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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 2007-25

WITHDRAWN / CANCELLED - TRANSPORT CANADA AD CF-2007-21R1 AND FAA AD 2007-19-53 HAVE BEEN ADOPTED BY EASA

The document titled 'WITHDRAWN / CANCELLED - TRANSPORT CANADA AD CF-2007-21R1 AND FAA AD 2007-19-53 HAVE BEEN ADOPTED BY EASA' is an EASA Safety Information Notice 2007-25 issued on 2007-09-17. It addresses tail rotor blade safety issues on various Bell helicopter models including the 204B, 205 series, 206 series, 206L series, 212, 222 series, 230, 407, 412 series, 427, and 430. The notice references Transport Canada Emergency AD CF-2007-2L1 and FAA Emergency AD 2007-19-53, which require inspections and corrective actions for tail rotor blades with missing balance weight screws.

Safety Information Bulletin

Bell 204B
Bell 205
Bell 206
Bell 206L
Bell 212
Bell 222
Bell 230
Bell 407
Bell 412
Bell 427
Bell 430

EASA SIB CE-11-04

Hawker Beechcraft 65, 90 and 100 series - Improper Wing Spar Repairs

The Special Airworthiness Information Bulletin SAIB: CE-11-04 is an FAA informational bulletin addressing improper wing spar repairs on Hawker Beechcraft King Air Models 65, 90, and 100 series aircraft. It highlights issues with nonconforming repairs to the fuselage keel skin aft of the wing main spar that may have caused structural damage. The bulletin provides guidance for inspection and repair but does not mandate regulatory action.

Safety Information Bulletin

Hawker Beechcraft King Air 65
Hawker Beechcraft King Air 90
Hawker Beechcraft King Air 100

EASA SIB SAFO10014

Airworthiness Concerns for Work Accomplished by US Aircraft Instruments

The Safety Alert for Operators (SAFO) 10014 titled 'Airworthiness Concerns for Work Accomplished by US Aircraft Instruments' informs aircraft owners and operators about potential airworthiness issues related to work performed by US Aircraft Instruments between April 1998 and July 9, 2009. The alert highlights concerns arising from FAA inspections that led to the emergency revocation of the repair station certificate held by US Aircraft Instruments in Hammonton, NJ. This SAFO is relevant to any aircraft or instruments serviced by this facility during the specified timeframe.

Safety Information Bulletin

EASA SIB SAFO10018

Piper, Maule and Taylorcraft - Powder Coating of Aircraft Wing Struts

SAFO 10018 is a Safety Alert for Operators issued by the FAA addressing the powder coating of aircraft wing struts on Piper, Maule, and Taylorcraft airplanes. It highlights airworthiness concerns related to the powder coating process that involves drilling vent holes in sealed wing lift struts, which compromises their sealed condition and may affect compliance with Airworthiness Directive 99-01-05. The document warns that these modifications can degrade structural integrity and corrosion protection of the struts.

Safety Information Bulletin

Piper
Maule
Taylorcraft

EASA SIB 2010-31

WITHDRAWN: TECHNICAL CONTENT COVERED IN CS-STAN, SUBPART B, CS-SC203

EASA Safety Information Bulletin SIB No. 2010-31 informs owners and operators of aeroplanes powered by spark-ignited piston engines about the use of unleaded Hjelmco Avgas 91/96 UL and 91/98 UL fuels. These fuels meet certain military and ASTM standards and may be used in engines approved for these grades without additional aeroplane approval. The bulletin specifically references engine types such as Rotax, Lycoming, and Kalisz.

Safety Information Bulletin

EASA SIB AWB-26-004

Chubb, Quell, Flameguard, Motorcraft, and Fire Smart - Fire Extinguisher Recall

The Airworthiness Bulletin AWB 26-004 Issue 1 titled 'Chubb, Quell, Flameguard, Motorcraft, and Fire Smart - Fire Extinguisher Recall' addresses a product safety recall of certain dry powder fire extinguishers that may be installed on aircraft, particularly manned hot air balloons. The affected extinguishers were manufactured between 16 February 2010 and 8 July 2010 and bear specific serial numbers under the brands Chubb, Quell, Flameguard, Motorcraft, and Fire Smart. This recall highlights potential non-compliance with Australian/New Zealand standards for filling capacity, which could impact fire safety performance.

