EASA Regulations & Airworthiness Directives

Browse 189 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 A318Clear filter

EASA SIB 2013-03

Jan 28, 2013

Seat Track Monument Fittings Replacement

EASA Safety Information Bulletin SIB No: 2013-03 titled 'Seat Track Monument Fittings Replacement' addresses concerns related to seat track lower attachment fittings Part Number ABS1262C010 installed on Airbus A318, A319, A320, A321, A330-243, and A330-343 aircraft. The bulletin informs operators about engineering static load test failures indicating these fittings may not meet required load specifications. It highlights that while Airbus-installed fittings comply with certification requirements, fittings installed via Supplemental Type Certificate modifications may pose a safety risk.

Safety Information Bulletin
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321
  • Airbus A330-243
  • Airbus A330-343

EASA SIB 2012-16R1

Nov 21, 2012

Hydraulic Systems — Implementation of automatic Power Transfer Unit inhibition logic

EASA Safety Information Bulletin 2012-16R1 is an informational bulletin addressing hydraulic system improvements on Airbus A318, A319, A320, and A321 aircraft. It informs operators about the implementation of automatic Power Transfer Unit (PTU) inhibition logic designed to prevent overheating and failure of a second hydraulic system following a single hydraulic system failure with fluid loss. The bulletin references Airbus Service Bulletins that provide retrofit and activation instructions for this safety enhancement.

Safety Information Bulletin
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA SIB 2012-17

Sep 20, 2012

CFM International CFM56-5B engines — High Cycle Fatigue Failure of Low Pressure Turbine Active Clearance Control Fuel Manifolds

EASA Safety Information Bulletin 2012-17 is an advisory document addressing high cycle fatigue failure of Low Pressure Turbine Active Clearance Control (LPTACC) fuel manifolds on CFM International CFM56-5B turbofan engines. These engines are installed on Airbus A318, A319, A320, and A321 aircraft. The bulletin aligns with FAA Special Airworthiness Information Bulletin NE-12-29 and informs European operators and maintenance organizations about the issue and recommended actions.

Safety Information Bulletin
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA SIB 2012-15R1

Aug 24, 2012

Airbus A318, A319, A320 and A321 aeroplanes — VHF Interference on 135.985 and 135.97 MHz

EASA Safety Information Bulletin 2012-15R1 addresses VHF radio interference issues on frequencies 135.97 MHz and 135.985 MHz affecting Airbus A318, A319, A320, and A321 aeroplanes. The bulletin informs operators about interference caused by certain Electronic Instrument System 1 Display Units, which generate background noise detectable by flight crews. It provides information on the origin of the interference and references Airbus Service Bulletin A320-31-1105 for corrective actions.

Safety Information Bulletin
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA SIB 2010-27

Sep 10, 2010

Airbus A318/A319/A320/A321 — Evacuation Systems - Coupling Pin Verification

EASA Safety Information Bulletin 2010-27 is an informational document addressing evacuation system issues on Airbus A318, A319, A320, and A321 aircraft. It highlights incidents where evacuation slides failed to deploy due to missing coupling pins in the reservoir and valve assemblies. The bulletin provides guidance to operators and maintenance organizations to verify and correct the installation of coupling pins in affected slide reservoirs.

Safety Information Bulletin
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA SIB 2010-25

Aug 27, 2010

Cabin Oxygen Mask Service Recommendations from Original Equipment Manufacturers, and Cabin Oxygen Masks with B/E Aerospace In-line Flow Indicators Part Number (P/N) 118023-02

EASA Safety Information Bulletin SIB No. 2010-25 provides service recommendations regarding cabin oxygen masks equipped with B/E Aerospace in-line flow indicators part number 118023-02. The bulletin applies to CS1-23 and CS-25 category aeroplanes, including Airbus A318, A319, A320, A321, Boeing 737, 747, 757, 767, 777, and Fokker F28 models. It addresses failures of the in-line flow indicators that can cause oxygen flow interruption during use.

Safety Information Bulletin
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321
  • Boeing 737
  • Boeing 747
  • Boeing 757
  • Boeing 767
  • Boeing 777
  • Fokker F28

EASA SIB 2010-16

Apr 19, 2010

Baby Bassinet Detachment

EASA Safety Information Bulletin 2010-16 addresses the detachment incident of the Innovint 7250 series baby bassinet from cabin partition walls on Airbus A318/A319/A320/A321 aircraft. The bulletin provides safety information following a reported event where the bassinet detached and caused minor injuries to a baby occupant. It includes updated installation instructions and maintenance requirements to ensure secure attachment during flight.

Safety Information Bulletin
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA SIB 2008-35R1

May 26, 2008

WITHDRAWN - FAA SAIB NE-08-17R3 TRANSFERRED TO EASA SUP WEBPAGE

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.

Safety Information Bulletin
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321
  • Airbus A340
  • Boeing 737
  • McDonnell Douglas DC-8

EASA SIB 2008-10

Feb 14, 2008

Airbus A318/A319/A320/A321 Standard Operating Procedures - Ground Spoilers do not Deploy Automatically After Landing

EASA Safety Information Notice No. 2008-10 is a safety information notice addressing the Airbus A318, A319, A320, and A321 aircraft. It highlights an issue where ground spoilers do not deploy automatically after landing if one throttle lever remains above idle, which can inhibit autobrake activation and contribute to landing overruns. The document provides updated standard operating procedures to mitigate this risk.

Safety Information Bulletin
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321