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EASA Regulations & Airworthiness Directives

Browse 4771 EASA regulations with AI-powered summaries.

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EASA SIB CE-08-13

Piper PA-28, PA-32, PA-34, PA-44 and PA-46 - Possible Failure of a Transient Voltage Suppressor (TVS)

Special Airworthiness Information Bulletin SAIB: CE-08-13 is an FAA informational bulletin addressing a potential failure of Transient Voltage Suppressor (TVS) devices in Piper aircraft models PA-28, PA-32, PA-34, PA-44, and PA-46. The affected aircraft include the PA-28-161 Warrior III, PA-28-181 Archer III, PA-28R-201 Arrow, PA-32R-301 Saratoga II TC and HP variants, PA-32-301FT 6X, PA-32-301XTC 6XT, PA-34-200T Seneca V, PA-44-180 Seminole, PA-46-350P Mirage, and PA-46-500TP Meridian. This bulletin informs operators of possible TVS failures that may increase pilot workload but does not mandate corrective action.

May 11, 2011
Safety Information BulletinMaintenanceSafety MgmtPiper PA-28-161 Warrior IIIPiper PA-28-181 Archer IIIPiper PA-28R-201 ArrowPiper PA-32R-301 Saratoga II TCPiper PA-32R-301 HPPiper PA-32-301FT 6XPiper PA-32-301XTC 6XTPiper PA-34-200T Seneca VPiper PA-44-180 SeminolePiper PA-46-350P MiragePiper PA-46-500TP Meridian

EASA SIB 2008-20

WITHDRAWN - FAA SAIB CE-08-12R1, CE-08-13 AND CE-08-14 NOW DIRECTLY ENDORSED

The document titled WITHDRAWN - FAA SAIB CE-08-12R1, CE-08-13 AND CE-08-14 NOW DIRECTLY ENDORSED is an EASA Safety Information Notice No. 2008-20 issued on 2008-03-07. It addresses an airworthiness concern related to the failure of transient voltage suppressors (TVS) in certain aircraft, as identified in FAA Special Airworthiness Information Bulletins CE-08-12, CE-08-13, and CE-08-14. The affected aircraft are those specified in the referenced FAA SAIBs, including models from Cirrus Design Corporation, Piper Aircraft, and Garmin equipment.

May 11, 2011
Safety Information BulletinMaintenanceSafety MgmtCirrus Design CorporationPiper Aircraft

EASA SIB 2011-06

WITHDRAWN - RECOMMENDATIONS NOT NEEDED ANYMORE

EASA Safety Information Bulletin SIB No. 2011-06 provides information regarding the separation of the Main Entry Door (MED) during flight on Gulfstream Aerospace LP (GALP) Model 1125 Astra Westwind, Astra SPX, and G100 aircraft. The bulletin addresses an incident involving a Gulfstream G100/Astra where the MED opened and separated during climb-out, with no injuries reported. It references related airworthiness directives issued by the Civil Aviation Authority of Israel (CAAI) and adopted by EASA and FAA.

May 5, 2011
Safety Information BulletinSafety MgmtMaintenanceGulfstream Aerospace LP 1125 Astra WestwindGulfstream Aerospace LP Astra SPXGulfstream Aerospace LP G100

EASA SIB 2011-07

WITHDRAWN - RECOMMENDATIONS NOT NEEDED ANYMORE. Topic addressed by Commission Regulation (EU) No 965/2012

EASA Safety Information Bulletin (SIB) No. 2011-07 titled 'WITHDRAWN - RECOMMENDATIONS NOT NEEDED ANYMORE. Topic addressed by Commission Regulation (EU) No 965/2012' addresses safety concerns related to functional check flights on all aircraft operated under an Air Operator Certificate (AOC), including Airbus A320, Boeing 737, and Dassault Falcon 2000. The bulletin highlights recent accidents during non-revenue flights conducted for maintenance checks or lease transfers and raises awareness of associated hazards.

May 5, 2011
Safety Information BulletinFlight OpsSafety MgmtAirbus A320Boeing 737Dassault Falcon 2000

EASA SIB CE-11-28

Hawker Beechcraft Corporation (formerly Raytheon, Beechcraft) 55, 56, 58 and 95-55 series - Fuel & Electrical Systems

The FAA Special Airworthiness Information Bulletin CE-11-28 is an informational document addressing fuel and electrical system concerns on Hawker Beechcraft Corporation Model 55, 56, 58, and 95-55 series Baron twin-engine airplanes. It highlights incidents of in-flight and ground fires related to fuel vent lines and electrical wiring arcing, aiming to raise awareness among owners, operators, and maintenance personnel. This bulletin does not mandate regulatory action but provides safety recommendations.

