Browse 5052 EASA regulations with AI-powered summaries.
EASA AD 2025-0250
EASA Airworthiness Directive 2025-0250 is an airworthiness directive addressing Fokker F28 Mark 0070 and Mark 0100 aeroplanes. It mandates a one-time inspection of the fuselage frame inboard boom area at specific wing spar joint locations to detect cracks that could compromise structural integrity. The directive also requires reporting inspection results to Fokker Services.
EASA AD CF-2024-22R1
The Navigation — Required Navigation Performance Authorization Required (RNP-AR) Approach Vertical Deviation Airworthiness Directive CF-2024-22R1 applies to Bombardier Inc. model BD-700-2A12 aeroplanes, serial numbers 70005 through 70193. This directive addresses vertical deviation issues during RNP-AR approaches caused by partial engine thrust loss under certain conditions. It mandates updates to the Airplane Flight Manual to ensure safe approach containment and obstacle clearance.
EASA AD 2025-0249-E
EASA Airworthiness Directive 2025-0249-E is an emergency directive addressing the Airbus Helicopters EC 130 T2 and EC 130 B4 models. It mandates the replacement of the tail rotor drive centre shaft assembly, part number 350A34021401, due to potential fatigue cracking that could lead to failure of the tail rotor drive shaft and loss of yaw control. This directive applies to all serial numbers of the affected helicopter models.
EASA AD 2025-0248
EASA Airworthiness Directive 2025-0248 is an airworthiness directive issued by the European Union Aviation Safety Agency addressing Airbus A318, A319, A320, and A321 aeroplanes equipped with ARIES overhead stowage compartments. The directive mandates inspection and repair of specific overhead stowage compartments to ensure their structural integrity. It applies to affected parts identified by certain part numbers and excludes aircraft with specific Airbus modifications embodied in production.
EASA SIB CASA-2025-11
Part Number MS20220-3 Pulleys with Corroded and Dislodged Bearings is a Transport Canada Civil Aviation Safety Alert (CASA 2025-11) addressing corrosion issues in flight control pulleys and pulley bearing assemblies installed on De Havilland Canada (DHC) DASH 8 series 100/200/300/400 aircraft. The alert highlights multiple service difficulty reports involving corroded and seized pulleys causing stiff roll control and autopilot disconnection. It targets operators and maintenance personnel responsible for the affected flight control systems.
EASA AD CF-2025-52
The Canadian Airworthiness Directive CF-2025-52 addresses interference caused by 5G C-Band wireless broadband signals with radio altimeter systems on De Havilland Aircraft of Canada Limited DHC-8-100, -200, and -300 series aircraft operating in the contiguous United States airspace. This directive mandates modifications to affected aircraft radio altimeters to ensure tolerance against 5G interference and introduces interim operational limitations. It specifically targets aircraft equipped with Honeywell RT-300 radio altimeters.
EASA AD 2025-0026R1
The document titled "Oxygen — Full-Face Quick Donning Masks — Functional Check" is an explanatory statement regarding the absence of an Airworthiness Directive (AD) for the Airbus A400M aeroplane in civil service. It clarifies that no publicly available AD exists because the Airbus A400M is not in civil operation, and the content is provided by EASA solely for information to military authorities and design approval holders. The applicable AD for this aircraft type is issued by the responsible military authority depending on the country of registration.
EASA AD 2025-0238
EASA Airworthiness Directive 2025-0238 is a corrective directive addressing the replacement of the Ram Air Turbine (RAT) module on Airbus A350-941 and A350-1041 aeroplanes. It targets RAT modules identified by Part Number 1713586A that have been deployed and retracted in flight, due to corrosion issues affecting electrical power generation. This directive applies to all manufacturer serial numbers of the specified Airbus A350 models.
EASA AD 2025-0244
The document titled 'Doors — Passenger / Crew Door Girt Bar Fitting Assemblies — Inspection' is an airworthiness directive applicable to AIRBUS S.A.S. A350 aircraft. It addresses the inspection requirements for the passenger and crew door girt bar fitting assemblies to ensure their continued airworthiness and safety. The directive provides guidance on inspection procedures specific to these door components on the Airbus A350 model.
EASA AD 2025-0246
EASA Airworthiness Directive 2025-0246 is issued for CFM International LEAP-1A engines installed on certain Airbus A319, A320, and A321 aircraft. It addresses non-synchronous vibration issues caused by affected bearing No. 3 spring finger housing parts, which may lead to engine stalls or turbine failures. The directive mandates monitoring and replacement of these parts to ensure continued airworthiness.
