Browse 140 EASA regulations with AI-powered summaries.
EASA AD 2018-0201
EASA Airworthiness Directive 2018-0201 is an official directive addressing Airbus A340-213, A340-311, and A340-313 aeroplanes with specific manufacturer serial numbers. It mandates a software update to the Fuel Control and Monitoring Computer (FCMC) to the 'Stage 12' standard or higher to prevent fuel starvation issues during flight.
EASA AD 2018-0192
EASA Airworthiness Directive 2018-0192 is an amendment addressing the engine bleed air system and flight warning computer on Airbus A340-211, A340-212, A340-213, A340-311, A340-312, and A340-313 aeroplanes. It mandates modifications to the Flight Warning Computer software to prevent engine bleed valve malfunctions that could lead to over-temperature conditions. The directive also involves changes to the Aircraft Flight Manual to reflect updated operational procedures.
EASA AD 2018-0151
EASA Airworthiness Directive 2018-0151 is an airworthiness directive applicable to Airbus A330 and A340 aeroplanes. It addresses inspection and replacement requirements for the outboard flap drive station elements and sensor struts to ensure continued safe operation of the flap systems on these aircraft models.
EASA AD 2018-0150
EASA Airworthiness Directive 2018-0150 addresses the reduced life limits for repaired main landing gear (MLG) wheel axles on Airbus A330 and A340 aeroplanes. This directive applies to specific serial numbers and part numbers of MLG wheel axles repaired by three identified Maintenance Repair Organisations (MROs). It mandates identification and replacement of affected axles to ensure continued airworthiness.
EASA AD 2016-0152R1
EASA Airworthiness Directive 2016-0152R1 is an updated directive affecting Airbus A340 series aeroplanes, including models A340-211, A340-212, A340-213, A340-311, A340-312, A340-313, A340-541, A340-542, A340-642, and A340-643. This directive mandates compliance with the Airbus A340 Airworthiness Limitations Section (ALS) Part 2, which covers damage tolerant airworthiness limitation items to ensure continued airworthiness and safety.
EASA AD 2018-0064
Hydraulic Power — Hydraulic Reservoir Pressure Relief Valve — Inspection / Replacement is a technical document issued by AIRBUS S.A.S. concerning the inspection and replacement procedures for the hydraulic reservoir pressure relief valve on Airbus A330 and A340 aircraft. The document provides guidance to ensure the proper functioning and safety of the hydraulic power system in these aircraft types.
EASA AD 2018-0062
Hydraulic Power — Ram Air Turbine Hydraulic Pumps — Replacement is a regulatory document issued for AIRBUS S.A.S. A330 and A340 aircraft types. It addresses the replacement requirements for the hydraulic pumps associated with the Ram Air Turbine system on these aircraft models. The document aims to ensure continued hydraulic power reliability and safety during flight.
EASA AD 2018-0005
EASA Airworthiness Directive 2018-0005 addresses inspection and repair requirements for fuselage bulk cargo door frames on Airbus A330 and A340 aeroplanes, specifically models with manufacturer serial numbers up to 1779. The directive focuses on detecting cracks caused by surface treatments affecting fatigue behavior in door fitting attachment holes. It mandates repetitive inspections and provides an optional modification to terminate these inspections.
EASA AD 2017-0245
EASA Airworthiness Directive 2017-0245 is an airworthiness directive issued by the European Aviation Safety Agency affecting Airbus A330 and A340 aeroplanes. It addresses the reduced life limits of repaired main landing gear (MLG) wheel axles due to specific repairs that compromised their fatigue life. The directive applies to various A330 and A340 models, excluding certain serial numbers and those with specific Airbus modifications.
EASA AD 2014-0068R2
EASA Airworthiness Directive 2014-0068R2 is an updated regulatory requirement addressing inspection and replacement of trimmable horizontal stabilizer (THS) support struts on Airbus A330 and A340-200/-300 series aircraft. It applies to specific serial numbers of these aircraft except those modified per Airbus Service Bulletins A330-53-3280 or A340-53-4240. The directive mandates detailed inspections for cracks in the THS support struts and corrective actions to maintain structural integrity of the horizontal tail plane.
EASA SIB 2014-07R1
EASA Safety Information Bulletin 2014-07R1 addresses unexpected autopilot behavior during Instrument Landing System (ILS) approaches, specifically when intercepting the glide slope (G/S) signal from above. The bulletin highlights incidents involving Boeing 737-800 and Airbus A340 aircraft where false glide slope signals caused sudden pitch-up maneuvers, risking stall conditions. It raises awareness among operators, Air Navigation Service Providers (ANSPs), and training organizations about this safety concern.
