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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 2010-10R1

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.

Nov 28, 2014
Safety Information BulletinSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321Airbus A330Airbus A340Boeing 737Boeing 767Boeing 777

EASA SIB NM-15-03

Boeing Aeroplanes — Inadvertent Actuation of Flight Deck Controls

The FAA Special Airworthiness Information Bulletin SAIB: NM-15-03 addresses an airworthiness concern regarding inadvertent actuation of flight deck controls on all Boeing transport category airplanes, specifically highlighting the Boeing 737-700 and 737-500 models. The bulletin informs operators about the risk of confusing the rudder trim switch with the flight deck door control switch, which can lead to unintended aircraft control inputs during flight.

Nov 27, 2014
Safety Information BulletinSafety MgmtFlight OpsBoeing 737-700Boeing 737-500

EASA SIB 2014-28R1

Ebola Virus Disease (EVD) — Operational Recommendations

EASA Safety Information Bulletin 2014-28R1 is an operational recommendation document addressing Ebola Virus Disease (EVD) risks in aviation. It provides guidance for National Aviation Authorities and aircraft operators on managing suspected communicable disease cases onboard aircraft, particularly related to EVD outbreaks in West Africa. The bulletin includes updated IATA guidelines for suspected communicable diseases and recommends equipping aircraft operating to or from affected countries with Universal Precaution Kits.

Nov 26, 2014
Safety Information BulletinFlight OpsSafety Mgmt

EASA SIB NE-14-30

Eastman Chemical Company (ECC) purchase of British Petroleum (BP) Turbine Engine Oil Products

The Special Airworthiness Information Bulletin SAIB: NE-14-30 issued by the FAA on October 1, 2014, informs aviation stakeholders about the Eastman Chemical Company (ECC) purchase of British Petroleum (BP) turbine engine oil products. The bulletin confirms that Eastman Turbo Oils (ETOs) are identical to the approved BP Turbo Oils (BPTOs) and are approved for use on certificated aircraft and engines. This applies to turbine engines and accessories using these oils.

Nov 21, 2014
Safety Information BulletinMaintenanceSafety Mgmt

EASA SIB CE-12-02R1

Cessna 172R/172S- Alternative Methods of Compliance (AMOC) for FAA AD 2001-06-17

The Cessna 172R/172S- Alternative Methods of Compliance (AMOC) for FAA AD 2001-06-17 is a Safety Information Bulletin addressing alternative compliance options for the FAA Airworthiness Directive 2001-06-17. It specifically concerns the Cessna 172R and 172S aircraft models. The bulletin provides guidance on acceptable alternative methods to meet the safety requirements outlined in the original AD.

Nov 14, 2014
Safety Information BulletinMaintenanceSafety MgmtCessna 172RCessna 172S

EASA SIB 2014-31

BRP-Powertrain Rotax 912 and 914 Engines Carburettor Float Non-Conformity

EASA Safety Information Bulletin SIB No. 2014-31 addresses a carburettor float non-conformity issue in BRP-Powertrain Rotax 912 and 914 engines. The affected carburettors and floats, identified by specific part numbers, are installed on various light aircraft including Cessna 150 series, Diamond Aircraft DA20-A1, and Tecnam P2006T among others. This bulletin informs operators and maintenance personnel about potential rough engine operation at low speeds caused by float buoyancy loss and fuel regulation issues.

Nov 7, 2014
Safety Information BulletinMaintenanceSafety MgmtBrp-Rotax Gmbh & Co Kg 912 ABrp-Rotax Gmbh & Co Kg 912 FBrp-Rotax Gmbh & Co Kg 912 SBrp-Rotax Gmbh & Co Kg 914 FCessna 150Diamond Aircraft DA20-A1Tecnam P2006T

EASA SIB 2014-29

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.

Oct 24, 2014
Safety Information BulletinFlight OpsSafety MgmtAirbus A300Airbus A310Airbus A330Airbus A340Airbus A380Airbus A350Boeing 747Boeing 767Boeing 777Boeing 787McDonnell Douglas DC10McDonnell Douglas MD11Lockheed L1011

EASA SIB SAFO14004

Garmin GRS 77/77H AHRS — Temporary Loss of Heading and Attitude Display

SAFO 14004 is a Safety Alert for Operators issued by the FAA addressing a temporary loss of heading and attitude display in aircraft equipped with Garmin GRS 77/77H AHRS systems. This issue affects several Garmin integrated flight deck systems including Garmin G1000, G1000H, G950, G900X, G500, G500H, G600, Cirrus Perspective™, and Embraer Prodigy®. The alert informs operators about potential heading drift and temporary loss of attitude information during critical phases of flight.