EASA AD 2025-0245
The document titled 'Fire Protection — Pyrotechnical Cartridge — Inspection' is a regulatory directive concerning the inspection of pyrotechnical cartridges used in fire protection systems on Dassault Aviation aircraft, specifically the Fan Jet Falcon, Mystère-Falcon 20, Mystère-Falcon 20GF, and 200 models. It addresses safety measures related to the maintenance and inspection of these critical fire protection components to ensure continued airworthiness.
EASA AD 2025-0207R1
EASA Airworthiness Directive 2025-0207R1 is an updated regulatory requirement addressing the replacement of nylon bushes with bronze bushes in the seat rail connections of Airbus A318, A319, A320, and A321 aircraft. This directive applies to all manufacturer serial numbers except those with Airbus modifications 152721 and 154725 incorporated. It aims to ensure continued airworthiness by mitigating risks associated with broken bolts in critical seat rail areas.
EASA AD 2025-0137
[Correction] Time Limits / Maintenance Checks — Airworthiness Limitations Section — Amendment is a regulatory document addressing the airworthiness limitations for AIRBUS HELICOPTERS AS 350 and EC 130 models. It provides updated instructions related to time limits and maintenance checks to ensure continued airworthiness of these helicopter types. The amendment clarifies or corrects previous maintenance requirements to enhance safety and compliance.
EASA AD US-2025-19-12
The document titled "Landing Gear - Main Landing Gear Outer Cylinders - Records Check / Inspection" is a final rule airworthiness directive (AD 2025-19-12) issued by the Federal Aviation Administration (FAA) affecting all Boeing 737-600, -700, -700C, -800, -900, and -900ER series airplanes. This AD addresses potential heat damage caused by improper grinding of the inner diameter of the main landing gear outer cylinders. It mandates inspections or records checks and replacement of affected parts to ensure continued airworthiness.
EASA AD 2025-0241
EASA Airworthiness Directive 2025-0241 is an airworthiness directive affecting Airbus A330 and A340 aeroplanes, specifically those with Angle of Attack (AOA) backplates having Part Number A5341054920000. The directive addresses potential safety issues related to incorrect data in Airbus technical drawings used for reinstalling AOA backplates. It mandates inspections and corrective actions to ensure the accuracy and reliability of AOA sensor data on affected aircraft.
EASA AD 2025-0243
EASA Airworthiness Directive 2025-0243 is an official regulatory document addressing the replacement of forward outer seals, high-pressure compressor stages 6-10 compressor rotor spools, and high-pressure turbine rotor stage 1 disks on CFM International LEAP-1A engines. These engines are commonly installed on Airbus A319, A320, and A321 aircraft. The directive mandates inspection and replacement of affected parts to ensure continued airworthiness and safety.
EASA AD 2025-0223R1
The document titled 'Parking, Mooring and Storage — Mooring Procedure — Prohibition' addresses regulations related to the mooring procedures for ATR42 and ATR72 aircraft types. It outlines prohibitions concerning specific mooring practices to ensure safety and compliance. This document is relevant for operators and maintenance teams managing ATR:ATR42 and ATR72 aircraft.
EASA AD 2022-0168R2
The Rotorcraft Flight Manual — Section Emergency Procedures — Amendment; Integrated Modular Avionics — Ethernet Network — Inspection is a regulatory document applicable to AIRBUS HELICOPTERS DEUTSCHLAND models EC135, 635, and MBB-BK 117. It addresses updates to the emergency procedures section of the flight manual and introduces inspection requirements for the integrated modular avionics Ethernet network. The document aims to enhance operational safety and avionics reliability for these specific rotorcraft types.
EASA AD 2025-0237
EASA Airworthiness Directive 2025-0237 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes, including both Current Engine Option (CEO) and New Engine Option (NEO) models. The directive addresses inspection and repair requirements for the 80 VU rack attachments, which house critical flight control, communication, and radio-navigation computers. It mandates repetitive inspections and corrective actions to ensure the structural integrity of the 80 VU rack fittings and prevent potential system failures.
EASA AD 2025-0239
EASA Airworthiness Directive 2025-0239 is an airworthiness directive affecting Airbus Helicopters SA 365, AS 365, and EC 155 models. It mandates inspections of the upper ball bearing end of the main rotor servo-controls to ensure proper nut tightening torque and prevent potential disconnection. The directive applies to all serial numbers of the specified helicopter models.