Browse 4987 EASA regulations with AI-powered summaries.
EASA AD 2024-0042
EASA Airworthiness Directive 2024-0042 is issued for all SAAB SF340A and 340B aeroplanes. It mandates compliance with the updated Airworthiness Limitation Manual (ALM) Revision 2, which includes new and more restrictive maintenance tasks and life limits. This directive ensures continued airworthiness by updating maintenance requirements for these aircraft models.
EASA AD 2024-0041
The document titled 'Time Limits / Maintenance Checks — Time Limits Manual / Maintenance Programme — Amendment' pertains to the Rolls-Royce Deutschland Ltd & Co KG Trent 7000 engine. It provides updated guidance and requirements related to the maintenance time limits and checks for this specific engine model. The amendment aims to ensure continued airworthiness and reliability of the Trent 7000 engine through revised maintenance protocols.
EASA AD 2024-0040-E
EASA Airworthiness Directive 2024-0040-E is an emergency directive addressing a potential unsafe condition in GE Aviation Czech M601 series engines installed on various aircraft including the LET L-410, Air Tractor AT series, Grumman G-164, and others. The directive mandates inspection of the centrifugal compressor case for cracks and restricts installation of affected parts. It applies to engines with specific part numbers M601-154.55 and M601-154.65 unless previously inspected and cleared.
EASA AD 2024-0039
EASA Airworthiness Directive 2024-0039 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Rolls-Royce Deutschland Ltd & Co KG RB211 Trent 900 and Trent 970 series engines, commonly installed on Airbus A380 aircraft. This directive mandates compliance with updated airworthiness limitations and maintenance tasks as specified in the Rolls-Royce Trent 900 Time Limits Manual Revision 65 dated 01 October 2023. It ensures continued airworthiness by enforcing life limits and mandatory inspections for critical engine components.
EASA AD US-2024-01-11
FAA Airworthiness Directive 2024-01-11 is a final rule addressing an unsafe condition in certain Pacific Scientific Company rotary buckle assemblies installed on various helicopters. The affected buckles, part numbers 1111475 (all dash numbers) and 1111548-01, were manufactured between January 2012 and September 2012 and contain screws susceptible to hydrogen embrittlement, risking buckle failure during occupant restraint. This directive applies specifically to helicopters and requires inspection and possible replacement of the buckles or screws to ensure safety.
EASA AD US-2024-01-04
Airworthiness Directive 2024-01-04 is a final rule issued by the Federal Aviation Administration addressing Boeing 787-8, 787-9, and 787-10 airplanes powered by Rolls-Royce Trent 1000 engines. It focuses on inspections and replacement of the inner fixed structure forward upper fire seal and thermal insulation blankets in the thrust reverser area to prevent damage and potential fire hazards. This directive mandates inspection and replacement of specific upper splitter fairing assemblies to enhance engine fire safety.
EASA SIB 2024-03R1
EASA Safety Information Bulletin 2024-03R1 addresses an issue with Collins Aerospace Satellite Based Augmentation Systems receivers models GPS-4000S, GLU-2100, GLUS-2100, and GLUS-2100A. The bulletin highlights incorrect processing of the integrity information message (Message Type 6) under certain conditions, potentially affecting the notification of compromised GNSS position integrity. This issue was exposed following an update to the EGNOS ground system in November 2023 and applies to specific hardware and software part numbers listed in the bulletin.
EASA AD 2024-0037R1
The document titled 'Engine — Main Bearing / Studs — Replacement' issued by AUSTRO ENGINE GMBH for the E4 engine model addresses the replacement requirements for main bearing studs. It provides guidance and regulatory instructions for maintaining engine integrity and safety. This document is relevant to operators and maintenance organizations working with the AUSTRO ENGINE GMBH E4 engine.
EASA AD US-2024-01-01
FAA Airworthiness Directive 2024-01-01 is a final rule addressing certain Boeing Model 787-8, 787-9, and 787-10 airplanes. It mandates repetitive visual inspections under all lavatory washbasins to detect intermittent and active water leaks from the faucet control module (FCM), which could migrate below the passenger floor and into electronic equipment bays. The directive aims to prevent damage to flight-critical equipment caused by these leaks.
EASA AD US-2024-01-06
Federal Aviation Administration Airworthiness Directive 2024-01-06 is a final rule addressing certain Boeing 737-600, 737-700, and 737-800 series airplanes. It mandates repetitive inspections of fuselage skin repairs at Stringer S-17 to detect cracks and requires corrective actions if necessary. This directive aims to ensure continued airworthiness by preventing fatigue cracking that could compromise structural integrity.