Apr 11, 2011
Safety Information BulletinMaintenanceSafety MgmtHawker Beechcraft 55Hawker Beechcraft 56Hawker Beechcraft 58Hawker Beechcraft 95-55

EASA SIB NM-11-25

AVOX Systems - Passenger Supplemental Oxygen Masks on Transport Aeroplanes

The FAA Special Airworthiness Information Bulletin SAIB: NM-11-25 addresses issues with passenger supplemental oxygen masks manufactured by AVOX Systems, specifically those with Scott part numbers 289-601, 289-701, 289-801, 289-601-441-1, 289-1001, 289-1002, 289-1020, and 289-1030, installed on transport category airplanes. This bulletin informs operators about failures in the in-flow indicators of these oxygen masks and provides guidance to maintain their effectiveness during emergencies. The document is informational and does not impose mandatory requirements.

Apr 6, 2011
Safety Information BulletinSafety MgmtMaintenance

EASA SIB NE-11-27

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.

Apr 6, 2011
Safety Information BulletinMaintenanceSafety MgmtAirbus A300Airbus A310Airbus A330Boeing 747Boeing 767McDonnell Douglas MD-11

EASA SIB NE-08-26R3

Lycoming Engines - TCM Ignition Systems (formerly Bendix) D2000 and D3000 Dual Magnetos

The Lycoming Engines - TCM Ignition Systems (formerly Bendix) D2000 and D3000 Dual Magnetos Special Airworthiness Information Bulletin (SAIB: NE-08-26R3) is an FAA informational bulletin addressing the risk of magneto separation from Lycoming four, six, and eight cylinder reciprocating engines equipped with TCM Series D2000 and D3000 Dual Magnetos. This bulletin specifically highlights issues found mostly in Lycoming IO-360-A1B6D and IO-360-A3B6D engines installed on Mooney M20J-201 and Cessna 177RG aircraft. It provides guidance on inspection, maintenance, and proper gasket and clamp usage to prevent magneto separation and subsequent engine power loss.

Apr 6, 2011
Safety Information BulletinMaintenanceSafety MgmtMooney M20J-201Cessna 177RG

EASA SIB NE-11-22

Rolls-Royce Corporation AE 3007 Engines — Replacement of Full Authority Digital Electronic Control (FADEC) Part Number 23073177

Special Airworthiness Information Bulletin SAIB: NE-11-22 is an FAA informational bulletin addressing Rolls-Royce Corporation AE 3007C and AE 3007C1 turbofan engines equipped with Full Authority Digital Electronic Control (FADEC) hardware part number 23073177. These engines, installed on aircraft such as the Cessna Citation 750, may experience uncommanded in-flight engine shutdowns due to electrical issues. The bulletin provides guidance to operators and maintenance personnel to mitigate this risk.

Apr 6, 2011
Safety Information BulletinMaintenanceSafety MgmtCessna Citation 750

EASA SIB NM-11-23

Boeing 767-400ER - Main Landing Gear Truck Beam

The FAA Special Airworthiness Information Bulletin SAIB: NM-11-23 addresses an airworthiness concern involving the main landing gear truck beam on Boeing 767-400ER airplanes. It informs operators about corrosion damage found in the inner bore of the main landing gear truck beam that led to a fracture and partial collapse during taxi. The bulletin provides guidance on inspection and maintenance to prevent similar issues.

Apr 5, 2011
Safety Information BulletinMaintenanceSafety MgmtBoeing 767-400ER

EASA SIB CE-11-26

M7 Aerospace (Fairchild, Swearingen) SA226/SA227 Aeroplanes - Wing Leading Edge Skins and Doublers Inspection / Repair

The FAA Special Airworthiness Information Bulletin SAIB: CE-11-26 provides guidance for registered owners and operators of M7 Aerospace LP SA226 and SA227 model aircraft regarding inspection and repair of wing leading edge skins and doublers at wing station 78. It addresses cracking concerns in part numbers 27-31000 (wing skin) and 27-35084 (doubler) and offers inspection and repair procedures without mandating compliance. This bulletin applies to aircraft under type certificate data sheets A5SW, A8SW, and A18SW.

Mar 31, 2011
Safety Information BulletinMaintenanceSafety MgmtM7 Aerospace SA226M7 Aerospace SA227

EASA SIB 2010-30R1

WITHDRAWN - REPLACED BY EASA SIB 2025-03

EASA Safety Information Bulletin 2010-30R1 is a safety information bulletin addressing risks associated with transporting lithium batteries as cargo on all aeroplanes and helicopters. It references FAA and ICAO publications to highlight the importance of adhering to ICAO Technical Instructions for the safe transport of dangerous goods by air. The bulletin is intended for aircraft operators registered in European Union Member States and associated countries.

Mar 31, 2011
Safety Information BulletinSafety Mgmt

EASA SIB SW-11-24

Garmin 400/500 series GPS on Rotorcraft with Aeroplane (fixed-wing) TAWS Function Activated

The FAA Special Airworthiness Information Bulletin SAIB: SW-11-24 addresses the use of Garmin 400/500 series GPS Navigation Systems with the airplane Terrain Awareness and Warning System (TAWS) function activated on rotorcraft. It highlights that these TAWS functions are designed for fixed-wing airplanes and are not approved for rotorcraft, such as helicopters, due to differences in operational altitudes and system algorithms. The bulletin specifically mentions rotorcraft equipped with these Garmin systems and the Bell 206B helicopter model with an approved HTAWS STC.

