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EASA Regulations & Airworthiness Directives

Browse 4771 EASA regulations with AI-powered summaries.

Aircraft:AllAirbus A320262Airbus A321257Airbus A319229Airbus A350206Airbus A330197All177Airbus A318172Boeing 737164Airbus A380162Airbus A340136Airbus A350-941119Airbus Helicopters AS 332110Airbus Helicopters EC 225107Airbus Helicopters SA 330107Boeing 787106Show all...

EASA SIB SW-13-08

Aspen Avionics EFD1000 and EFD500 Multifunction Displays

The FAA Special Airworthiness Information Bulletin SAIB: SW-13-08 addresses an issue with Aspen Avionics EFD1000 and EFD500 Multifunction Displays (MFD) where the displays may unintentionally reset when processing a large number of Temporary Flight Restrictions (TFRs). This bulletin applies to aircraft equipped with these Aspen Avionics MFDs connected to sources receiving TFR data, such as XM Satellite receivers. The primary flight displays are not affected by this reset issue.

Dec 14, 2012
Safety Information BulletinSafety Mgmt

EASA SIB NE-13-06

Lycoming 320, 360 and 540 Series Engines with Engine Components International (ECi) Pushrod Shroud Spring Retainers installed

The Special Airworthiness Information Bulletin (SAIB) NE-13-06 issued by the FAA addresses an airworthiness concern involving Engine Components International (ECi) pushrod shroud spring retainers, part number AEL14995, installed on Lycoming Engines 320, 360, and 540 series reciprocating parallel valve engines. The bulletin informs owners, operators, and certified repair facilities about potential failures of these retainers that may cause pushrod tubes or shrouds to loosen and possibly leak oil. The document provides guidance on identifying and replacing older designs of these retainers to maintain engine reliability.

Nov 22, 2012
Safety Information BulletinMaintenanceSafety Mgmt

EASA SIB SW-13-05

Weber Aircraft LLC Seats — Rear Track Fittings P/N 840620-401/-403 Incorrect Installation

The FAA Special Airworthiness Information Bulletin SAIB: SW-13-05 addresses potential incorrect installation of rear track fittings, part numbers 840620-401 and 840620-403, on Weber Aircraft LLC seat models 4001, 4004, 5150, 5200, 6002, 6200, 7001, 7501, 7502, 8000, and 8001 installed in transport category aircraft. This bulletin provides information and recommendations but does not mandate regulatory action. It highlights concerns about loose seat installations related to improper rear seat track fitting installation or maintenance.

Nov 22, 2012
Safety Information BulletinMaintenanceSafety Mgmt

EASA SIB NE-13-04

Continental Motors, Inc. — Connecting Rod Piston Pin Bushing Inspection

The FAA Special Airworthiness Information Bulletin NE-13-04 provides guidance on inspecting the connecting rod piston pin bushings in all Continental Motors, Inc. (CMI) series engines. It alerts owners, operators, and certified repair facilities to inspect these components during cylinder removal or when piston pin bushing material is found during routine maintenance. This bulletin applies to all models of CMI series engines and aims to ensure continued airworthiness without mandating regulatory action.

Nov 21, 2012
Safety Information BulletinMaintenanceSafety Mgmt

EASA SIB SW-12-45

Garmin 400W/500W GPS-WAAS Navigation System

The FAA Special Airworthiness Information Bulletin SAIB: SW-12-45 addresses an airworthiness concern related to the Garmin Model 400W/500W series GPS-WAAS Navigation System installed on Part 27 helicopters listed on the Approved Model List of Supplemental Type Certificate SR02232LA, excluding the Agusta S.p.A Model A109A-II. This bulletin provides information for owners and operators about installation compliance issues but does not mandate corrective action. The Agusta S.p.A Model A109A-II is now the only model approved for installation under the amended STC SR02232LA.

Nov 21, 2012
Safety Information BulletinMaintenanceSafety MgmtAgusta S.p.A A109A-II

EASA SIB 2012-16R1

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.

