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EASA Regulations & Airworthiness Directives

Browse 176 EASA regulations with AI-powered summaries.

Aircraft:AllAirbus A320281Airbus A321277Airbus A319247Airbus A350216Airbus A330211All198Airbus A318186Airbus A380178Boeing 737172Airbus A340140Airbus A350-941126Airbus BD-500 (A220 Series)119Airbus Helicopters AS 332118Airbus Helicopters EC 225115Airbus Helicopters SA 330115Show all...
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EASA AD 2018-0118R1

SUPERSEDED BY EASA AD 2020-0012

EASA Airworthiness Directive 2018-0118R1 is an updated safety directive addressing inspection and maintenance requirements for the auxiliary wing landing gear doors on Airbus A380-841, A380-842, and A380-861 aircraft. It mandates repetitive inspections of specific hinge fittings prone to fatigue cracking and outlines corrective actions to maintain structural integrity. This directive applies to all manufacturer serial numbers of the affected Airbus A380 models.

Jun 11, 2018
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380

EASA AD 2018-0117R1

Exhaust — Inner J-Ring and V-Groove Interface — Inspection

EASA Airworthiness Directive 2018-0117R1 is an amendment addressing inspection requirements for the inner J-ring and V-groove interface on Airbus A380-861 aeroplanes powered by GP7200 engines. It mandates repetitive detailed inspections of the inner J-ring to detect wear damage that could compromise the structural integrity of the engine thrust reverser unit and fan exhaust cowl. The directive applies to all manufacturer serial numbers of the Airbus A380-861 and references Airbus Service Bulletin A380-78-8012 for inspection procedures.

Jun 8, 2018
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380

EASA AD 2018-0121

Engine — Low Pressure Turbine Blades — Replacement

EASA Airworthiness Directive 2018-0121 is an official directive addressing the replacement of low pressure turbine blades on Rolls-Royce RB211 Trent 970-84, 972-84, and 972E-84 engines, commonly installed on Airbus A380 aircraft. The directive mandates inspection and replacement of affected turbine blades that were subject to cleaning with OMat 198 during overhaul. This AD aims to prevent engine failures caused by internal corrosion leading to uncommanded in-flight engine shutdowns.

Jun 1, 2018
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg RB211 TRENT 900Airbus A380

EASA AD 2018-0116

SUPERSEDED BY EASA AD 2020-0239

EASA Airworthiness Directive 2018-0116 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 inspections of the inboard and outboard elevator hinges and actuator fittings to detect bushing migration and other potential structural issues. The directive aims to ensure the continued structural integrity and safe control of the aircraft elevators.

May 29, 2018
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380Airbus A380-841Airbus A380-842Airbus A380-861

EASA AD 2018-0119

Wings — Outboard Flaps Skin — Inspection

EASA Airworthiness Directive 2018-0119 is an airworthiness directive issued by EASA concerning Airbus A380-841, A380-842, and A380-861 aeroplanes. It mandates inspection of the outboard flaps skin, specifically the upper and lower skin surfaces between certain ribs on both left-hand and right-hand outer flaps. The directive addresses potential structural issues related to incorrect repair zoning in the aircraft's Structural Repair Manual.

May 29, 2018
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380

EASA AD 2018-0100

SUPERSEDED BY EASA AD 2020-0129

EASA Airworthiness Directive 2018-0100 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A380-841, A380-842, and A380-861 aeroplanes. It addresses issues related to the bleed air overheat detection system, specifically concerning insulation mufflers and sleeves installed in the wings, pylons, and certain pneumatic tubing in the nose and center fuselage. The directive mandates modifications to replace affected parts with improved components to ensure continued airworthiness.

Apr 25, 2018
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380

EASA AD 2018-0099

Fuel — Trim Tank Vent Pipes — Inspection

EASA Airworthiness Directive 2018-0099 is an airworthiness directive issued for Airbus A380-841, A380-842, and A380-861 aeroplanes. It mandates a one-time borescope inspection of the forward trim tank vent pipes to detect any blockages that could affect the structural integrity of the horizontal tail plane. The directive also requires corrective actions and detailed inspections if blockages are found.

Apr 24, 2018
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380

EASA AD 2018-0097

SUPERSEDED BY EASA AD 2019-0072

EASA Airworthiness Directive 2018-0097 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 2, Revision 06 and variation 6.1, which contain damage tolerant airworthiness limitation items. This directive ensures continued airworthiness by enforcing maintenance tasks and corrective actions as specified in the ALS.

Apr 24, 2018
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380

EASA AD 2018-0096

SUPERSEDED BY EASA AD 2019-0217

EASA Airworthiness Directive 2018-0096 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 updated safe life airworthiness limitations as specified in Airbus A380 Airworthiness Limitations Section Part 1 Revision 10. This directive ensures continued airworthiness by enforcing replacement of life-limited parts and updating maintenance programs accordingly.