Airworthiness Directive

EASA SIB 2010-12R1

Loss of tail rotor effectiveness (LTE) or unanticipated yaw in helicopters

EASA Safety Information Bulletin 2010-12R1 addresses the phenomenon of Loss of Tail Rotor Effectiveness (LTE) or unanticipated yaw in helicopters. This bulletin applies to all single main rotor helicopters equipped with a tail anti-torque device and explains that LTE is a critical low-speed aerodynamic condition causing uncommanded yaw, which varies depending on the main rotor rotation direction. The document references several authoritative sources for understanding, preventing, and recovering from LTE.

Safety Information Bulletin

EASA SIB SW-09-44

WITHDRAWN — REPLACED BY EASA AD 2010-0219

WITHDRAWN — REPLACED BY EASA AD 2010-0219 is a Special Airworthiness Information Bulletin issued by the FAA regarding the potential in-flight separation of cabin doors on Schweizer Models 269 series helicopters, including 269A, TH-55A, 269A-1, 269B, 269C, 269C-1, and 269D with specified serial numbers. The bulletin addresses a design issue with the door hinge pins that could lead to door detachment during flight. It informs operators about the concern and provides recommendations to mitigate the risk.

Safety Information Bulletin

Schweizer 269
Schweizer 269A1
Schweizer TH-55A
Schweizer 269B
Schweizer 269C1
Schweizer 269D

EASA SIB 2010-09R1

Piper PA-31 - Wing Leading Edge Stall Strip Configuration

EASA Safety Information Bulletin 2010-09R1 is an advisory document addressing the wing leading edge stall strip configuration for Piper PA-31 series aircraft, including PA-31, PA-31-300, PA-31-325, and PA-31-350 models. It highlights the importance of correct stall strip installation to maintain conformity with the aircraft's Type Design and improve low-speed handling characteristics. The bulletin supports CASA Australia's Airworthiness Bulletin 57-009 Issue 2 and provides guidance for European operators and maintainers.

Safety Information Bulletin

Piper PA-31300325350

EASA SIB 2010-23

Use of Portable Devices in Aircraft by the Flight Crew

EASA Safety Information Bulletin SIB No. 2010-23 addresses the use of portable devices by flight crew on aircraft. It highlights that portable devices, including those depicting aircraft position or flight information, are not subject to EASA airworthiness approval and cannot replace certified aircraft systems. The bulletin applies broadly to all aircraft types and emphasizes that such devices do not comply with EU-OPS 1.630(d) or JAR-OPS 3.630(d) regulations.

Safety Information Bulletin

EASA SIB CE-11-01

Piper PA-28, PA-32, PA-34 and PA-44 series - Horizontal Stabilator Turnbuckle

The Special Airworthiness Information Bulletin SAIB: CE-11-01 is an FAA informational bulletin addressing a potential airworthiness concern involving the horizontal stabilator turnbuckle and control cable assembly on Piper PA-28, PA-32, PA-34, and PA-44 series airplanes. The issue involves stress corrosion cracking that could lead to failure of the turnbuckle/control cable assembly and loss of pitch control. This bulletin applies to all serial numbers of the specified Piper models.

Safety Information Bulletin

Piper PA-28
Piper PA-32
Piper PA-34
Piper PA-44

EASA SIB 2010-03

Carburetor Icing Prevention

EASA Safety Information Bulletin SIB No: 2010-03 is an advisory document addressing carburetor icing prevention for all piston engines with carburetors installed on any aircraft, including fixed-wing aeroplanes and piston-engine rotorcraft such as helicopters. It supports and extends the FAA Special Airworthiness Information Bulletin CE-09-35 recommendations to European operators and emphasizes the particular risks and operational considerations for rotorcraft like the Robinson R22 equipped with Lycoming O-320 engines. The bulletin provides detailed guidance on recognizing, preventing, and responding to carburetor icing conditions.

Safety Information Bulletin

EASA SIB 2010-29

Thales Angle of Attack (AoA) Sensors

EASA Safety Information Bulletin SIB No. 2010-29 addresses issues with Thales Angle of Attack (AoA) sensors installed on ATR 42 and ATR 72 aircraft. The bulletin highlights that certain AoA sensors, identified by specific part and serial numbers, were repaired using improperly calibrated test equipment, potentially affecting their accuracy. It references Thales Avionics service bulletins that provide instructions for testing and adjustment of the affected units.