Mar 29, 2011
Safety Information BulletinFlight OpsSafety MgmtBell 206B

EASA SIB 2011-05

ROLLS ROYCE DEUTSCHLAND engines - Bearing Support Housing - Notification of Non-conforming Parts

EASA Safety Information Bulletin SIB No. 2011-05 is a notification regarding Rolls Royce Deutschland BR700-710 engines. It addresses non-conforming Bearing Support Housing parts, specifically Part Number FW34006, which have a defective chamfer at the RDS roller bearing location. This issue may reduce the bearing life and affect engine reliability.

Mar 29, 2011
Safety Information BulletinMaintenanceSafety Mgmt

EASA SIB 2011-03

Advisory Vertical Guidance

EASA Safety Information Bulletin SIB No. 2011-03 titled Advisory Vertical Guidance addresses the use of advisory vertical guidance systems in General Aviation aircraft during Non Precision Approaches. It explains that such guidance may be based on GNSS, SBAS augmentations like EGNOS or WAAS, barometric altimetry, or other means, but these systems are not approved for official vertical guidance. The bulletin applies specifically to General Aviation aircraft equipped with advisory vertical guidance systems.

Mar 24, 2011
Safety Information BulletinFlight OpsSafety Mgmt

EASA SIB 2011-04

WITHDRAWN - RECOMMENDATIONS NOT NEEDED ANYMORE

EASA Safety Information Bulletin SIB No. 2011-04 titled 'WITHDRAWN - RECOMMENDATIONS NOT NEEDED ANYMORE' addresses the nuclear emergency in Japan following the 9.0 magnitude earthquake and tsunami on March 11, 2011. It applies to all commercial air transport flights to and from Japan operated by EASA States. The bulletin provides information on the establishment of a flight prohibited area around the Fukushima No. 1 nuclear power plant and references relevant safety guidelines and monitoring resources but does not specify affected aircraft types or engines.

Mar 22, 2011
Safety Information BulletinFlight OpsSafety Mgmt

EASA SIB 2011-02

ATR Main Landing Gear (MLG) Shock Absorbers — Cross Locking Bolt of the Attachment Pin

EASA Safety Information Bulletin 2011-02 is an informational document addressing the ATR 42 and ATR 72 aeroplanes' main landing gear (MLG) shock absorbers, specifically the cross locking bolt of the attachment pin. It highlights the risk of migration and rupture of the shock absorber attachment pin due to missing locking bolts, referencing previous maintenance manuals and service bulletins.

Mar 18, 2011
Safety Information BulletinMaintenanceSafety MgmtATR 42ATR 72

EASA SIB 2010-26R1

Potential Performance Degradation of Anti-icing Fluids — Reduced Holdover Times

EASA Safety Information Bulletin 2010-26R1 is an informational document addressing potential performance degradation of aircraft anti-icing fluids due to contamination by runway de-icing fluids. It applies to all aeroplanes operating in winter conditions and highlights that mixing thickened anti-icing fluids with small amounts of formate or acetate-based runway de-icing fluids can reduce holdover times. The bulletin does not target specific aircraft or engine models but provides guidance relevant to ground operations involving de-icing and anti-icing procedures.

Feb 23, 2011
Safety Information BulletinFlight OpsSafety Mgmt

EASA SIB CE-11-21

Hawker Beechcraft 33, 35 and 36 (Bonanza), 55, 56, 58 and 95 (Baron), and 60 (Duke) aeroplanes - Trailing Edge Flap Nose Rib P/N 35-165050-84 Cracking

The Special Airworthiness Information Bulletin SAIB: CE-11-21 is an FAA informational bulletin addressing potential cracking in the trailing edge flap nose rib part number 35-165050-84 on Hawker Beechcraft Bonanza Model Series 33, 35, and 36; Baron Model Series 55, 56, 58, and 95; and Duke Model Series 60 aircraft. This bulletin informs owners, operators, and maintenance personnel about the airworthiness concern but does not mandate any regulatory action. The cracking issue has been observed on both left-hand and right-hand flap nose ribs, with no current determination that it warrants an airworthiness directive.

Feb 22, 2011
Safety Information BulletinMaintenanceSafety MgmtHawker Beechcraft Bonanza 33Hawker Beechcraft Bonanza 35Hawker Beechcraft Bonanza 36Hawker Beechcraft Baron 55Hawker Beechcraft Baron 56Hawker Beechcraft Baron 58Hawker Beechcraft Baron 95Hawker Beechcraft Duke 60

EASA SIB SAFO11002

Hawker Beechcraft Model 60 (Duke) - Flap Pre-flight Check

SAFO 11002 is a Safety Alert for Operators issued by the U.S. Federal Aviation Administration concerning the Beechcraft Duke (BE-60) aircraft. It highlights the critical need for proper flap operation checks before takeoff to ensure flight safety. The alert is based on an accident investigation where improper flap actuator maintenance contributed to a fatal crash.

Feb 10, 2011
Safety Information BulletinFlight OpsMaintenanceSafety MgmtBeechcraft Duke 60