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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 US-2020-21-02

KIDDE AEROSPACE & DEFENSE - Cargo Fire Extinguisher Halon Bottles - Inspection / Replacement

The Federal Aviation Administration's Airworthiness Directive 2020-21-02 addresses Kidde Aerospace & Defense cargo fire extinguisher halon bottles installed on various transport category airplanes, including Boeing models. This directive responds to reports of low charge pressure in certain halon bottles used in cargo compartments, which could compromise fire suppression effectiveness.

Nov 12, 2020
Airworthiness DirectiveMaintenanceSafety MgmtBoeing

EASA AD US-2020-22-18

Engine - Propeller Gearbox Shaft and Carrier Assembly - Usage Hours Assignment / Replacement

The Federal Aviation Administration's Airworthiness Directive 2020-22-18 addresses all Rolls-Royce Corporation AE 2100A, AE 2100D2, AE 2100D2A, and AE 2100P turboprop engines. This directive responds to a fatigue crack issue found in the propeller gearbox shaft and carrier assembly that caused high vibration during manufacturer testing. It mandates usage hour assignment and replacement of these assemblies before exceeding newly established life limits to ensure continued airworthiness.

Nov 11, 2020
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Corporation (Usa) AE 2100

EASA AD 2020-0251

Fuselage — Central Fuselage Frames 21, 23 and 24 / Wing Fitting Attachments — Inspections; Time Limits / Maintenance Checks — Airworthiness Limitations List — Amendment

The document titled 'Fuselage — Central Fuselage Frames 21, 23 and 24 / Wing Fitting Attachments — Inspections; Time Limits / Maintenance Checks — Airworthiness Limitations List — Amendment' is an airworthiness directive concerning the AIRBUS DEFENCE & SPACE S.A. CN-235 aircraft. It addresses inspection requirements and time limits for central fuselage frames and wing fitting attachments, as well as updates to the maintenance checks listed in the Airworthiness Limitations List. The amendment aims to ensure continued structural integrity and airworthiness of the affected aircraft components.

Nov 11, 2020
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Defence & Space CN-235

EASA AD US-2020-22-07

Nacelle / Pylons - Excessive Pylon Pitch Vibrations - Rotorcraft Flight Manual - Revision

The Federal Aviation Administration's Airworthiness Directive 2020-22-07 is a final rule affecting all Bell Textron Inc. Model 412, 412CF, and 412EP helicopters. This directive addresses an unsafe condition related to excessive pylon pitch vibrations that have caused cracked main gearbox support cases. The AD mandates revisions to the Rotorcraft Flight Manual to include cautions for pilots regarding vibration events during specific flight conditions.

Nov 11, 2020
Airworthiness DirectiveFlight OpsSafety MgmtBell Textron Inc. (Bti) 412Bell Textron Inc. 412Bell Textron Inc. 412CFBell Textron Inc. 412EP

EASA AD 2020-0250

Powerplant — Engine Mount Shackle — Replacement

EASA Airworthiness Directive 2020-0250 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A319, A320, and A321 aeroplanes with specific forward engine mount shackle assemblies. It addresses potential premature wear and failure of the forward engine mount shackles, which could lead to engine detachment in flight. The directive applies to certain part numbers of engine mount shackles and requires replacement with serviceable parts.

Nov 11, 2020
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A319Airbus A320Airbus A321

EASA AD 2020-0224R1

Tail Rotor — Tail Rotor Blades — Inspection / Replacement / Modification

EASA Airworthiness Directive 2020-0224R1 is a regulatory document addressing inspection, replacement, and modification requirements for tail rotor blades on Airbus Helicopters AS 350 and AS 355 models. It targets specific pre-modification 075580 tail rotor blades identified by certain part numbers due to risks of debonding of leading edge protection shields. The directive mandates inspections and replacement to ensure continued airworthiness and safe operation of affected helicopters.

Nov 11, 2020
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters AS 350Airbus Helicopters EC 130Airbus Helicopters AS 355

EASA AD US-2020-18-01

Fuselage - Forward Cabin Doorposts at the Strut Attach Fitting - Repetitive Inspections

Fuselage - Forward Cabin Doorposts at the Strut Attach Fitting - Repetitive Inspections is a Federal Aviation Administration (FAA) Airworthiness Directive (AD 2020-18-01) that applies to multiple Textron Aviation Inc. airplane models including various Cessna 172, 182, 206, 207, and 210 series aircraft. This AD mandates repetitive inspections of the lower area of the forward cabin doorposts at the strut attach fitting to detect cracks and requires repairs if cracks are found. The directive addresses a critical structural safety concern related to potential wing strut attach point failure.

