EASA Regulations & Airworthiness Directives

Browse 180 EASA regulations with AI-powered summaries.

Aircraft:AllAirbus A320286Airbus A321285Airbus A319253Airbus A350222Airbus A330220Airbus A318189Airbus A380182Boeing 737175Airbus A340141Airbus A350-941132Airbus BD-500 (A220 Series)123Airbus Helicopters AS 332119Airbus Helicopters EC 225116Airbus Helicopters SA 330116Boeing 787114Show all...
Filtered by: Airbus A380Clear filter

EASA AD 2018-0185

Aug 29, 2018

Superseded by EASA AD 2019-0101

EASA Airworthiness Directive 2018-0185 is an airworthiness directive addressing Rolls-Royce RB211 Trent 970-84, 972-84, and 972E-84 engines, commonly installed on Airbus A380 aircraft. The directive mandates inspections and potential replacement of specific drains mast parts to prevent cracks that could compromise the engine fire wall. This directive ensures continued airworthiness and safety of affected engines by requiring repetitive inspections and corrective actions.

Airworthiness DirectiveSuperseded
  • Rolls-Royce Deutschland Ltd & Co Kg RB211 TRENT 900
  • Airbus A380

EASA AD 2018-0171-E

Aug 6, 2018

CANCELLED - SEE EASA AD 2019-0251

EASA Airworthiness Directive 2018-0171-E is an emergency directive affecting all Airbus A380-841, A380-842, and A380-861 aeroplanes. It addresses a critical safety issue involving damage to the engine bleed air system and wing structure caused by overpressure scenarios during take-off, which could compromise structural integrity. The directive mandates updates to the Airbus A380 Airplane Flight Manual to mitigate this risk.

Airworthiness DirectiveSuperseded
  • Airbus A380841842861

EASA AD 2018-0160

Jul 25, 2018

Wings — Frame 46 Horizontal Cruciform Fittings — Inspection / Modification

EASA Airworthiness Directive 2018-0160 is an official safety directive addressing the Airbus A380-841, A380-842, and A380-861 aeroplanes. It mandates inspections and modifications of the frame 46 horizontal cruciform fittings on the wings to detect and correct fatigue cracks. The directive applies to all manufacturer serial numbers of these aircraft models.

Airworthiness Directive
  • Airbus A380841842861

EASA AD 2018-0138

Jun 28, 2018

Powerplant — Forward Engine Mount Shackle Assembly — Inspection

EASA Airworthiness Directive 2018-0138 is an official safety directive addressing Airbus A380-861 aeroplanes equipped with Engine Alliance GP7200 engines. It mandates a one-time special detailed inspection of the forward engine mount shackle assemblies and safety tabs to detect potential quality defects that could lead to engine loss in flight. The directive provides inspection instructions based on Airbus Service Bulletin A380-71-8015.

Airworthiness Directive
  • Airbus A380

EASA AD 2018-0118R1

Jun 11, 2018

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.

Airworthiness DirectiveSuperseded
  • Airbus A380

EASA AD 2018-0117R1

Jun 8, 2018

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.

Airworthiness Directive
  • Airbus A380

EASA AD 2018-0121

Jun 1, 2018

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.

Airworthiness Directive
  • Rolls-Royce Deutschland Ltd & Co Kg RB211 TRENT 900
  • Airbus A380

EASA AD 2018-0116

May 29, 2018

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.

Airworthiness DirectiveSuperseded
  • Airbus A380841842861

EASA AD 2018-0119

May 29, 2018

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.

Airworthiness Directive
  • Airbus A380

EASA AD 2018-0100

Apr 25, 2018

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.

Airworthiness DirectiveSuperseded
  • Airbus A380

EASA AD 2018-0099

Apr 24, 2018

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.

Airworthiness Directive
  • Airbus A380

EASA AD 2018-0097

Apr 24, 2018

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.

Airworthiness DirectiveSuperseded
  • Airbus A380

EASA AD 2018-0096

Apr 24, 2018

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.

Airworthiness DirectiveSuperseded
  • Airbus A380841842861

EASA AD 2018-0098

Apr 24, 2018

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.

Airworthiness DirectiveSuperseded
  • Airbus A380841842861

EASA AD 2018-0074

Apr 5, 2018

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.

Airworthiness Directive
  • Airbus A380

EASA AD 2018-0054

Mar 9, 2018

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.

Airworthiness Directive
  • Airbus A380841842861

EASA AD 2016-0193R1

Feb 28, 2018

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.

Airworthiness DirectiveSuperseded
  • Rolls-Royce Deutschland Ltd & Co Kg RB211 TRENT 900
  • Airbus A380

EASA AD 2017-0249

Dec 14, 2017

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.

Airworthiness Directive
  • Airbus A380841842861

EASA SIB 2014-29

Oct 24, 2014

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.

Safety Information Bulletin
  • Airbus A300
  • Airbus A310
  • Airbus A330
  • Airbus A340
  • Airbus A380
  • Airbus A350
  • Boeing 747
  • Boeing 767
  • Boeing 777
  • Boeing 787
  • McDonnell Douglas DC10
  • McDonnell Douglas MD11
  • Lockheed L1011

EASA SIB 2009-06R1

May 26, 2009

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.

Safety Information Bulletin
  • Boeing 737
  • Boeing 747
  • Boeing 757
  • Boeing 767
  • Boeing 777
  • Airbus A300-600
  • Airbus A310
  • Airbus A320
  • Airbus A330
  • Airbus A340
  • Airbus A380
  • Bombardier CL-600