EASA Regulations & Airworthiness Directives

Browse 220 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 787114Show all...
Filtered by: Airbus A330Clear filter

EASA AD 2018-0068

Mar 26, 2018

Superseded by EASA AD 2019-0059

EASA Airworthiness Directive 2018-0068 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A330 aeroplanes, including models A330-201 through A330-343. It mandates compliance with the Airbus A330 Airworthiness Limitations Section Part 2, Revision 02, which covers damage tolerant airworthiness limitation items. This directive ensures continued airworthiness by requiring specific maintenance tasks and inspections.

Airworthiness DirectiveSuperseded
  • Airbus A330

EASA AD 2018-0064

Mar 23, 2018

Hydraulic Power — Hydraulic Reservoir Pressure Relief Valve — Inspection / Replacement

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.

Other
  • Airbus A330
  • Airbus A340

EASA AD 2018-0062

Mar 20, 2018

Hydraulic Power — Ram Air Turbine Hydraulic Pumps — Replacement

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.

Airworthiness Directive
  • Airbus A330
  • Airbus A340

EASA AD 2017-0105R2

Mar 16, 2018

Electrical Power — Alternating Current Emergency Generation — Flight Warning Computer Software Update

Electrical Power — Alternating Current Emergency Generation — Flight Warning Computer Software Update is an Airworthiness Directive issued for the Airbus A330 aircraft. This directive addresses updates to the flight warning computer software related to the alternating current emergency power generation system to enhance system reliability and safety.

Airworthiness Directive
  • Airbus A330

EASA AD 2018-0019

Jan 26, 2018

Engine — Critical Parts — Reduction of Declared Safe Cyclic Life

EASA Airworthiness Directive 2018-0019 addresses the reduction of declared safe cyclic life for critical parts of Rolls-Royce RB211 Trent 700 engines, commonly installed on Airbus A330 aircraft. The directive mandates revised life limits for low pressure turbine shafts and removal of obsolete parts to ensure continued airworthiness. It applies to all serial numbers of RB211 Trent 768-60, 772-60, 772B-60, and 772C-60 engines.

Airworthiness Directive
  • Rolls-Royce Deutschland Ltd & Co Kg RB211 TRENT 700
  • Airbus A330

EASA AD 2018-0005

Jan 10, 2018

Fuselage — Fuselage Bulk Cargo Door Frames — Inspection / Repair

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.

Airworthiness Directive
  • Airbus A330
  • Airbus A340

EASA AD 2017-0245

Dec 11, 2017

Superseded by EASA AD 2018-0150

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.

Airworthiness DirectiveSuperseded
  • Airbus A330
  • Airbus A340

EASA AD 2014-0068R2

Dec 8, 2017

Fuselage — Trimmable Horizontal Stabilizer Support Struts — Inspection / Replacement

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.

Airworthiness Directive
  • Airbus A330
  • Airbus A340200300

EASA AD 2017-0241

Dec 6, 2017

Superseded by EASA AD 2018-0188

EASA Airworthiness Directive 2017-0241 is an airworthiness directive addressing Rolls-Royce RB211 Trent 700 engines installed on Airbus A330 aircraft. It mandates ultrasonic inspections and potential replacement of low pressure compressor blades to prevent blade release events that could cause engine damage or injury. The directive applies to specific part numbers of compressor blades and outlines inspection intervals and corrective actions.

Airworthiness DirectiveSuperseded
  • Rolls-Royce Deutschland Ltd & Co Kg RB211 TRENT 700
  • Airbus A330

EASA SIB 2010-10R1

Nov 28, 2014

Fuel Tank Safety — Flammability Reduction System (FRS) for High Flammability Exposure Fuel Tanks

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.

Safety Information Bulletin
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321
  • Airbus A330
  • Airbus A340
  • Boeing 737
  • Boeing 767
  • Boeing 777

EASA SIB 2014-29

Oct 24, 2014

WITHDRAWN: Comments received indicate the need for a review of applicable recommendation

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.

Safety Information Bulletin
  • Airbus A300
  • Airbus A310
  • Airbus A330
  • Airbus A340
  • Airbus A380
  • Airbus A350
  • Boeing 747
  • Boeing 767
  • Boeing 777
  • Boeing 787
  • McDonnell Douglas DC10
  • McDonnell Douglas MD11
  • Lockheed L1011

EASA SIB 2014-05

Feb 10, 2014

Airbus A330/A340 Aeroplanes - Hydraulic Pump Electrical Motor Connectors Incorrect Installation

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.