Nov 21, 2012
Safety Information BulletinMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA SIB 2012-20

WITHDRAWN - RECOMMENDATIONS NOT NEEDED ANYMORE

EASA Safety Information Bulletin SIB No. 2012-20 titled "WITHDRAWN - RECOMMENDATIONS NOT NEEDED ANYMORE" addresses the impact of thickened de/anti-icing fluids on aircraft performance. It specifically references a serious incident involving the Saab 340 aircraft at Helsinki/Vantaa Airport in 2010, where thickened fluids affected elevator control during take-off. The bulletin discusses regulatory context and certification specifications related to the use of these fluids on all aeroplanes.

Nov 20, 2012
Safety Information BulletinSafety MgmtFlight OpsSaab 340

EASA SIB NM-13-02

Boeing 747-8F Aeroplanes - Improper installation of Air Distribution System Riser Duct and Manifold Assemblies

The FAA Special Airworthiness Information Bulletin SAIB: NM-13-02 addresses an airworthiness concern related to the improper installation of air distribution system riser duct and manifold assemblies on Boeing 747-8F airplanes. This bulletin informs registered owners and operators about potential leaks and damage in the main deck air distribution system that can reduce cabin airflow. It provides guidance based on Boeing's Special Attention Service Bulletin 747-21-2541 for inspection and corrective actions.

Oct 25, 2012
Safety Information BulletinMaintenanceSafety MgmtBoeing 747-8F

EASA SIB NM-13-01

Large (JAR/FAR/CS 25) Aeroplanes — Discrepant Windows and Windshields

The FAA Special Airworthiness Information Bulletin SAIB: NM-13-01 addresses airworthiness concerns related to discrepant windows and windshields repaired by Aircraft Transparencies Repair (ATR) and related companies on large transport category airplanes. The bulletin highlights issues with repairs performed between January 2007 and the present, affecting windshields, cockpit side windows, passenger windows, and wingtip lenses. No specific aircraft models or part numbers are listed, but affected parts can be identified through maintenance records showing FAA Form 8130-3 approvals by ATR or associated entities.

Oct 25, 2012
Safety Information BulletinMaintenanceSafety Mgmt

EASA SIB 2012-18

Potential effects of inflated floats or float-type landing gears on flight characteristics of helicopters

EASA Safety Information Bulletin SIB No. 2012-18 addresses the potential effects of inflated floats or float-type landing gears on the flight characteristics of helicopters, specifically referencing the Robinson R22 Mariner. The bulletin highlights incidents involving European registered helicopters fitted with float-type landing gear during simulated engine failure and autorotation descent maneuvers. It aims to raise pilot awareness about altered handling characteristics caused by these float systems.

Oct 25, 2012
Safety Information BulletinFlight OpsSafety MgmtTrainingRobinson R22 Mariner

EASA SIB 2012-17

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.

Sep 20, 2012
Safety Information BulletinMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA SIB 2012-15R1

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.

Aug 24, 2012
Safety Information BulletinSafety MgmtMaintenanceAirbus A318Airbus A319Airbus A320Airbus A321

EASA SIB CE-12-41

Cessna (incl. formerly Reims Aviation) 177, F177, 182, F182, 206, 207, 210, 337 and F337 Series Aeroplanes — Flight Control Column Loose Glide Screw

The Special Airworthiness Information Bulletin SAIB: CE-12-41 is an FAA advisory concerning a potential loose glide screw in the flight control columns of various Cessna aircraft models, including the 177, F177, 182, F182, 206, 207, 210, 337, and F337 series. This bulletin informs owners, operators, and maintenance personnel about the risk of the glide screw backing out and jamming the elevator control system. The affected screw part numbers are NAS220-14 and MS27039-0814.

Aug 14, 2012
Safety Information BulletinMaintenanceSafety MgmtCessna 177Cessna F177Cessna 182Cessna F182Cessna 206Cessna 207Cessna 210Cessna 337Cessna F337

EASA SIB NM-12-40

Boeing 747-400 Aeroplanes — External Power System Connector

The FAA Special Airworthiness Information Bulletin SAIB: NM-12-40 addresses an airworthiness concern for Boeing 747-400 series airplanes related to the external power system connector. The bulletin highlights issues caused by damage to the safety guide on the external power receptacle, which can lead to incorrect connection and electrical short circuits. This information bulletin provides guidance to operators to prevent damage and potential fire risks associated with ground power connections.