Sep 18, 2014
Safety Information BulletinFlight OpsSafety Mgmt

EASA SIB NM-14-21

Honeywell RTA 44D VHF Transceivers — Frequency Interference / Spurious Transmissions

The FAA Special Airworthiness Information Bulletin SAIB: NM-14-21 addresses frequency interference and spurious transmissions issues associated with Honeywell RTA 44D VHF transceivers installed on Airbus A318, A319, A320, and A321 series airplanes. The bulletin informs operators and maintenance personnel about off-frequency transmissions that can interfere with air traffic control communications but do not currently warrant an airworthiness directive. It highlights the affected Honeywell transceiver part numbers 064-50000-0202 and 064-50000-0505 and provides background on the issue and mitigation recommendations.

Sep 17, 2014
Safety Information BulletinMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA SIB NE-14-28

Use of NATO Grade F-24 Jet Fuel

The FAA Special Airworthiness Information Bulletin SAIB: NE-14-28 provides guidance on the use of NATO grade F-24 jet fuel in aircraft and engines certified for ASTM International D1655 grade Jet A fuel. It clarifies that F-24 jet fuel meets the performance requirements of Jet A fuel and is acceptable for use provided the fuel system icing inhibitor (FSII) concentration complies with the aircraft's operating limitations. This bulletin applies broadly to aircraft operators, FAA repair stations, and foreign civil aviation authorities.

Sep 17, 2014
Safety Information BulletinFlight OpsMaintenanceSafety Mgmt

EASA SIB CE-09-13R1

Piper PA-46 Aeroplanes - Engine Mount - Cracking at Nose Landing Gear

The Special Airworthiness Information Bulletin (SAIB) CE-09-13R1 issued by the FAA addresses potential cracking in the engine mounts of certain Piper PA-46 series airplanes, specifically the PA-46-310P, PA-46-350P, PA-46R-350T, and PA-46-500TP models. The cracks occur at the nose landing gear trunnion and actuator attachment points, which could affect the structural integrity of the engine mount. This bulletin provides updated service information and recommendations for inspections and replacements to mitigate the issue.

Aug 27, 2014
Safety Information BulletinMaintenanceSafety MgmtPiper PA-46-310PPiper PA-46-350PPiper PA-46R-350TPiper PA-46-500TP

EASA SIB CE-14-22

Piper PA-28 Aeroplanes — Fuel Selector/Shut-Off Valve

Special Airworthiness Information Bulletin SAIB: CE-14-22 is an FAA informational bulletin addressing a fuel selector valve issue in Piper Aircraft Models PA-28-140, PA-28-150, PA-28-160, PA-28-180, PA-28R-180, and PA-28R-200 airplanes. It highlights the risk of inadvertent fuel selector valve shutoff or binding during fuel tank switching, which can cause engine power loss in flight. The bulletin provides recommendations to prevent such occurrences but does not mandate regulatory action.

Aug 26, 2014
Safety Information BulletinMaintenanceSafety MgmtPiper PA-28-140Piper PA-28-150Piper PA-28-160Piper PA-28-180Piper PA-28R-180Piper PA-28R-200

EASA SIB CE-14-23

Piper PA-28, PA-32, PA-34, PA-44 and PA-46 Aeroplanes — Air Inlet Hose

The Special Airworthiness Information Bulletin SAIB: CE-14-23 is an FAA informational bulletin addressing an airworthiness concern for Piper Aircraft Models PA-28, PA-32, PA-34, PA-44, and PA-46 series airplanes. It highlights the risk of structural deterioration and possible collapse of the air inlet hose, which can reduce engine airflow and cause rough running or power loss. The bulletin does not mandate corrective action but provides important safety information for these Piper models.

Aug 26, 2014
Safety Information BulletinMaintenanceSafety MgmtPiper PA-28Piper PA-32Piper PA-34Piper PA-44Piper PA-46

EASA SIB 2014-16

[Corrected] Aeroplane Refuelling with One Engine Running

The [Corrected] Aeroplane Refuelling with One Engine Running is an EASA Safety Information Bulletin (SIB No. 2014-16) that provides guidance on the hazardous practice of hot refuelling multi-engine turbojet aeroplanes, specifically with Jet-A and Jet-A1 fuels. It addresses procedures for refuelling with one engine operating, typically in exceptional circumstances such as Auxiliary Power Unit (APU) unserviceability. The bulletin applies to commercial and non-commercial operators of multi-engine turbojet aircraft.

