EASA Regulations & Airworthiness Directives

Browse 5,166 EASA regulations with AI-powered summaries.

Aircraft:AllAirbus A320286Airbus A321285Airbus A319253Airbus A350224Airbus A330221Airbus A318189Airbus A380182Boeing 737175Airbus A340141Airbus A350-941134Airbus BD-500 (A220 Series)123Airbus Helicopters AS 332119Airbus Helicopters EC 225116Airbus Helicopters SA 330116Boeing 787116Show all...

EASA AD 2020-0173

Aug 5, 2020

Time Limits / Maintenance Checks – Certification Maintenance Requirements and Airworthiness Limitations – Amendment

EASA Airworthiness Directive 2020-0173 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting ATR 72-101, ATR 72-102, ATR 72-201, ATR 72-202, ATR 72-211, ATR 72-212, and ATR 72-212A aeroplanes. It mandates compliance with updated airworthiness limitations and certification maintenance requirements as specified in the ATR 72 Time Limits Document Revision 17. This directive ensures continued safe operation by enforcing life limits and maintenance tasks for critical components.

Airworthiness DirectiveSuperseded
  • ATR ATR72
  • ATR 72-101
  • ATR 72-102
  • ATR 72-201
  • ATR 72-202
  • ATR 72-211
  • ATR 72-212
  • ATR 72-212A

EASA AD 2020-0174

Aug 5, 2020

Wings – Outer Flaps and Tabs – Identification/ Inspection (Improper Heat Treatment) / Replacement (Wrong Material)

EASA Airworthiness Directive 2020-0174 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes. It addresses structural concerns related to outer flaps and tabs that were manufactured with improper heat treatment or wrong materials. The directive mandates inspections and corrective actions to ensure continued airworthiness of these aircraft.

Airworthiness DirectiveSuperseded
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2020-0172

Aug 3, 2020

Wings — Lower Skin Covers at Rib Bays — Inspection

EASA Airworthiness Directive 2020-0172 is an airworthiness directive addressing inspection requirements for Airbus A340-541, A340-542, A340-642, and A340-643 aeroplanes. It mandates inspections of the wing lower skin covers at specific rib bays on both left-hand and right-hand wings to detect cracks that could compromise structural integrity. The directive applies to certain manufacturer serial numbers as identified in the associated Airbus Service Bulletin.

Airworthiness Directive
  • Airbus A340541542642643

EASA AD 2020-0141R1

Jul 30, 2020

Main Rotor Drive — Main Gearbox Freewheel Shafts — Replacement ; Placards and Markings — ENG1 Training Idle Switch — Installation / Operational Restriction

EASA Airworthiness Directive 2020-0141R1 is an updated regulatory requirement affecting Airbus Helicopters AS 332 L2 models. It addresses the replacement of main gearbox freewheel shafts and installation of placards related to the ENG1 Training Idle switch to impose operational restrictions during flight. The directive aims to ensure continued airworthiness and safe operation of helicopters equipped with specific main gearbox configurations.

Airworthiness Directive
  • Airbus Helicopters SA 330
  • Airbus Helicopters AS 332
  • Airbus Helicopters EC 225
  • Airbus Helicopters AS 332 L2

EASA AD 2017-0198-CN

Jul 29, 2020

CANCELLED : Engine Fuel and Control — Engine Electronic Controller Firebox Assembly — Replacement

EASA Airworthiness Directive 2017-0198-CN is a cancellation notice for the previous directive concerning the replacement of the Engine Electronic Controller (EEC) firebox assembly on Rolls-Royce Deutschland BR700-710 series engines. This directive affects BR700-710A2-20 and BR700-710C4-11 engines installed on aircraft such as the Gulfstream GV-SP (G500, G550) and Bombardier BD-700 series. The cancellation reflects updated findings that the previously mandated replacement is no longer necessary.

Airworthiness Directive
  • Rolls-Royce Deutschland Ltd & Co Kg BR700-710
  • Gulfstream GV-SP
  • Bombardier BD-700

EASA AD 2020-0168R1

Jul 29, 2020

Equipment / Furnishings — Pilot Seat Belt Nuts — Inspection / Replacement

EASA Airworthiness Directive 2020-0168R1 is an updated regulatory requirement addressing the inspection and replacement of pilot seat belt nuts on Dassault Mystère-Falcon 900, Falcon 900EX, Falcon 2000, and Falcon 2000EX aircraft. The directive mandates detailed inspections and corrective actions for seat belt attaching point nuts with Part Number 142 series to ensure flight crew safety. It applies to specific manufacturer serial numbers as identified in Dassault service bulletins.

