The directive mandates repetitive ultrasonic inspections of the wing outer rear spar top and bottom flanges to detect cracks that could compromise structural integrity. It applies to the 25 oldest wing sets and requires reporting of inspection results to Airbus.

Sep 6, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380

EASA AD 2019-0222

SUPERSEDED BY EASA AD 2022-0100

EASA Airworthiness Directive 2019-0222 is an airworthiness directive issued for Airbus A380 aeroplanes, specifically models A380-841, A380-842, and A380-861 with certain manufacturer serial numbers. The directive addresses cracks found in the belly fairing torsion box parts on both left-hand and right-hand sides of the fuselage. It mandates modification of these parts to ensure continued airworthiness and safety.

Sep 6, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380

EASA AD 2019-0099R2

SUPERSEDED BY EASA AD 2024-0118

EASA Airworthiness Directive 2019-0099R2 is an updated safety directive addressing the inspection and operational limitations of Rolls-Royce Trent 1000 series engines installed on Boeing 787 aircraft. It focuses on high pressure turbine (HPT) blades with specific part numbers KH10575 and KH64485, requiring repetitive borescope inspections to detect axial cracking and imposing flight cycle limits to prevent engine failure. This directive aims to mitigate risks of in-flight engine shutdown due to blade deterioration.

Sep 6, 2019
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg TRENT 1000Boeing 787

EASA AD US-2019-16-05

SUPERSEDED BY FAA AD 2024-15-03

FAA Airworthiness Directive 2019-16-05 is a final rule applicable to all Boeing Model 777 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 and applicable corrective actions. This directive aims to mitigate the risk of flight control obstruction or unintended inputs caused by seat movement during critical flight phases.

Sep 6, 2019
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 777

EASA AD 2019-0221

Flight Controls — Rudder Pedal Control System — Inspection / Modification

EASA Airworthiness Directive 2019-0221 is an official regulatory document addressing the rudder pedal control system on Airbus Defence and Space C-212 aeroplanes. It applies to specific C-212 variants and targets rudder pedal support boxes and shafts with certain part numbers. The directive mandates inspections and modifications to ensure the structural integrity of the rudder pedal system.

Sep 5, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Defence & Space C-212Airbus Defence and Space C-212

EASA AD US-2019-16-10

Stabilizers - Horizontal Stabilizer Pivot Pin Assemblies - Inspection

Federal Aviation Administration Airworthiness Directive 2019-16-10 is a final rule addressing certain Boeing Company Model 787-8 airplanes. It mandates a one-time inspection of the horizontal stabilizer pivot pin assemblies to check for misalignment and incorrect gapping, with required corrective actions if issues are found. This directive aims to ensure the integrity of the horizontal stabilizer pivot pin assemblies to maintain safe flight control.

Sep 5, 2019
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 787Boeing 787-8

EASA AD US-2019-16-12

Wings - Vertical Stiffeners - Installation / Replacement

Airworthiness Directive 2019-16-12 is a final rule issued by the Federal Aviation Administration (FAA) addressing The Boeing Company Model 737-100, -200, -200C, -300, -400, and -500 series airplanes. It mandates replacement of vertical stiffeners at left and right buttock line 6.15 on the rear spar of the wing center section, along with installation of angle and bonding jumpers, brackets, sealant, and paint. This directive responds to identified cracks in vertical stiffeners and potential ignition sources in the fuel tank due to degraded fault current bonding paths.

Sep 5, 2019
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 737Boeing 737-100Boeing 737-200Boeing 737-200CBoeing 737-300Boeing 737-400Boeing 737-500

EASA AD 2019-0215

SUPERSEDED BY EASA AD 2021-0173

EASA Airworthiness Directive 2019-0215 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A330 freighter aircraft converted from passenger versions using EASA Supplemental Type Certificates 10063798 and 10063795. The directive addresses the inspection and replacement of flexible hoses in the courier area oxygen distribution system to prevent oxygen leakage. It applies to specific part numbers of flexible hoses installed in the courier area oxygen system on these converted A330 freighter aircraft.

Sep 4, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A330

EASA AD 2019-0218

Fuel — Fuel Tank Connection Hoses — Replacement

EASA Airworthiness Directive 2019-0218 is an airworthiness directive addressing fuel tank connection hoses on Diamond Aircraft Industries GmbH DA 42, DA 42 M, DA 42 NG, and DA 42 M-NG aeroplanes. It targets specific fuel tank connection hoses with part number D4D-2817-10-70 that were found to be defective due to dissolved rubber components. The directive mandates replacement of these affected hoses to ensure continued safe operation of the aircraft.

