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EASA Regulations & Airworthiness Directives

Browse 5,166 EASA regulations with AI-powered summaries.

Aircraft:All Airbus A320286 Airbus A321285 Airbus A319253 Airbus A350224 Airbus A330221 Airbus A318189 Airbus A380182 Boeing 737175 Airbus A340141 Airbus A350-941134 Airbus BD-500 (A220 Series)123 Airbus Helicopters AS 332119 Airbus Helicopters EC 225116 Airbus Helicopters SA 330116 Boeing 787116 Show all...

EASA SIB CE-13-09

Cessna 425 Aeroplanes — Cargo/Baggage Door

The Special Airworthiness Information Bulletin SAIB: CE-13-09 is an FAA advisory concerning the Cessna Model 425 airplanes. It addresses the issue of the nose baggage door or avionics door opening during flight and recommends pilots follow the emergency procedures in the Pilot’s Operating Handbook if this occurs. The bulletin clarifies that this concern does not currently warrant an airworthiness directive under 14 CFR part 39.

Safety Information Bulletin

Cessna 425

EASA SIB CE-13-10

M7 Aerospace (formerly Fairchild, Swearingen) SA26, SA226 and SA227 Aeroplanes — Windshields Heating Element Failures

The FAA Special Airworthiness Information Bulletin SAIB: CE-13-10 addresses windshield heating element failures in M7 Aerospace LLC SA26, SA226, and SA227 series airplanes. It highlights a potential overheating issue in certain modified windshields that could lead to glass damage and reduced pilot visibility. The bulletin provides safety information and recommendations but does not mandate regulatory action.

Safety Information Bulletin

M7 Aerospace SA26
M7 Aerospace SA226
M7 Aerospace SA227

EASA SIB SW-13-11

Robinson R44 Helicopters - Bladder Fuel Tank Retrofit

The Special Airworthiness Information Bulletin (SAIB) SW-13-11 issued by the FAA provides information about a fuel tank bladder retrofit program for Robinson Helicopter Company Model R44 and R44 II helicopters. This bulletin highlights the availability of a retrofit to replace aluminum fuel tanks with bladder-type tanks to enhance safety. The retrofit aims to reduce the risk of post-accident fuel leaks and potential fires in these helicopter models.

Safety Information Bulletin

Robinson R44
Robinson R44 II

EASA SIB 2012-21

WITHDRAWN - Temporary Degradation of EGNOS Performance

EASA Safety Information Bulletin 2012-21 is a notification regarding the temporary degradation of the European Geostationary Navigation Overlay Service (EGNOS) performance in the North and North East of Europe. This affects all aircraft certified for RNAV/GNSS approaches to LPV minima or LNAV/VNAV minima when using SBAS/GNSS altitude guidance. The bulletin informs that while the EGNOS Safety of Life service integrity remains uncompromised, there are periods of degraded performance impacting APV-I and Open Service accuracy, particularly around midnight UTC.

Safety Information Bulletin

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.

Safety Information Bulletin

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.

Safety Information Bulletin

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.

Safety Information Bulletin

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.

Safety Information Bulletin

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.

Safety Information Bulletin

Agusta 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.

Safety Information Bulletin

Airbus A318
Airbus A319
Airbus A320
Airbus 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.

Safety Information Bulletin

Saab 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.

Safety Information Bulletin

Boeing 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.

Safety Information Bulletin

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.

Safety Information Bulletin

Robinson 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.

Safety Information Bulletin

Airbus A318
Airbus A319
Airbus A320
Airbus 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.

Safety Information Bulletin

Airbus A318
Airbus A319
Airbus A320
Airbus 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.

Safety Information Bulletin

Cessna 177
Cessna F177
Cessna 182
Cessna F182
Cessna 206
Cessna 207
Cessna 210
Cessna 337
Cessna 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.

Safety Information Bulletin

Boeing 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.

Safety Information Bulletin

Bell 205A-1
Bell 205B
Bell 212
Bell 412CF
Bell 412EP
Bell UH-1B
Bell 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.

Safety Information Bulletin