Airworthiness Directive
  • Dassault Falcon 2000
  • Dassault Falcon 900EX
  • Dassault Mystère-Falcon 900
  • Dassault Mystère-Falcon 900
  • Dassault Falcon 2000EX

EASA AD 2020-0170R1

Jul 29, 2020

Superseded by EASA ADR 2023-0025

EASA Airworthiness Directive Record 2023-0025 is an explanatory statement regarding the absence of an Airworthiness Directive (AD) document for the Airbus A400M aircraft. Since there are no Airbus A400M aeroplanes in civil service, no public AD exists. This record serves as an informational notice to military airworthiness authorities and design approval holders, recommending that military authorities issue their own ADs for the affected aircraft.

Other
  • Airbus Military A400M
  • Airbus A400M

EASA SIB SAFO20013

Jul 29, 2020

Textron Aviation Inc. (Cessna) Single Engine Aeroplanes - Right-Hand Control Wheel Removal for Skydiving Operations

The Safety Alert for Operators SAFO 20013 issued by the U.S. Federal Aviation Administration addresses the removal of the right-hand control wheel on Textron Aviation Inc. (Cessna) single-engine aeroplanes used in skydiving operations. It warns against leaving the associated right-side control tube protruding from the instrument panel after removing the control wheel, as this poses a serious safety hazard. The affected aircraft specifically include Cessna single-engine, dual-control models such as the Cessna P206A.

Safety Information Bulletin

EASA AD 2020-FATA-01020A-11

Jul 28, 2020

NOT ADOPTED - EASA DECISION ATTACHED

The document titled NOT ADOPTED - EASA DECISION ATTACHED is an EASA decision regarding the non-adoption of Russian Federation Federal Air Transport Agency (FATA) Airworthiness Directives AD 2020-FATA-01020A-11 and AD 2021-FATA-01020A-02. These directives concern repetitive inspections and maintenance of the stabilizer trimming mechanism attachment bracket with Part Number 8-28-Ц-ОСТ31138-80. EASA decided not to adopt these FATA ADs and instead requires mandatory repetitive detailed visual inspections and replacement of the affected parts to ensure airworthiness.

Agency Decision
  • Irkut Corporation Jsc RRJ-95

EASA SIB 2020-13

Jul 28, 2020

Provision of Groundhandling Services at Aerodromes

EASA Safety Information Bulletin 2020-13 provides guidance on the provision of groundhandling services at aerodromes, particularly in the context of the COVID-19 pandemic's impact on flight operations and groundhandling businesses. It addresses the challenges faced by groundhandling service providers due to suspended flights and emphasizes the importance of safe and efficient groundhandling as aviation recovers. The bulletin applies to competent authorities and aerodrome operators and does not target specific aircraft or engine types.

Safety Information Bulletin

EASA AD 2020-0171

Jul 28, 2020

Rotors – Main Gearbox Oil Cooling Fan – Inspection / Replacement

EASA Airworthiness Directive 2020-0171 is an airworthiness directive issued for Airbus Helicopters SA 330 J helicopters. It addresses the risk of main gearbox (MGB) oil cooling fan rotor shaft bearing degradation that could lead to rotor burst and damage to critical hydraulic pipes and flight controls. The directive mandates inspections and replacement of specific MGB oil cooling fan rotor shaft bearings to ensure continued safe operation.

Airworthiness DirectiveSuperseded
  • Airbus Helicopters SA 330
  • Airbus Helicopters AS 332
  • Airbus Helicopters EC 225
  • Airbus Helicopters SA 330 J

EASA AD 2020-0166

Jul 27, 2020

Fuselage — Seat Track Extremities — Inspection / Repair

EASA Airworthiness Directive 2020-0166 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A350-941 and A350-1041 aeroplanes. It mandates inspection and potential repair of seat track extremities located between specific fuselage frames to address a structural deficiency. The directive applies to aircraft identified by manufacturer serial numbers as specified in Airbus Service Bulletin A350-53-P061.

Airworthiness Directive
  • Airbus A3509411041

EASA AD BR-2020-07-02

Jul 24, 2020

Engine Fuel & Control - Full Authority Digital Engine Control - Software Update

Brazilian Airworthiness Directive AD No. 2020-07-02 is a regulatory document issued by the Agência Nacional de Aviação Civil (ANAC) that mandates a software update for the Full Authority Digital Engine Control (FADEC) systems installed on various Yaborã Indústria Aeronáutica S.A. aircraft models including EMB-135 and EMB-145 series equipped with specific FADEC part numbers. The directive addresses safety concerns related to the Automatic Takeoff Thrust Control System (ATTCS) calculations during single-engine and anti-ice operations.