Safety Information Bulletin
  • Airbus A330
  • Airbus A340

EASA SIB NE-13-31

May 14, 2013

Pratt & Whitney PW4000 Engines — Scavenge Oil Tube Coking and Proper Cleaning at Overhaul

The Special Airworthiness Information Bulletin (SAIB) NE-13-31 issued by the FAA on May 9, 2013, addresses potential scavenge oil tube coking and nozzle blockage in Pratt & Whitney PW4000 series turbofan engines. This issue affects engines installed on aircraft such as the Airbus A300, A310, A330, Boeing 747-400, 767, 777, and McDonnell Douglas MD-11. The bulletin provides guidance on proper cleaning and inspection procedures during engine overhaul to prevent reduced oil flow and possible engine damage.

Safety Information Bulletin
  • Airbus A300
  • Airbus A310
  • Airbus A330
  • Boeing 747-400
  • Boeing 767
  • Boeing 777
  • McDonnell Douglas MD-11

EASA SIB 2012-07

May 9, 2012

Diehl Comfort Modules (formerly DASELL) Baby Nursing Tables - Hinge Replacement

EASA Safety Information Bulletin 2012-07 addresses the replacement of pivot-type hinges with piano-type hinges on Diehl Comfort Modules (formerly DASELL) baby nursing tables installed on Airbus A319, A320, A321, A300-600, A310, and A330 aircraft. The bulletin informs operators about reported incidents of finger injuries and infant entrapment caused by the folding mechanism of these nursing tables. It provides references to Airbus service bulletins and operator information telexes related to design improvements and safety measures.

Safety Information Bulletin
  • Airbus A319
  • Airbus A320
  • Airbus A321
  • Airbus A300-600
  • Airbus A310
  • Airbus A330

EASA SIB NE-11-27

Apr 6, 2011

General Electric CF6-80 Engines - Improperly Welded Fuel Nozzles

The FAA Special Airworthiness Information Bulletin SAIB: NE-11-27 addresses improperly welded fuel nozzles in General Electric CF6-80A, CF6-80C2, and CF6-80E1 series turbofan engines. These engines are installed on aircraft including Airbus A300, A310, A330, Boeing 747, 767, and McDonnell Douglas MD-11 series airplanes. The bulletin informs operators and maintenance personnel about the discovery of incomplete welds on specific fuel injector nozzles, which could lead to fuel leaks and potential engine shutdowns.

Safety Information Bulletin
  • Airbus A300
  • Airbus A310
  • Airbus A330
  • Boeing 747
  • Boeing 767
  • McDonnell Douglas MD-11

EASA SIB 2009-17

Jun 9, 2009

Unreliable Airspeed indication

EASA Safety Information Bulletin SIB No: 2009 - 17 addresses the issue of unreliable airspeed indication, highlighting risks observed during the Airbus A330 accident on 01 June 2009. The bulletin discusses potential causes such as pitot-static system malfunctions due to maintenance errors, contamination, environmental conditions, or water ingestion. It emphasizes the importance of flight crew familiarity with procedures to handle unreliable airspeed indications to maintain safe aircraft control.

Safety Information Bulletin
  • Airbus A330

EASA SIB 2009-06R1

May 26, 2009

WITHDRAWN - Rockwell-Collins GPS Receiver — Date Roll-Over Anomaly

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.

Safety Information Bulletin
  • Boeing 737
  • Boeing 747
  • Boeing 757
  • Boeing 767
  • Boeing 777
  • Airbus A300-600
  • Airbus A310
  • Airbus A320
  • Airbus A330
  • Airbus A340
  • Airbus A380
  • Bombardier CL-600

EASA SIB 2008-86

Nov 18, 2008

Airbus A330-A340 - Uncertified Aircraft Configuration

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.

Safety Information Bulletin
  • Airbus A330
  • Airbus A340

EASA SIB 2007-43

Nov 12, 2007

WITHDRAWN - SEE FAA AD 2012-06-25

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.

Safety Information Bulletin
  • Airbus A330
  • Airbus A340

EASA SIB 2007-12

Apr 24, 2007

Airbus A330 and A340 Aeroplanes - Installation of a Placard on Passenger/Crew and Emergency Exit Doors

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.

Safety Information Bulletin
  • Airbus A330
  • Airbus A340