Browse 5,141 EASA regulations with AI-powered summaries.
EASA AD 2025-0178
Aug 8, 2025The document titled 'Auto Flight — Emergency Procedure Section — Modification' is an official regulatory communication concerning the Airbus A330 aircraft model. It addresses updates related to the auto flight system's emergency procedures section for this specific aircraft type.
EASA AD 2025-0177
Aug 8, 2025Fuselage — Aft Fitting of Frame 40 — Inspection is a regulatory document concerning the Airbus A300-600ST (Beluga) aircraft. It addresses inspection requirements for the aft fitting at Frame 40 of the fuselage structure. The document aims to ensure the structural integrity and continued airworthiness of this specific aircraft model.
EASA AD 2019-0011R2
Aug 8, 2025Fuselage — Aft Fitting of Frame 40 — Inspection is a regulatory document concerning the inspection requirements for the aft fitting of Frame 40 on Airbus A300 and A300-600 aircraft. It addresses structural integrity checks specific to this fuselage component to ensure continued airworthiness of these aircraft models.
EASA AD CF-2025-38
Aug 8, 2025Canadian Airworthiness Directive CF-2025-38 addresses missing or loose bolts on the horizontal stabilizer (H-Stab) anti-yaw steady fitting block in MHI RJ Aviation ULC aircraft models CL-600-2C10, CL-600-2C11, CL-600-2D15, CL-600-2D24, and CL-600-2E25 within specified serial number ranges. The directive mandates inspections and torque checks of the fitting block bolts to ensure they are secure until replacement hardware with secondary locking features is installed. This AD aims to prevent potential loss of the horizontal stabilizer due to bolt failure under certain loading conditions.
EASA AD CF-2025-39
Aug 8, 2025Canadian Airworthiness Directive CF-2025-39 addresses an issue with oversized holes in rib 6 of the wings on Bombardier Inc. model BD-700-2A12 aeroplanes, specifically serial numbers 70042 through 70074, 70079, and 70080. The directive mandates inspection and potential rework of fasteners and fastener holes to ensure structural integrity. This AD aims to prevent fuel leakage and potential structural failure due to cracks in the wing rib shear-ties.
EASA AD 2025-0154R1
Aug 7, 2025The document titled Aircraft Flight Manual - Limitation / Wings — Front and Rear Spar — Inspections is an EASA Airworthiness Directive 2025-0154R1 issued on 7 August 2025. It applies to LAVIA ARGENTINA S.A. PA-25, PA-25-235, and PA-25-260 aeroplanes and mandates inspections of specific front and rear wing spars identified by part numbers. The directive addresses corrosion and crack findings in wing spars and related fittings to ensure continued airworthiness.
EASA AD 2025-0176
Aug 7, 2025The document titled Air — Intermediate / High Pressure Air Tubes / Connectors — Inspection is a regulatory directive concerning the inspection requirements for intermediate and high pressure air tubes and connectors on Rolls-Royce Deutschland Ltd & Co KG Trent 1000 engines. It specifies inspection protocols to ensure the integrity and safety of these components in affected aircraft powered by Trent 1000 engines.
EASA AD CF-2025-37
Aug 6, 2025Airworthiness Directive CF-2025-37 is issued by Transport Canada and applies to Airbus Canada Limited Partnership model BD-500-1A10 and BD-500-1A11 aircraft. It addresses loose fasteners and missing brush seals on the fuel boost pump canister to wing rib 6 interface, which may cause fuel leaks and corrosion. The directive mandates inspections and corrective actions to ensure continued airworthiness.
EASA AD 2025-0173
Aug 5, 2025EASA Airworthiness Directive 2025-0173 is an amendment addressing the Aircraft Flight Manual normal procedures for ATR 42-400, ATR 42-500, ATR 72-212, and ATR 72-212A aeroplanes. The directive mandates updates to smoke detector check procedures in the flight manuals to enhance safety during cargo operations. It applies to all manufacturer serial numbers of the specified ATR models.
EASA AD 2025-0172
Aug 4, 2025EASA Airworthiness Directive 2025-0172 is an official safety directive addressing hydraulic pump motor replacement on General Atomics AeroTec Systems GmbH Dornier 228 aeroplanes, including models Dornier 228-100 through Dornier 228-212. The directive targets hydraulic pump motor Part Number 1259A, requiring replacement with an improved motor Part Number A-752511A00B to prevent overheating issues. This directive applies to all serial numbers of the affected Dornier 228 aircraft.