Nov 10, 2020
Airworthiness DirectiveMaintenanceSafety MgmtTextron Aviation 172 (Skyhawk)Textron Aviation 172RGTextron Aviation 182 (Skylane)Textron Aviation 206Textron Aviation U206 (Super Skywagon)Textron Aviation 207 (Skywagon)Textron Aviation 210 (Centurion)Textron Aviation F172Textron Aviation F182Textron Aviation FR172 (Reims Rocket)Textron Aviation P206Textron Aviation TP206 (Super Skylane)Textron Aviation R172 (Hawk XP)Textron Aviation Cessna 172Textron Aviation Cessna 182Textron Aviation Cessna 206Textron Aviation Cessna 207Textron Aviation Cessna 210

EASA AD US-2020-23-04

SUPERSEDED BY FAA AD 2024-05-04

FAA Airworthiness Directive 2020-23-04 is a final rule addressing certain Gulfstream Aerospace Corporation Model GVII-G500 and GVII-G600 airplanes. It requires revisions to the airplane flight manual and airplane maintenance manual to include new warnings and updated maintenance procedures related to the fuel boost pump. This directive aims to mitigate the risk of fuel tank fire or explosion due to misassembled fuel boost pump impellers.

Nov 10, 2020
Airworthiness DirectiveMaintenanceSafety MgmtGulfstream Aerospace Corporation GVIIGulfstream GVII-G500Gulfstream GVII-G600

EASA AD 2020-0246

Wiring Harness — Lateral Control Rod Wiring — Inspection

EASA Airworthiness Directive 2020-0246 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus Helicopters Deutschland GmbH MBB-BK117 D-2 helicopters, specifically all serial numbers up to 20334 inclusive except for a few listed exceptions. The directive mandates inspection of the wiring harness near the lateral control rod to detect chafing and clearance issues. It also requires updating the Aircraft Maintenance Programme to include ongoing inspection tasks.

Nov 10, 2020
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters MBB-BK 117Airbus Helicopters MBB-BK117 D-2

EASA AD 2020-0245

Flight Controls — Slat Geared Rotary Actuators — Repair / Replacement

Flight Controls — Slat Geared Rotary Actuators — Repair / Replacement is a regulatory document applicable to the Airbus A330 aircraft. It addresses maintenance procedures specifically related to the repair and replacement of slat geared rotary actuators used in the flight control systems of these aircraft. The document provides guidance to ensure continued airworthiness and safe operation of the affected components.

Nov 9, 2020
OtherMaintenanceSafety MgmtAirbus A330

EASA AD 2020-0240

Engine — Intermediate Pressure Compressor Blade Kits — Introduction

EASA Airworthiness Directive 2020-0240 addresses safety concerns related to Rolls-Royce Deutschland Trent 1000 series engines installed on Boeing 787 aircraft. It focuses on the introduction of new intermediate pressure compressor blade kits and mandates repetitive inspections of specific IPC Rotor 1 and Rotor 2 blades to detect cracks. The directive applies to multiple Trent 1000 engine variants except those modified per Rolls-Royce Service Bulletin TRENT 1000 72-J941.

Nov 5, 2020
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg TRENT 1000Boeing 787

EASA AD 2020-0241

SUPERSEDED BY EASA AD 2022-0210

EASA Airworthiness Directive 2020-0241 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Rolls-Royce Deutschland Trent 1000 series engines, including models Trent 1000U0-A2 through Trent 1000-L2. This directive mandates compliance with updated maintenance tasks and life limits as specified in the Rolls-Royce Trent 1000 Time Limits Manual Revision 20 dated 01 August 2020. It ensures continued airworthiness by requiring operators to follow revised maintenance programs and replacement schedules for critical engine parts.

Nov 5, 2020
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg TRENT 1000

EASA AD 2020-0243

SUPERSEDED BY EASA AD 2022-0247

EASA Airworthiness Directive 2020-0243 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Rolls-Royce Trent 1000 series engines, including models AE3, CE3, D3, G3, H3, J3, K3, L3, M3, N3, P3, Q3, and R3. This directive mandates compliance with updated maintenance tasks and life limits as specified in the Rolls-Royce Trent 1000 Time Limits Manual Revision 16 dated 01 August 2020. It ensures continued airworthiness by requiring operators to follow the revised maintenance program and replace critical components before exceeding new life limits.