Safety Information Bulletin

ATR 42
ATR 72

EASA SIB NE-09-48R1

Propellers and component parts, repaired, inspected, or overhauled by Western Aircraft Propeller Service, Inc. (WAP)

Special Airworthiness Information Bulletin SAIB NE-09-48R1 is a revised FAA information bulletin concerning propellers and component parts repaired, inspected, or overhauled by Western Aircraft Propeller Service, Inc. (WAP). It addresses the airworthiness status of McCauley 200/300/400 series threadless compact propellers and related non-destructive inspection and testing services. This bulletin does not apply to any specific aircraft or engine models beyond those propeller series mentioned.

Safety Information Bulletin

EASA SIB 2010-15R1

Improper Maintenance of Safety Belts / Torso Restraint Systems

EASA Safety Information Bulletin 2010-15R1 addresses the improper maintenance of safety belts and torso restraint systems installed on aircraft. It highlights that some Part 145 maintenance organisations in Europe, including Germany, Austria, and the Netherlands, have performed maintenance without using applicable current maintenance data, rendering affected safety belts and restraint systems potentially non-airworthy. The bulletin applies to all safety belts and torso restraint systems maintained after 28 November 2003 without proper data and lists specific design approval holders forbidding webbing replacement in their Component Maintenance Manuals.

Safety Information Bulletin

EASA SIB 2010-28

Possible effects of Thickened Anti-icing Fluids on Take off Rotation for Airplanes with Unpowered Elevator Controls

EASA Safety Information Bulletin 2010-28 is a safety advisory addressing the possible effects of thickened Type II or IV anti-icing fluids on the takeoff rotation of airplanes with unpowered elevator controls, such as the BAE Systems ATP. It highlights incidents of rejected takeoffs due to increased elevator control forces required after anti-icing fluid application. The bulletin supports FAA Safety Alert for Operators SAFO 10001 and aims to inform European operators about these safety concerns during winter operations.

Safety Information Bulletin

BAE Systems ATP

EASA SIB 2010-27

Airbus A318/A319/A320/A321 — Evacuation Systems - Coupling Pin Verification

EASA Safety Information Bulletin 2010-27 is an informational document addressing evacuation system issues on Airbus A318, A319, A320, and A321 aircraft. It highlights incidents where evacuation slides failed to deploy due to missing coupling pins in the reservoir and valve assemblies. The bulletin provides guidance to operators and maintenance organizations to verify and correct the installation of coupling pins in affected slide reservoirs.

Safety Information Bulletin

Airbus A318
Airbus A319
Airbus A320
Airbus A321

EASA SIB CE-10-48

Cessna 402C — Incorrect Assembly of MLG Torque Link Centre Pivot Attachment

The FAA Special Airworthiness Information Bulletin SAIB: CE-10-48 addresses the incorrect assembly of the main landing gear (MLG) torque link center pivot attachment on Cessna Model 402C airplanes. It informs operators and maintenance personnel about new caution statements to be added to the Cessna 402C Maintenance Manual regarding the proper handling and installation of washer part number 5045018-2. This bulletin is informational and does not mandate regulatory action.

Safety Information Bulletin

Cessna 402C

EASA SIB SAFO10016

Cessna (including Reims Aviation) - Missing or Improper Seat Stops

The Safety Alert for Operators (SAFO) 10016 titled "Cessna (including Reims Aviation) - Missing or Improper Seat Stops" addresses the requirement for type design seat stops on seat rails in various Cessna aircraft models. Affected aircraft include Cessna models 150, 152, 172, 206, 303, 336, 337, and legacy single-engine models such as 170, 175, 177, 180, 182, 185, 188, 190, 195, 205, 207, and 210. The document highlights the importance of proper seat stop installation to maintain airworthiness and safety during critical flight phases.

Safety Information Bulletin

Cessna 150
Cessna 152
Cessna 172
Cessna 206
Cessna 303
Cessna 336
Cessna 337
Cessna 170
Cessna 175
Cessna 177
Cessna 180
Cessna 182
Cessna 185
Cessna 188
Cessna 190
Cessna 195
Cessna 205
Cessna 207
Cessna 210

EASA SIB NM-10-45

Cessna 680 and 750 - Nose Landing Gear Extension Mechanism

Special Airworthiness Information Bulletin SAIB: NM-10-45 is an FAA informational bulletin addressing an airworthiness concern for Cessna Aircraft Company Model 680 and 750 airplanes related to the nose landing gear extension mechanism. The bulletin highlights a potential issue with the nose landing gear door linkages that may cause improper extension of the nose gear without cockpit indication until gear deployment is attempted. This bulletin provides guidance to operators and maintenance personnel to ensure proper inspection and maintenance procedures are followed.

Safety Information Bulletin

Cessna 680
Cessna 750