EASA Regulations & Airworthiness Directives

Browse 5,129 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 787115Show all...

EASA AD US-2025-02-05

Feb 12, 2025

Landing Gear - Outer Cylinders - Replacement

The Federal Register document titled "Landing Gear - Outer Cylinders - Replacement" is a final rule airworthiness directive (AD 2025-02-05) issued by the FAA affecting all Boeing Model 747 series airplanes including 747-100, 747-200, 747-300, 747-400, 747SP, and 747SR variants. The AD addresses a safety issue related to improper inner diameter grinding of landing gear outer cylinders that may cause heat damage to the nose, body, and wing landing gear outer cylinders. This directive mandates the replacement of any affected outer cylinders to ensure continued airworthiness.

Airworthiness Directive
  • Boeing 747

EASA AD 2025-0037

Feb 12, 2025

Superseded by EASA AD 2025-0118

EASA Airworthiness Directive 2025-0037 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A319, A320, and A321 aeroplanes with specific Airbus modifications embodied. The directive addresses issues related to loss of synchronization between radio management panels, which can result in loss of radio communications, transponder functionality, and standby navigation. It requires amendments to the Aircraft Flight Manual to include procedures to manage these failures.

Airworthiness Directive
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2025-0035

Feb 12, 2025

Superseded by EASA AD 2025-0139

EASA Airworthiness Directive 2025-0035 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A350-941 and A350-1041 aeroplanes, excluding those with Airbus modification 116830 incorporated in production. The directive addresses issues related to hydraulic engine driven pumps and requires a software update to the Hydraulic Monitoring and Control Application (HMCA) to enhance protection against overheating. This directive is effective from 26 February 2025.

Airworthiness DirectiveSuperseded
  • Airbus A350

EASA AD 2025-0031

Feb 10, 2025

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

EASA Airworthiness Directive 2025-0031 is an amendment addressing the Time Limits and Maintenance Checks in the Airworthiness Limitations Section Part 3 for Airbus A318, A319, A320, and A321 aeroplanes. It applies to all manufacturer serial numbers of these models and mandates compliance with updated Certification Maintenance Requirements. The directive ensures continued airworthiness by requiring operators to follow the latest Airbus ALS Part 3 Revision 10 maintenance tasks and intervals.

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

EASA AD 2025-0032

Feb 10, 2025

Time Limits / Maintenance Checks — Airworthiness Limitations Section Part 4 — System Equipment Maintenance Requirements — Amendment

EASA Airworthiness Directive 2025-0032 is an amendment addressing the Time Limits and Maintenance Checks in the Airworthiness Limitations Section Part 4 for Airbus A318, A319, A320, and A321 aeroplanes. It applies to all manufacturer serial numbers of these models and mandates compliance with updated system equipment maintenance requirements. This directive ensures continued airworthiness by enforcing specific maintenance tasks and life limits.

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

EASA AD 2025-0033

Feb 10, 2025

Time Limits / Maintenance Checks — Airworthiness Limitations Section Part 5 — Fuel Airworthiness Limitations — Amendment

EASA Airworthiness Directive 2025-0033 is an amendment addressing time limits and maintenance checks in the Airworthiness Limitations Section Part 5 related to fuel airworthiness limitations for Airbus A318, A319, A320, and A321 aeroplanes. It applies to all manufacturer serial numbers of these models and mandates compliance with Airbus A318/A319/A320/A321 ALS Part 5 Revision 09. The directive ensures continued airworthiness by enforcing updated maintenance tasks and life limits for fuel system components.

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

EASA AD US-2025-01-09

Feb 10, 2025

Windows - No. 1 Flight Compartment Windows - Replacement

The document titled "Windows - No. 1 Flight Compartment Windows - Replacement" is a regulatory directive concerning the replacement of the primary flight compartment windows on certain aircraft. It addresses the procedures and requirements for replacing these windows to ensure continued airworthiness and safety. Specific aircraft types or engine models affected are not clearly identified in the provided content.

Airworthiness Directive
  • Boeing 787

EASA AD 2025-0028

Feb 7, 2025

Main Rotor — Main Rotor Head — Inspection / Re-identification

The document titled 'Main Rotor — Main Rotor Head — Inspection / Re-identification' applies to the AIRBUS HELICOPTERS DEUTSCHLAND MBB-BK 117 helicopter model. It addresses inspection and re-identification procedures for the main rotor head to ensure continued airworthiness and safety of the affected aircraft. The document provides guidance on maintaining the integrity of the main rotor assembly.

Airworthiness Directive
  • Airbus Helicopters MBB-BK 117

EASA AD 2025-0029

Feb 7, 2025

Main Rotor — Swashplate — Inspection

EASA Airworthiness Directive 2025-0029 is an airworthiness directive addressing the inspection of the main rotor swashplate on MBB-BK117 D-3 and D-3m helicopters. It specifically targets swashplates with Part Number D623M2050102 and serial numbers up to 0487 inclusive, except those already subjected to a supplementary inspection. The directive mandates a one-time inspection and corrective actions to ensure continued safe operation of affected helicopters.

Airworthiness Directive
  • Airbus Helicopters MBB-BK 117

EASA SIB CASA-2023-07_02

Feb 5, 2025

Degraded Anti-Skid Performance when Landing on a Contaminated Runway

The Transport Canada Civil Aviation Safety Alert CASA 2023-07 Issue No. 02 addresses degraded anti-skid performance when landing on contaminated runways for Airbus Canada Limited Partnership A220 series aeroplanes, specifically models BD-500-1A10 and BD-500-1A11. The alert highlights the risk of transient locked wheels due to low friction conditions, which can lead to reduced braking effectiveness and directional control issues during landing. It reinforces existing guidance and mitigation measures recommended by Airbus Canada to enhance safety during operations on contaminated surfaces.