EASA AD 2025-0170
Aug 4, 2025The document titled 'Main Landing Gear — Replacement' is a regulatory communication concerning the Airbus A300, A300-600, and A300-600ST (Beluga) aircraft models. It addresses the replacement procedures or requirements related to the main landing gear components of these specific Airbus aircraft types. The document serves as a guideline or directive for maintenance and operational compliance.
EASA AD BR-E2025-07-03R1
Aug 4, 2025Brazilian Emergency Airworthiness Directive E2025-07-03R1 is issued by the Agência Nacional de Aviação Civil (ANAC) and applies to Embraer ERJ190-300 and ERJ190-400 aircraft equipped with Engine Feed Check Valve Part Number L85E38-003. This directive mandates inspections and functional tests of the engine feed check valves to address potential valve failures that could lead to engine flameout or fuel starvation during flight.
EASA AD G-2025-0004-E
Aug 1, 2025The Civil Aviation Authority Emergency Airworthiness Directive G-2025-0004-E addresses safety concerns for hot air balloons equipped with fuel cylinders fitted with Pressure Relief Valve (PRV) adaptor CB8426, including models such as Thunder & Colt, Sky Lindstrand, and various Cameron Balloons Limited cylinders. This directive mandates inspection for cracks in the CB8426 adaptors and replacement with the new CB7922 adaptor to prevent uncontrolled LPG fuel leaks.
EASA AD US-2025-15-07
Jul 31, 2025Airworthiness Directive 2025-15-07 is a final rule issued by the Federal Aviation Administration addressing The Boeing Company Model 747 series airplanes, including 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, 747-8F, and 747-8. It focuses on inspection and checks of the Captain's and First Officer's seats, specifically the horizontal movement system (HMS), to ensure safety and prevent uncommanded seat movement during critical flight phases.
EASA AD 2025-0169
Jul 31, 2025EASA Airworthiness Directive 2025-0169 is an official regulatory document addressing modifications to the flight controls, specifically the Trimmable Horizontal Stabilizer Actuator (THSA) and Electric Load Sensing Device (ELSD) on Airbus A330 and A340 aeroplanes. This directive applies to various Airbus A330 models up to manufacturer serial number 1919 (excluding MSN 1915) and all Airbus A340-211, -212, -213, -311, -312, and -313 models. The AD mandates modifications to improve safety related to the THSA's secondary load path and the installation and activation of the ELSD.
EASA AD 2025-0043R1
Jul 31, 2025EASA Airworthiness Directive 2025-0043R1 is an amendment addressing Airbus A330-243, A330-243F, A330-841, and A330-941 aeroplanes equipped with Airbus modification 207423 but not modification 211442. The directive mandates updates to the Aircraft Flight Manual and Master Minimum Equipment List to mitigate issues related to loss of data synchronization between Radio Management Panels and the Audio Management Unit. This AD aims to prevent loss of radio communication control, transponder and TCAS setting changes, and standby navigation activation.
EASA AD 2025-0168
Jul 31, 2025The document titled 'Wings — Frame 40 Lower Junction Fastener Holes — Inspection' is an inspection directive applicable to the AIRBUS S.A.S. A300-600ST (Beluga) aircraft. It addresses the condition and integrity of the fastener holes located at the lower junction of Frame 40 on the wings. The directive aims to ensure continued airworthiness by mandating specific inspection procedures for these critical structural elements.
EASA AD 2014-0272R1
Jul 31, 2025EASA Airworthiness Directive 2014-0272R1 is an updated regulation addressing inspection and repair requirements for the frame 40 lower junction fastener holes on Airbus A300 and A300-600 aeroplanes. It mandates specific inspections to detect cracks in the fittings around these fastener holes to ensure structural integrity. The directive applies to all models and serial numbers of these aircraft types.
EASA AD 2025-0166
Jul 30, 2025The document titled 'Fuselage — Inner Cap and Frame Flange at Frame 68 Stringer 22 — Inspections' is a regulatory directive applicable to Airbus S.A.S. aircraft models A318, A319, A320, and A321. It addresses inspection requirements focused on the fuselage structure, specifically the inner cap and frame flange at frame 68 stringer 22. The directive aims to ensure structural integrity and continued airworthiness of these aircraft types.
EASA AD 2025-0163
Jul 30, 2025The Rotors Flight Control — Brake Pedal Assembly — Inspection document addresses inspection requirements for the brake pedal assembly on LEONARDO S.p.A. helicopters, specifically the AB139, AW139, and AW189 models. It provides guidance to ensure the continued airworthiness and safety of the rotor flight control system components related to braking.