Nov 5, 2020
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg TRENT 1000

EASA AD 2020-0244

SUPERSEDED BY EASA AD 2022-0248

EASA Airworthiness Directive 2020-0244 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Rolls-Royce Deutschland Trent 7000-72 and Trent 7000-72C engines. It mandates compliance with updated maintenance tasks and life limits as specified in the Rolls-Royce Trent 7000 Time Limits Manual Revision 7 dated 10 July 2020. This directive ensures continued airworthiness by requiring operators to follow the revised maintenance program and replace critical parts within updated life limits.

Nov 5, 2020
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg TRENT 7000

EASA AD 2020-0242

SUPERSEDED BY EASA AD 2022-0259

EASA Airworthiness Directive 2020-0242 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Rolls-Royce Trent 1000 series engines, including models Trent 1000-A, -AE, -C, -CE, -D, -E, -G, and -H. The directive mandates compliance with updated maintenance tasks and life limits as specified in the Rolls-Royce Trent 1000 Time Limits Manual Revision 23 dated 01 August 2020. It ensures continued airworthiness by requiring operators to follow revised maintenance instructions and replacement schedules for critical engine components.

Nov 5, 2020
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg TRENT 1000

EASA AD 2020-0238

Airplane Flight Manual — Section Abnormal Procedures — Amendment

EASA Airworthiness Directive 2020-0238 is an amendment to the Airplane Flight Manual (AFM) Section on Abnormal Procedures for Fokker F28 Mark 0070 and Mark 0100 aeroplanes. It addresses a safety issue related to the cabin pressurization control fault procedure following an incident where a passenger door opened under residual cabin pressure after landing. This directive mandates updates to the AFM to improve the procedure and prevent similar occurrences.

Nov 4, 2020
Airworthiness DirectiveFlight OpsSafety MgmtFokker F28Fokker F28 Mark 0070Fokker F28 Mark 0100

EASA SIB AIR-20-15

Boeing 787 Airplanes - Navigation Localizer System

The Special Airworthiness Information Bulletin SAIB: AIR-20-15 is an FAA informational bulletin addressing a potential issue with the autopilot flight director system (AFDS) on Boeing 787-8, -9, and -10 airplanes. It warns that the AFDS may fail to properly capture the localizer during ILS approaches when intercepting at large angles, potentially leading to incorrect heading alignment. This bulletin provides background on the issue and references Boeing's Flight Crew Operations Manual Bulletin TBC-106 for guidance.

Nov 4, 2020
Safety Information BulletinFlight OpsSafety Mgmt

EASA AD 2020-0100R1

Equipment / Furnishings — Cargo Compartment Lining Panels — Repair / Replacement

EASA Airworthiness Directive 2020-0100R1 is an amendment addressing repair and replacement of cargo compartment lining panels made of honeycomb core material on Airbus A330, A340, A350, and A380 aeroplanes. It targets panels repaired with 'Speedpatch AF800 series' patches on both sides, which do not meet flame penetration standards, posing a fire risk. The directive applies to all manufacturer serial numbers of the affected Airbus models.

Nov 4, 2020
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A330Airbus A340Airbus A350Airbus A380

EASA AD 2020-0239

Stabilizers — Inboard and Outboard Elevator Hinges / Actuator Fittings — Inspection

EASA Airworthiness Directive 2020-0239 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting 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 structural issues that could compromise elevator connection integrity. The directive provides detailed inspection instructions and corrective actions to maintain continued airworthiness of these aircraft.

Nov 4, 2020
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380

EASA AD US-2020-22-02

Engine Fuel and Control - Hydromechanical Unit - Removal / Replacement

Federal Aviation Administration Airworthiness Directive 2020-22-02 is a final rule addressing all General Electric Company CF6-80C2 and CF6-80E1 model turbofan engines equipped with a specific hydromechanical unit (HMU). The directive mandates the removal and replacement of the HMU due to fuel coking in the HMU fuel metering valve electro-hydraulic servo valves, which has caused tailpipe fires. This AD aims to ensure continued airworthiness and safety of affected engines.

Oct 30, 2020
Airworthiness DirectiveMaintenanceSafety MgmtGeneral Electric CF6-80CGeneral Electric CF6-80E1