EASA SIB 2010-10R1
EASA Safety Information Bulletin 2010-10R1 is an informational document addressing fuel tank safety through the introduction of Flammability Reduction Systems (FRS) for high flammability exposure fuel tanks. It applies to Airbus A318, A319, A320, A321, A330, A340 and Boeing 737, 767, and 777 aircraft with center wing tanks manufactured from January 1, 2012. The bulletin provides background on the safety improvements following the TWA Flight 800 accident and outlines regulatory requirements for new production aircraft fuel tanks.
EASA SIB 2014-29
EASA Safety Information Bulletin 2014-29 provides clarification on the minimum cabin crew requirements for twin aisle aeroplanes including Airbus A300, A310, A330, A340, A380, A350 series, Boeing 747, 767, 777, 787, DC10, MD11 series, and Lockheed L1011 series. It explains the operational and certification regulations governing cabin crew numbers, emphasizing the need for at least one cabin crew member per emergency exit on twin aisle aircraft due to evacuation management challenges. The bulletin addresses misunderstandings arising from Commission Regulation (EU) No 965/2012 and highlights the importance of adequate cabin crew supervision for passenger safety during evacuations.
EASA SIB 2014-05
EASA Safety Information Bulletin SIB No. 2014-05 addresses incorrect installation of hydraulic pump electrical motor connectors on Airbus A330 and A340 aeroplanes. The bulletin covers multiple A330 and A340 variants and highlights issues related to internal arcing and fluid ingress caused by missing sealing plugs and incorrect sleeve installation. It provides information to raise awareness among operators and maintenance organizations about proper installation practices.
EASA SIB 2010-24
EASA Safety Information Bulletin 2010-24 is an informational bulletin addressing the Airbus A340 exhaust thrust reverser (TR) actuation system doors. It applies to Airbus A340 models -211, -212, -213, -311, -312, and -313 across all manufacturer serial numbers. The bulletin recommends installing warning placards on certain thrust reverser cowls to support previous modifications mandated by EASA Airworthiness Directive 2010-0044.
EASA SIB 2009-06R1
EASA Safety Information Bulletin 2009-06R1 is an informational bulletin addressing a software anomaly in certain Rockwell-Collins Multi-Mode Receivers (MMR) installed on various Boeing, Airbus, and Bombardier aircraft models. The anomaly causes a date roll-over error at midnight on 20/21 June 2009, resulting in the receiver reporting an incorrect date approximately 19.7 years off. Affected aircraft include Boeing 737, 747, 757, 767, 777, Airbus A300-600, A310, A320, A330, A340, A380, and Bombardier CL-600 series.
EASA SIB 2008-86
EASA Safety Information Bulletin No: 2008 – 86 is an informational document addressing uncertified aircraft configurations affecting Airbus A330 and A340 models. It highlights incidents where unauthorized Flight Control Primary Computer (FCPC) configurations caused elevator and spoiler control issues, leading to unsafe aircraft behavior. The bulletin covers all serial numbers of specified Airbus A330 and A340 variants.
EASA SIB 2008-35R1
EASA Safety Information Bulletin SIB No. 2008-35 Revision 1 is a safety information bulletin addressing critical parts for CFM56 series engines that may have been improperly repaired and approved for return to service. This bulletin applies to CFM56 engines installed on or held as spares for aircraft including Airbus A318, A319, A320, A321, A340 series, Boeing 737 series, and McDonnell Douglas DC-8-70 series. The bulletin references the FAA Special Airworthiness Information Bulletin NE-08-17 Revision 1.
EASA SIB 2007-43
EASA Safety Information Notice No. 2007-43 is an informational document regarding the FAA Airworthiness Directive 2007-23-01, which addresses issues with Goodrich Evacuation Systems installed on Airbus A330 and A340 series aircraft. The affected evacuation systems, qualified under TSO-C69b, have experienced pressure relief valve leakage that impacts raft mode functionality. This notice informs stakeholders that EASA has not adopted the FAA AD but considers it an interim solution.
EASA SIB 2007-12
EASA Safety Information Notice No. 2007-12 is a safety information notice addressing Airbus A330 and A340 aeroplanes, specifically models A330-200, A330-300, A340-200, A340-300, A340-500, and A340-600 series. The notice recommends installing a placard on passenger, crew, and emergency exit doors to ensure correct electrical harness routing for slide or slide/raft deployment.