EASA Regulations & Airworthiness Directives

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

EASA SIB 2009-18R1

May 12, 2011

Inspection of Main Rotor Blade Retention Bolts

EASA Safety Information Bulletin 2009-18R1 is an advisory document addressing the inspection of main rotor blade retention bolts on MD Helicopters MD900 models fitted with part number 900R3100001-105 bolts. It provides updated guidance following previous inspections related to bolts with part number 900R3100001-103 and references MD Helicopters Service Bulletin SB900-116R1 dated 9 April 2010. The bulletin aims to enhance safety by recommending repetitive gap checks and inspections of these critical components.

Safety Information Bulletin
  • MD Helicopters MD900

EASA SIB CE-11-30

May 11, 2011

Air Tractor, Inc. (all types & models) - Airframe Structure Corrosion

The Special Airworthiness Information Bulletin SAIB: CE-11-30 is an informational document issued by the FAA addressing airframe structure corrosion in all Air Tractor, Inc. model series AT-250, AT-300, AT-400, AT-500, AT-600, and AT-800 aircraft. It highlights the susceptibility of these aircraft to severe corrosion due to their operation in harsh environments such as chemical dispersal and firebomber missions. The bulletin provides guidance on inspection and repair procedures but does not mandate regulatory action.

Safety Information Bulletin
  • Air Tractor AT-250
  • Air Tractor AT-300
  • Air Tractor AT-400
  • Air Tractor AT-500
  • Air Tractor AT-600
  • Air Tractor AT-800

EASA SIB CE-08-12R1

May 11, 2011

Cirrus Design Corporation (CDC) Models SR20 and SR22 airplanes - Possible Failure of a Transient Voltage Suppressor (TVS)

The Special Airworthiness Information Bulletin SAIB: CE-08-12R1 addresses a potential failure of a transient voltage suppressor (TVS) in Cirrus Design Corporation Models SR20 and SR22 airplanes. This failure may cause loss of NAV/COMM 1 functionality and produce short-term smoke and fumes in the cockpit, increasing pilot workload. The bulletin provides updated service information from Cirrus Design Corporation to mitigate this issue.

Safety Information Bulletin
  • Cirrus Design Corporation SR20
  • Cirrus Design Corporation SR22

EASA SIB CE-08-14

May 11, 2011

Diamond Models DA 40 and DA 40F airplanes equipped with Garmin G1000 installations per Garmin Supplemental Type Certificate (STC) SA01254WI and STC SA01389WI - Possible Failure of a Transient Voltage Suppressor (TVS)

Special Airworthiness Information Bulletin SAIB: CE-08-14 is an FAA informational bulletin addressing a potential airworthiness concern for Diamond Models DA 40 and DA 40F airplanes equipped with Garmin G1000 installations under Garmin Supplemental Type Certificates SA01254WI and SA01389WI. The bulletin highlights possible failure of transient voltage suppressors (TVS) that may cause cockpit smoke, loud popping sounds, and loss of standby attitude indicator and audio panel functionality. This bulletin does not mandate corrective action but provides important safety information for operators of these aircraft.

Safety Information Bulletin
  • Diamond DA 40
  • Diamond DA 40F

EASA SIB CE-08-13

May 11, 2011

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.

Safety Information Bulletin
  • Piper PA-28-161 Warrior III
  • Piper PA-28-181 Archer III
  • Piper PA-28R-201 Arrow
  • Piper PA-32R-301 Saratoga II TC
  • Piper PA-32R-301 HP
  • Piper PA-32-301FT 6X
  • Piper PA-32-301XTC 6XT
  • Piper PA-34-200T Seneca V
  • Piper PA-44-180 Seminole
  • Piper PA-46-350P Mirage
  • Piper PA-46-500TP Meridian

EASA SIB 2008-20

May 11, 2011

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.

Safety Information Bulletin
  • Cirrus Design Corporation
  • Piper Aircraft

EASA SIB 2011-06

May 5, 2011

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.

Safety Information Bulletin
  • Gulfstream Aerospace LP 1125 Astra Westwind
  • Gulfstream Aerospace LP Astra SPX
  • Gulfstream Aerospace LP G100

EASA SIB 2011-07

May 5, 2011

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.

Safety Information Bulletin
  • Airbus A320
  • Boeing 737
  • Dassault Falcon 2000

EASA SIB CE-11-28

Apr 11, 2011

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.

Safety Information Bulletin
  • Hawker Beechcraft 55
  • Hawker Beechcraft 56
  • Hawker Beechcraft 58
  • Hawker Beechcraft 95-55

EASA SIB NM-11-25

Apr 6, 2011

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.

Safety Information Bulletin
All aircraft

EASA SIB NE-11-27

Apr 6, 2011

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.

Safety Information Bulletin
  • Airbus A300
  • Airbus A310
  • Airbus A330
  • Boeing 747
  • Boeing 767
  • McDonnell Douglas MD-11

EASA SIB NE-08-26R3

Apr 6, 2011

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.

Safety Information Bulletin
  • Mooney M20J-201
  • Cessna 177RG

EASA SIB NE-11-22

Apr 6, 2011

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.

Safety Information Bulletin
  • Cessna Citation 750

EASA SIB NM-11-23

Apr 5, 2011

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.

Safety Information Bulletin
  • Boeing 767-400ER

EASA SIB CE-11-26

Mar 31, 2011

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.

Safety Information Bulletin
  • M7 Aerospace SA226
  • M7 Aerospace SA227

EASA SIB 2010-30R1

Mar 31, 2011

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.

Safety Information BulletinSuperseded
All aircraft

EASA SIB SW-11-24

Mar 29, 2011

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.

Safety Information Bulletin
  • Bell 206B

EASA SIB 2011-03

Mar 24, 2011

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.

Safety Information Bulletin
All aircraft

EASA SIB 2011-04

Mar 22, 2011

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.

Safety Information Bulletin
All aircraft