Sep 3, 2019
Airworthiness DirectiveMaintenanceSafety MgmtDiamond Aircraft Industries DA 42Diamond Aircraft Industries GmbH DA 42Diamond Aircraft Industries GmbH DA 42 MDiamond Aircraft Industries GmbH DA 42 NGDiamond Aircraft Industries GmbH DA 42 M-NG

EASA AD 2019-0216

SUPERSEDED BY EASA AD 2020-0232

EASA Airworthiness Directive 2019-0216 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all Airbus A380-841, A380-842, and A380-861 aeroplanes. It mandates compliance with the Airbus A380 Airworthiness Limitations Section Part 2 Revision 08, which includes damage tolerant airworthiness limitation items. This directive ensures the continued airworthiness of these aircraft by requiring updated maintenance tasks and intervals.

Sep 2, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380Airbus A380-841Airbus A380-842Airbus A380-861

EASA AD 2019-0217

SUPERSEDED BY EASA AD 2022-0105

EASA Airworthiness Directive 2019-0217 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all Airbus A380-841, A380-842, and A380-861 aeroplanes. It mandates compliance with the updated Airbus A380 Airworthiness Limitations Section (ALS) Part 1, Revision 11, which includes safe life airworthiness limitation items and maintenance tasks. This directive ensures continued airworthiness by enforcing replacement of components before exceeding life limits and updating maintenance programs accordingly.

Sep 2, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380Airbus A380-841Airbus A380-842Airbus A380-861

EASA AD DCA-750XL-38A

Flap Assembly Screw Jack — Inspection

The Airworthiness Directive DCA/750XL/38A Flap Assembly Screw Jack – Inspection issued by the Civil Aviation Authority of New Zealand mandates inspection of flap screw jack assemblies on Pacific Aerospace Limited 750XL aircraft, specifically serial numbers 101 through 215, 220, 8001, and 8002, as well as spare parts with part numbers 11-45621-1 and 11-45622-1. This directive addresses potential incorrect assembly of the flap screw jack bearing retainer and stop, which could lead to fatigue failure. Compliance with the inspection and corrective actions outlined in Pacific Aerospace Mandatory Service Bulletin PACSB/XL/117 issue 2 is required.

Aug 30, 2019
Airworthiness DirectiveMaintenanceSafety MgmtNzskydive 750XLPacific Aerospace 750XL

EASA AD DCA-750XL-39

Fuel Condition Lever — Inspection

Airworthiness Directive DCA/750XL/39 is issued by the Civil Aviation Authority of New Zealand and applies to Pacific Aerospace Limited 750XL aircraft with serial numbers 101 through 216, 220, 8001, and 8002. This directive mandates inspection and adjustment of the fuel condition lever to prevent inadvertent movement into the cut-off position when ground idle is selected. The directive references Pacific Aerospace Mandatory Service Bulletin PACSB/XL/111 issue 1 dated 18 June 2019 for detailed instructions.

Aug 30, 2019
Airworthiness DirectiveMaintenanceSafety MgmtNzskydive 750XLPacific Aerospace 750XL

EASA AD 2019-0214

Wings — Trailing Edge Flap Track #2 and #5 Supports — Modification

EASA Airworthiness Directive 2019-0214 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 trailing edge flap track #2 and #5 supports on both left-hand and right-hand wings. The directive mandates modifications to these flap track supports to ensure continued airworthiness and safe operation of the affected aircraft.

Aug 30, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380Airbus A380-841Airbus A380-842Airbus A380-861

EASA AD US-2019-14-12

Flight Controls - Main Slat Track Assemblies - Inspection

Federal Aviation Administration Airworthiness Directive 2019-14-12 is a final rule addressing certain Boeing 737-8 and 737-9 airplanes. It mandates inspection and maintenance record checks of main slat track assemblies due to concerns about hydrogen embrittlement affecting their structural integrity. This directive aims to prevent potential slat failure that could jeopardize flight safety.

Aug 29, 2019
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 737Boeing 737-8Boeing 737-9

EASA AD 2019-0213

Hydraulic Power - Hydraulic Pumps - Inspection / Replacement

EASA Airworthiness Directive 2019-0213 is an official regulatory document addressing hydraulic pumps installed on Leonardo S.p.A. AW109SP helicopters. It mandates inspection and replacement of specific hydraulic pumps with Part Number 109-0760-42-103, which are not eligible for installation, to ensure continued airworthiness and safety of the helicopters.

Aug 29, 2019
Airworthiness DirectiveMaintenanceSafety MgmtLeonardo S.P.A. Helicopters A109Leonardo S.P.A. Helicopters A119Leonardo AW109SP

EASA AD 2019-0200R1

SUPERSEDED BY EASA AD 2023-0058

EASA Airworthiness Directive 2019-0200R1 is an amendment addressing the airworthiness limitations for Dassault Mystère-Falcon 20-( )5 series aeroplanes. It mandates compliance with updated maintenance tasks and life limits as specified in the Dassault Mystère-Falcon 20 Aircraft Maintenance Manual Chapter 5-40, Revision 13. This directive excludes aircraft that have incorporated the Dassault Mystère-Falcon 20 Supplemental Structural Inspection Program into their maintenance programs.

Aug 29, 2019
Airworthiness DirectiveMaintenanceSafety MgmtDassault Mystère-Falcon 20Dassault Mystère-Falcon 20-( )5