Airworthiness Directive
  • Embraer EMB-135
  • Embraer EMB-145

EASA AD 2020-0165

Jul 23, 2020

Landing Gear — Nose Landing Gear Main Fitting — Replacement [Reduced Life Limit]

EASA Airworthiness Directive 2020-0165 is an airworthiness directive addressing the nose landing gear main fitting (part number 50-3751048-00) on Airbus A318, A319, A320, and A321 aeroplanes. It applies to specific serial numbers of the affected parts and mandates replacement or life limit reductions due to potential sub-surface cavities caused by improper oil removal during production. The directive affects all manufacturer serial numbers of the listed Airbus models.

Airworthiness Directive
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2020-0164

Jul 22, 2020

Fuselage — Pylon Skin — Inspection

EASA Airworthiness Directive 2020-0164 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus Helicopters EC 175 B models with specific serial numbers 5018, 5023, 5026, and 5037. The directive mandates inspection of the tail rotor pylon right-hand side centre skin for potential damage to the honeycomb panel following retrofit installations. This inspection aims to ensure the structural integrity of the pylon and prevent possible safety hazards.

Airworthiness Directive
  • Airbus Helicopters EC175
  • Airbus Helicopters EC 175 B

EASA AD US-2020-14-02

Jul 21, 2020

[Correction] Fuselage - Bulkhead Structure - Inspection

Correction to Airworthiness Directive 2020-14-02 issued by the Federal Aviation Administration (FAA) affecting all Boeing 747 series airplanes including models 747-100 through 747SP. The directive addresses inspection requirements for the fuselage bulkhead structure at body station 2598 to detect and repair fatigue cracking. This correction fixes previously incorrect AD and amendment numbers published in the original document.

Airworthiness Directive
  • Boeing 747

EASA AD 2020-0090R1

Jul 21, 2020

Indicating / Recording Systems – Integrated Control Panels – Modification; Airplane Flight Manual – Abnormal / Normal Procedures Sections – Amendment

EASA Airworthiness Directive 2020-0090R1 is an amendment addressing safety concerns on Airbus A350-941 and A350-1041 aeroplanes related to inadvertent liquid spillage on the ENG START panel or Electronic Centralized Aircraft Monitoring Control Panel. This directive mandates modifications and operational changes to prevent uncommanded engine in-flight shutdowns caused by liquid contamination. It applies to all affected A350 aircraft except those with specific water-resistant modifications.

Airworthiness DirectiveSuperseded
  • Airbus A3509411041

EASA AD 2020-0162

Jul 21, 2020

Pneumatic – Pylon / Wing Interface Bleed Duct and Fuel Pipe – Inspection

EASA Airworthiness Directive 2020-0162 is an airworthiness directive issued for Airbus A380-841, A380-842, and A380-861 aeroplanes. It addresses a safety issue involving the bleed duct and fuel pipe at the pylon/wing interface, where a bracket weld failure could cause contact between these components. The directive mandates inspection and corrective actions to prevent potential fire hazards.

Airworthiness DirectiveSuperseded
  • Airbus A380

EASA AD 2020-0161-E

Jul 17, 2020

Engine — Stage 3 Turbine Wheels — Replacement

EASA Airworthiness Directive 2020-0161-E is an emergency directive addressing the replacement of Stage 3 turbine wheels on SAFRAN Helicopter Engines ASTAZOU XIV B and XIV H engines. These engines are commonly installed on Airbus Helicopters SA 319 B (Alouette III) and SA 342 J (Gazelle) models. The directive targets specific turbine wheels with part number 0265257050 and certain serial numbers due to detected material defects.

Airworthiness Directive
  • Safran ASTAZOU XIV
  • Airbus Helicopters SA 319 B
  • Airbus Helicopters SA 342 J

EASA AD CF-2020-25

Jul 17, 2020

Time Limits / Maintenance Checks – Airworthiness Limitations - Implementation

Airworthiness Directive CF-2020-25 is issued by Transport Canada and applies to Airbus Canada Limited Partnership aeroplanes, specifically models BD-500-1A10 and BD-500-1A11. This directive mandates updates to the aircraft maintenance schedules to incorporate the latest Airworthiness Limitations as published in Issue No. 011.00 of the AWL document. It ensures continued airworthiness by enforcing compliance with updated maintenance tasks and intervals.

Airworthiness DirectiveSuperseded
  • Airbus BD-500 (A220 Series)
  • Airbus Canada BD-500-1A10
  • Airbus Canada BD-500-1A11