Jul 1, 2014
Safety Information BulletinFlight OpsSafety Mgmt

EASA SIB 2014-20

Aeroplane Operations in Crosswind Conditions

EASA Safety Information Bulletin No. 2014-20 titled 'Aeroplane Operations in Crosswind Conditions' provides guidance for aeroplane manufacturers, operators, flight crews, and training organisations on managing operations under strong and gusty crosswind conditions. It highlights findings from studies involving CS-25 certified aeroplanes in commercial air transport, emphasizing the importance of clear understanding and procedures related to maximum demonstrated crosswind limits. The bulletin does not target specific aircraft models but applies broadly to large aeroplanes certified under CS-25.

Jun 23, 2014
Safety Information BulletinFlight OpsTrainingSafety Mgmt

EASA SIB 2014-19

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. 2014-19 notifies aviation stakeholders about unapproved aircraft parts and equipment, specifically including components installed on AgustaWestland A109 helicopters. The bulletin lists several parts such as watches, an antenna, and a fuel filter that were lost during operator transfers and are now considered unapproved for installation. This document serves as an informational notice regarding these unapproved parts.

Jun 17, 2014
Safety Information BulletinMaintenanceSafety MgmtAgustaWestland A109

EASA SIB 2014-18

Notification of Unapproved Parts due to theft

EASA Safety Information Bulletin SIB No. 2014-18 notifies aviation professionals about unapproved parts resulting from theft at Cyprus Airways between February and May 2013. The affected parts include electronic engine controls by Hamilton Sundstrand, avionics systems by Airbus France, and other components from manufacturers such as Diehl Aerospace, Woodward Governor, Honeywell, Messier-Bugatti Dowty, and Goodrich Control Systems. These parts are considered unapproved and must not be installed on any aircraft.

Jun 11, 2014
Safety Information BulletinMaintenanceSafety Mgmt

EASA SIB 2014-17

Aeroplane Mode Awareness During Final Approach

EASA Safety Information Bulletin 2014-17 addresses aeroplane mode awareness during final approach, focusing on Airbus A320 aircraft. It highlights incidents involving low airspeed and energy conditions linked to the use of OPEN DESCENT mode and the activation of Alpha Floor protection during approach. The bulletin emphasizes the importance of pilot understanding of automated flight modes and energy management in critical flight phases.

Jun 10, 2014
Safety Information BulletinFlight OpsSafety MgmtTrainingAirbus A320

EASA SIB NM-14-20

Boeing 747-8F Aeroplanes modified by Telair International, Inc. STC ST02367LA — Cargo Compartments

The Boeing 747-8F Aeroplanes modified by Telair International, Inc. STC ST02367LA — Cargo Compartments is a Special Airworthiness Information Bulletin (SAIB NM-14-20) issued by the FAA. It addresses an airworthiness concern related to the cargo handling system on Boeing 747-8F aircraft modified with this supplemental type certificate. The bulletin informs operators about potential uncontrolled movement of Unit Load Devices (ULDs) during cargo loading operations due to Power Drive Units entering sleep mode.

Jun 5, 2014
Safety Information BulletinSafety MgmtMaintenanceBoeing 747-8F

EASA SIB CE-14-19

Cessna 310, 401, 402, 411, 414 and 421 series Aeroplanes — MLG Torque Link

The FAA Special Airworthiness Information Bulletin SAIB: CE-14-19 addresses an airworthiness concern related to the main landing gear (MLG) torque link assembly on Cessna 300 and 400 series airplanes, including models 310P, 310Q, 310R, 401, 401A, 401B, 402, 402A, 402B, 402C, 411, 411A, 414, 414A, 421, 421A, 421B, and 421C. The bulletin highlights the need to inspect and ensure the correct thickness and positioning of washers in the MLG torque link assembly. This information bulletin is advisory and does not mandate regulatory action under 14 CFR part 39.

Jun 4, 2014
Safety Information BulletinMaintenanceSafety MgmtCessna 310PCessna 310QCessna 310RCessna 401Cessna 401ACessna 401BCessna 402Cessna 402ACessna 402BCessna 402CCessna 411Cessna 411ACessna 414Cessna 414ACessna 421Cessna 421ACessna 421BCessna 421C