EASA Regulations & Airworthiness Directives

Browse 4771 EASA regulations with AI-powered summaries.

EASA AD 2020-0248

[Correction] Flight Controls — Backup Control Module — Modification / Fuel — Fuel Control and Monitoring Computer — Modification / Indicating / Recording Systems — Flight Warning Computer — Modification / Landing Gear — Braking and Steering Control Unit — Modification / Replacement / Fuselage — Circumferential and Longitudinal Joints — Modification / Wings — Leading Edge Overhang — Reinforcement

EASA Airworthiness Directive 2020-0248 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting specific Airbus A340-541 and A340-642 aeroplanes with manufacturer serial numbers 371, 383, 464, 624, 628, 698, 775, and 779. The directive mandates modifications to various aircraft systems including flight controls, fuel control and monitoring computers, flight warning computers, braking and steering control units, fuselage joints, and wing leading edge overhangs. These modifications are required to ensure continued airworthiness and address previously identified unsafe conditions.

Nov 17, 2020
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A340Airbus A340-541Airbus A340-642

EASA AD 2020-0257

Rotors Flight Control — Main Rotor Actuator — Inspection

EASA Airworthiness Directive 2020-0257 is an airworthiness directive addressing the main rotor actuator (MRA) inspection on Airbus Helicopters Deutschland GmbH MBB-BK117 C-2 and D-2 helicopters. It mandates repetitive inspections of specific main rotor actuators with part numbers B673M30A1002 or D673M30A1003 to detect cracks or damage in the piston nuts. The directive aims to ensure continued safe flight control by preventing potential loss of helicopter control.

Nov 17, 2020
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters MBB-BK 117Airbus Helicopters MBB-BK117 C-2Airbus Helicopters MBB-BK117 D-2

EASA AD 2020-0256

SUPERSEDED BY EASA AD 2022-0153

EASA Airworthiness Directive 2020-0256 is an airworthiness directive issued for Leonardo S.p.A. A109E helicopters, specifically serial numbers 11001 to 11674 inclusive. It mandates repetitive inspections and repairs of the centre fuselage frame assembly at station 1815, where cracks have been reported. The directive aims to ensure the structural integrity of affected helicopters by requiring inspections and corrective actions as per Leonardo Alert Service Bulletin 109EP-173.

Nov 17, 2020
Airworthiness DirectiveMaintenanceSafety MgmtLeonardo S.P.A. Helicopters A109Leonardo S.P.A. Helicopters A119Leonardo A109E

EASA AD 2020-0255

Equipment / Furnishings — Lower Deck Mobile Crew Rest Fire Extinguisher Bottle Outlet Tube — Replacement

EASA Airworthiness Directive 2020-0255 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A330 and A340 aeroplanes equipped with a lower deck mobile crew rest (LDMCR) fire extinguisher assembly. The directive addresses a potential issue with the halon outlet tube connection on certain fire extinguisher bottles installed in these aircraft models. It mandates replacement of the affected halon outlet tubes to ensure proper fire suppression functionality.

Nov 13, 2020
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A330Airbus A340

EASA AD 2020-0254

SUPERSEDED BY CAA UK AD G-2021-0009

SUPERSEDED BY CAA UK AD G-2021-0009 is a regulatory document concerning BAE SYSTEMS (OPERATIONS) LTD aircraft, specifically the AVRO146RJ and BAE146 models. This document has been officially replaced by the CAA UK Airworthiness Directive G-2021-0009. It pertains to airworthiness and safety requirements for these aircraft types.

Nov 13, 2020
Airworthiness DirectiveMaintenanceSafety MgmtBae Systems (Operations) AVRO146RJBae Systems (Operations) BAE146BAE SYSTEMS AVRO146RJBAE SYSTEMS BAE146

EASA AD 2020-0253

Engine — Low Pressure Compressor Blades / Discs — Inspection / Re-lubrication / Restoration

EASA Airworthiness Directive 2020-0253 is an airworthiness directive addressing Rolls-Royce Deutschland RB211 Trent 700 engines, specifically models Trent 768-60, Trent 772-60, Trent 772B-60, and Trent 772C-60, commonly installed on Airbus A330 aircraft. The directive mandates inspection, re-lubrication, and restoration of low pressure compressor blades and discs with specified part and serial numbers to prevent potential blade or disc failure. It includes instructions for repetitive on-wing ultrasonic inspections and in-shop restoration to ensure continued airworthiness.

Nov 12, 2020
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg RB211 TRENT 700Airbus A330

EASA AD 2020-0252

Fuel — Fuel Drain System — Modification

EASA Airworthiness Directive 2020-0252 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Pilatus Aircraft Ltd PC-24 aeroplanes with manufacturer serial numbers 101 to 184 inclusive. The directive mandates modifications to the fuel drain system to address safety concerns. It specifically targets the fuel drain pipe routing and installation of a drain mast to improve system performance.

Nov 12, 2020
Airworthiness DirectiveMaintenanceSafety MgmtPilatus Aircraft PC-24Pilatus PC-24

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