EASA AD BR-2024-02-01
Brazilian Airworthiness Directive AD No. 2024-02-01 issued by the Agência Nacional de Aviação Civil (ANAC) mandates inspection and possible replacement of Kidde Aerospace & Defense Overheat Detection System (ODS) sensing elements on Embraer S.A. ERJ 190-300 and ERJ 190-400 aircraft. The directive addresses potential failures in ODS sensing elements produced before January 31, 2021, which could lead to undetected thermal bleed leaks and pose fire risks. It requires operators to inspect specific bleed lines and wing anti-ice and bleed system sensing elements to ensure flight safety.
EASA AD 2024-0038
EASA Airworthiness Directive 2024-0038 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes. It addresses inspection and modification requirements for forward-facing galley parts with specific part numbers to prevent damage that could lead to trolley detachment during emergency landings. This directive applies to all manufacturer serial numbers of the listed aircraft models.
EASA AD 2024-0031
EASA Airworthiness Directive 2024-0031 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes. It mandates compliance with updated Damage Tolerance Airworthiness Limitations Items specified in the Airbus Airworthiness Limitations Section Part 2 Revision 10. This directive ensures continued airworthiness by requiring operators to follow new and/or more restrictive maintenance tasks.
EASA AD ISR-I-57-2021-12-4R1
Airworthiness Directive ISR I-57-2021-12-4R1 issued by the State of Israel Civil Aviation Authority addresses the repair of wing flap fairing seals on GALP model G200 aircraft, serial numbers 004 through 250. The directive mandates inspection and resealing of the fillet seal between the wing structure and flap fairings to prevent flap fairing debonding, moisture intrusion, and corrosion of the wing lower skin at rib 3 and rib 11.
EASA AD ISR-I-57-2021-12-3R1
Airworthiness Directive AD ISR I-57-2021-12-3R1 issued by the State of Israel Civil Aviation Authority addresses the GALP model G150 aircraft, serial numbers 201 through 326. This directive mandates inspection and repair of wing flap fairing seals to prevent flap fairing debonding, moisture intrusion, and corrosion of the wing lower skin at rib 3 and rib 11. The repair must be performed according to Gulfstream Service Bulletin No. 150-57-197 or later approved revisions.
EASA SIB BEA-2024-01
FFE Ltd: Fire Suppression — Toilet Compartment Fire Extinguishers is a Special Airworthiness Bulletin (BEA 2024-01) issued to inform owners and operators about inspection recommendations for certain Toilet Compartment Fire Extinguishers FE-36 installed on Embraer ERJ 170, ERJ 190, EMB-135, EMB-145, EMB-545, and EMB-550 aircraft. The bulletin addresses fire extinguishers manufactured by FFE Ltd. with specific part numbers and serial numbers produced before June 12, 2023. It highlights a potential manufacturing defect that may cause leakage and loss of fire suppression capability.
EASA AD 2024-0032
EASA Airworthiness Directive 2024-0032 is an airworthiness directive issued for Airbus A380-841, A380-842, and A380-861 aeroplanes with specific manufacturer serial numbers. It mandates inspection of the centre fuselage shims on frames 47 to 53 to detect missing or mislocated shims that could affect structural integrity. The directive provides detailed inspection and corrective action procedures to ensure continued airworthiness.
EASA AD 2024-0030
EASA Airworthiness Directive 2024-0030 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes. It mandates compliance with the updated Airbus Airworthiness Limitations Section (ALS) Part 3 Revision 09, which contains certification maintenance requirements essential for continued airworthiness. This directive applies to all manufacturer serial numbers of the specified Airbus A320 family models.
EASA AD 2024-0033
EASA Airworthiness Directive 2024-0033 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Dassault Aviation Falcon 7X aeroplanes, including those modified to Falcon 8X standard. It mandates compliance with updated airworthiness limitations specified in the Dassault Falcon 7X Aircraft Maintenance Manual, Airworthiness Limitations Section, Revision 12. This directive ensures continued airworthiness by enforcing maintenance tasks and life limits for components.
EASA AD 2024-0034
EASA Airworthiness Directive SUPERSEDED BY EASA AD 2025-0290 is a regulatory document related to the Dassault Aviation Falcon 900EX aircraft. The directive has been superseded by a newer airworthiness directive numbered 2025-0290. No further technical details or specific requirements are available due to the document content extraction failure.