Aug 7, 2012
Safety Information BulletinMaintenanceSafety MgmtBoeing 747-400

EASA SIB SW-12-38

Bell (BHTI) 205A-1, 205B, 212, 412CF and 412EP helicopters — Emergency (Push Out) Passenger Door Windows

The FAA Special Airworthiness Information Bulletin SAIB: SW-12-38 addresses the potential risk of in-flight loss of emergency "push out" passenger door windows on Bell Helicopter models 205A-1, 205B, 212, 412CF, 412EP, and restricted category UH-1B and UH-1H helicopters. This bulletin provides information about the issue without mandating regulatory action. It highlights concerns related to the bonding quality of window retainers on composite passenger doors.

Aug 6, 2012
Safety Information BulletinSafety MgmtMaintenanceBell 205A-1Bell 205BBell 212Bell 412CFBell 412EPBell UH-1BBell UH-1H

EASA SIB 2012-13

Improved protection of balloon basket occupants during firm landings

EASA Safety Information Bulletin 2012-13 provides guidance on improving the protection of balloon basket occupants during firm landings, particularly for passengers unfamiliar with such conditions. It applies to all balloon baskets used for carrying occupants and offers recommendations to enhance occupant safety without mandating regulatory changes. The bulletin does not target specific aircraft or engine models but focuses on hot-air and gas balloon operations.

Aug 3, 2012
Safety Information BulletinSafety MgmtTraining

EASA SIB 2012-14

Improving the safety of aiders on the ground when relocating an inflated hot air balloon

EASA Safety Information Bulletin 2012-14 is an informational document addressing the safety of aiders on the ground when relocating an inflated hot air balloon. It applies to all hot air balloons and highlights risks associated with aiders holding the basket's carrying handles during relocation. The bulletin recommends using a device called a “Spider” to improve safety and coordination during ground handling.

Aug 3, 2012
Safety Information BulletinSafety Mgmt

EASA SIB FA-24-2012

EMBRAER ERJ 170/175 and ERJ 190/195 Aeroplanes — Landing Gear — Brake Carbon Disks Damage

The EMBRAER ERJ 170/175 and ERJ 190/195 Aeroplanes — Landing Gear — Brake Carbon Disks Damage Flight Alert FA Nº 24/2012 is a regulatory document addressing brake carbon disk damage issues on these aircraft models. It informs operators about potential carbon disk brake failures during normal operation that can lead to runway contamination by brake debris. The alert provides updated maintenance instructions to detect and prevent brake assembly failures.

Jun 29, 2012
Safety Information BulletinMaintenanceSafety MgmtEmbraer ERJ 170Embraer ERJ 175Embraer ERJ 190Embraer ERJ 195

EASA SIB 2012-12

WITHDRAWN - Current status can be followed on the EASA SUP website: https://www.easa.europa.eu/en/domains/aircraft-products/suspected-unapproved-parts.

EASA Safety Information Bulletin SIB No. 2012-12 notifies aviation stakeholders about unapproved aircraft parts due to theft from an aircraft parked long-term since 2009. The bulletin lists specific stolen parts and equipment, including components from Honeywell, B/E Aerospace, Auxilec/Thales, and others, affecting various aircraft. The document highlights that these parts are unapproved and should not be installed on any aircraft.

Jun 28, 2012
Safety Information BulletinMaintenanceSafety Mgmt

EASA SIB 2012-11

Tyre Specification(s) and Installation

EASA Safety Information Bulletin SIB No. 2012-11 titled "Tyre Specification(s) and Installation" addresses issues related to tyre specifications and installation on aeroplanes with retractable landing gears, including the Diamond DA 42. The bulletin highlights a safety concern where a gear-up landing occurred due to a tyre outer diameter deviation caused by using a tyre brand different from that specified by the manufacturer. It applies to all aeroplanes certified or validated by EASA under CS-23, CS-VLA, CS-22, or CS-LSA, or certified by European National authorities before 28 September 2003 under equivalent standards.

Jun 27, 2012
Safety Information BulletinMaintenanceSafety MgmtDiamond DA 42