Apr 24, 2018
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380Airbus A380-841Airbus A380-842Airbus A380-861

EASA AD 2018-0098

Time Limits / Maintenance Checks — Airworthiness Limitations Section — Part 3 — Certification Maintenance Requirements — Amendment

EASA Airworthiness Directive 2018-0098 is an amendment concerning the Airbus A380-841, A380-842, and A380-861 aeroplanes. It updates the airworthiness limitations related to Certification Maintenance Requirements as specified in Airbus A380 Airworthiness Limitations Section Part 3, Revision 06. This directive mandates compliance with updated maintenance tasks to ensure continued airworthiness of these aircraft.

Apr 24, 2018
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380Airbus A380-841Airbus A380-842Airbus A380-861

EASA AD 2018-0074

Oxygen - Main Passenger Oxygen Distribution Line Flexible Hoses - Replacement

EASA Airworthiness Directive 2018-0074 is an airworthiness directive addressing the replacement of main passenger oxygen distribution line flexible hoses on Airbus A380-841, A380-842, and A380-861 aeroplanes. It targets specific flexible hoses installed in the upper deck crossbeam and framework areas that may be prone to rupture due to installation issues. The directive applies to all manufacturer serial numbers of these Airbus A380 models.

Apr 5, 2018
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380

EASA AD 2018-0054

Flight Controls — Trimmable Horizontal Stabilizer Actuator — Modification

EASA Airworthiness Directive 2018-0054 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A380-841, A380-842, and A380-861 aeroplanes. It addresses a design weakness in the trimmable horizontal stabilizer actuator (THSA) related to the secondary load path, which could lead to loss of control of the aircraft. The directive mandates modification or replacement of affected THSA components to ensure continued safe operation.

Mar 9, 2018
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380Airbus A380-841Airbus A380-842Airbus A380-861

EASA AD 2016-0193R1

Engine — Low Pressure Turbine Exhaust Case and Support Assembly (Tail Bearing Housing) — Inspection / Replacement

EASA Airworthiness Directive 2016-0193R1 is an updated regulatory document addressing inspection and replacement requirements for the Low Pressure Turbine Exhaust Case and Support Assembly (Tail Bearing Housing) on Rolls-Royce RB211 Trent 900 engines, commonly installed on Airbus A380 aircraft. The directive mandates inspections to detect cracks and damage in specific turbine components and outlines corrective actions to ensure continued airworthiness.

Feb 28, 2018
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg RB211 TRENT 900Airbus A380

EASA AD 2017-0249

Landing Gear — Nose Landing Gear Components — Replacement [Life Limit]

EASA Airworthiness Directive 2017-0249 is an airworthiness directive issued by the European Union Aviation Safety Agency concerning the Airbus A380-841, A380-842, and A380-861 aeroplanes. It addresses the replacement of certain nose landing gear (NLG) components, specifically main fittings and sliding tubes, due to a manufacturing issue involving improper preparation of 300M material. The directive sets reduced life limits for these affected parts to prevent potential structural failure and nose landing gear collapse.

Dec 14, 2017
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380Airbus A380-841Airbus A380-842Airbus A380-861

EASA SIB 2014-29

WITHDRAWN: Comments received indicate the need for a review of applicable recommendation

EASA Safety Information Bulletin 2014-29 provides clarification on the minimum cabin crew requirements for twin aisle aeroplanes including Airbus A300, A310, A330, A340, A380, A350 series, Boeing 747, 767, 777, 787, DC10, MD11 series, and Lockheed L1011 series. It explains the operational and certification regulations governing cabin crew numbers, emphasizing the need for at least one cabin crew member per emergency exit on twin aisle aircraft due to evacuation management challenges. The bulletin addresses misunderstandings arising from Commission Regulation (EU) No 965/2012 and highlights the importance of adequate cabin crew supervision for passenger safety during evacuations.

Oct 24, 2014
Safety Information BulletinFlight OpsSafety MgmtAirbus A300Airbus A310Airbus A330Airbus A340Airbus A380Airbus A350Boeing 747Boeing 767Boeing 777Boeing 787McDonnell Douglas DC10McDonnell Douglas MD11Lockheed L1011

EASA SIB 2009-06R1

WITHDRAWN - Rockwell-Collins GPS Receiver — Date Roll-Over Anomaly

EASA Safety Information Bulletin 2009-06R1 is an informational bulletin addressing a software anomaly in certain Rockwell-Collins Multi-Mode Receivers (MMR) installed on various Boeing, Airbus, and Bombardier aircraft models. The anomaly causes a date roll-over error at midnight on 20/21 June 2009, resulting in the receiver reporting an incorrect date approximately 19.7 years off. Affected aircraft include Boeing 737, 747, 757, 767, 777, Airbus A300-600, A310, A320, A330, A340, A380, and Bombardier CL-600 series.

May 26, 2009
Safety Information BulletinMaintenanceSafety MgmtBoeing 737Boeing 747Boeing 757Boeing 767Boeing 777Airbus A300-600Airbus A310Airbus A320Airbus A330Airbus A340Airbus A380Bombardier CL-600