Safety Information Bulletin
  • Airbus BD-500 (A220 Series)

EASA AD 2025-0027

Feb 5, 2025

Main Rotor — Swashplate Inner and Outer Ring Bolts — Inspection / Replacement

EASA Airworthiness Directive 2025-0027 is an airworthiness directive addressing the inspection and replacement of main rotor swashplate inner and outer ring bolts on MBB-BK117 D-3 and D-3m helicopters. It applies to swashplates with part number D623M2050102 up to serial number 0503, excluding certain serial numbers and those already inspected and corrected. The directive mandates inspection and replacement of bolts to ensure structural integrity of the swashplate.

Airworthiness Directive
  • Airbus Helicopters MBB-BK 117

EASA AD US-2025-01-06

Feb 5, 2025

Superseded by FAA AD 2025-15-08

The FAA Airworthiness Directive 2025-01-06 supersedes AD 2019-14-13 and applies to all Boeing 767-200, -300, -300F, and -400ER series airplanes. It addresses uncommanded fore and aft movement of the Captain's and First Officer's seats by requiring identification of seat part and serial numbers, inspections of the horizontal movement system (HMS), and applicable on-condition actions. The directive incorporates updated Boeing and Ipeco service bulletins to include previously omitted seat part numbers.

Airworthiness Directive
  • Boeing 767

EASA AD 2007-0260-CN

Feb 4, 2025

CANCELLED: Engine — Intermediate Pressure Turbine Bearing Oil Feed Tube — Inspection / Modification

EASA Airworthiness Directive Cancellation Notice 2007-0260-CN cancels the previous directive 2007-0260R1 concerning the inspection and modification of the intermediate pressure turbine bearing oil feed tube on Rolls-Royce RB211 Trent 700 engines. These engines are commonly installed on Airbus A330 aircraft. The cancellation reflects that all affected engines have been modified, eliminating the unsafe condition addressed by the original directive.

Airworthiness Directive
  • Rolls-Royce Deutschland Ltd & Co Kg RB211 TRENT 700

EASA AD US-2024-26-02

Feb 4, 2025

Pacific Scientific Company: Rotary Buckle Assemblies - Inspection / Replacement

Pacific Scientific Company: Rotary Buckle Assemblies - Inspection / Replacement is a regulatory document addressing the inspection and replacement requirements for rotary buckle assemblies manufactured by Pacific Scientific Company. The document focuses on ensuring the continued airworthiness and safety of aircraft equipped with these specific rotary buckle assemblies. It applies to operators and maintenance organizations responsible for aircraft using these components.

Airworthiness Directive

EASA AD US-2024-26-03

Feb 3, 2025

Water / Waste - Potable Water System - Installation / Leakage Test

The document titled 'Water / Waste - Potable Water System - Installation / Leakage Test' is a regulatory guideline focused on the installation and leakage testing procedures for potable water systems in aircraft. It addresses standards to ensure the integrity and safety of potable water installations, although no specific aircraft types or engine models are mentioned. The document aims to maintain the hygiene and operational reliability of potable water systems onboard.

Other
  • Boeing 767

EASA AD 2020-0010R3

Jan 30, 2025

Engine — De-Pairing Limitation

EASA Airworthiness Directive 2020-0010R3 is an updated regulatory document addressing engine surge risks in Rolls-Royce Trent 1000 series engines installed on Boeing 787 aircraft. It applies to Trent 1000-A, -AE, -C, -CE, -D, -E, -G, and -H engines except those modified with Rolls-Royce Service Bulletin TRENT1000-72-K434. The directive mandates de-pairing limitations to mitigate the risk of dual engine surges that could lead to in-flight shutdowns.

Airworthiness Directive
  • Rolls-Royce Deutschland Ltd & Co Kg TRENT 1000

EASA AD 2019-0249R1

Jan 30, 2025

Engine — Intermediate Pressure Compressor Blades / Shafts — Inspection

EASA Airworthiness Directive 2019-0249R1 is an updated regulatory requirement addressing inspection of intermediate pressure compressor blades and shafts on Rolls-Royce Trent 1000 engines, commonly installed on Boeing 787 aircraft. The directive mandates repetitive inspections of specific IPC Rotor 1 and Rotor 2 blades and IPC shaft components to detect cracks and prevent in-flight blade release. It applies to all serial numbers of Trent 1000-A, -AE, -C, -CE, -D, -E, -G, and -H engine variants.

Airworthiness Directive
  • Rolls-Royce Deutschland Ltd & Co Kg TRENT 1000

EASA AD CF-2025-07

Jan 29, 2025

Flight Controls — Horizontal Stabilizer Trim Actuator (HSTA) — Incorrect Installation of the Interface Pin in the Upper Gimbal

Canadian Airworthiness Directive CF-2025-07 addresses a safety issue in Airbus Canada Limited Partnership aircraft models BD-500-1A10 and BD-500-1A11. The directive concerns the incorrect installation of the interface pin in the upper gimbal of the Horizontal Stabilizer Trim Actuator (HSTA). It mandates inspection and correction to ensure proper mechanical connection of the horizontal stabilizer.

Airworthiness Directive
  • Airbus BD-500 (A220 Series)

EASA AD 2024-0152R1

Jan 29, 2025

Ignition — Advanced Start System — Deactivation

Ignition — Advanced Start System — Deactivation is a technical document concerning the TECNAM Costruzioni Aeronautiche P2008 JC aircraft. It addresses procedures or requirements related to the deactivation of the advanced start ignition system on this specific aircraft model. The document provides guidance relevant to maintaining or modifying the ignition system to ensure compliance and safety.

Other
  • Tecnam P2008 JC