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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 2012-14

Improving the safety of aiders on the ground when relocating an inflated hot air balloon

EASA Safety Information Bulletin 2012-14 is an informational document addressing the safety of aiders on the ground when relocating an inflated hot air balloon. It applies to all hot air balloons and highlights risks associated with aiders holding the basket's carrying handles during relocation. The bulletin recommends using a device called a “Spider” to improve safety and coordination during ground handling.

Safety Information Bulletin

EASA SIB FA-24-2012

EMBRAER ERJ 170/175 and ERJ 190/195 Aeroplanes — Landing Gear — Brake Carbon Disks Damage

The EMBRAER ERJ 170/175 and ERJ 190/195 Aeroplanes — Landing Gear — Brake Carbon Disks Damage Flight Alert FA Nº 24/2012 is a regulatory document addressing brake carbon disk damage issues on these aircraft models. It informs operators about potential carbon disk brake failures during normal operation that can lead to runway contamination by brake debris. The alert provides updated maintenance instructions to detect and prevent brake assembly failures.

Safety Information Bulletin

Embraer ERJ 170
Embraer ERJ 175
Embraer ERJ 190
Embraer ERJ 195

EASA SIB 2012-12

WITHDRAWN - Current status can be followed on the EASA SUP website: https://www.easa.europa.eu/en/domains/aircraft-products/suspected-unapproved-parts.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. 2012-12 notifies aviation stakeholders about unapproved aircraft parts due to theft from an aircraft parked long-term since 2009. The bulletin lists specific stolen parts and equipment, including components from Honeywell, B/E Aerospace, Auxilec/Thales, and others, affecting various aircraft. The document highlights that these parts are unapproved and should not be installed on any aircraft.

Safety Information Bulletin

EASA SIB 2012-11

Tyre Specification(s) and Installation

EASA Safety Information Bulletin SIB No. 2012-11 titled "Tyre Specification(s) and Installation" addresses issues related to tyre specifications and installation on aeroplanes with retractable landing gears, including the Diamond DA 42. The bulletin highlights a safety concern where a gear-up landing occurred due to a tyre outer diameter deviation caused by using a tyre brand different from that specified by the manufacturer. It applies to all aeroplanes certified or validated by EASA under CS-23, CS-VLA, CS-22, or CS-LSA, or certified by European National authorities before 28 September 2003 under equivalent standards.

Safety Information Bulletin

Diamond DA 42

EASA SIB CE-12-33

Mitsubishi Heavy Industries MU-2B Aeroplanes — Nose Landing Gear Retraction/Extension System

The Special Airworthiness Information Bulletin SAIB CE-12-33 is an FAA informational bulletin addressing the nose landing gear retraction/extension system on Mitsubishi Heavy Industries MU-2B series aircraft. It notifies operators of clarifications made to maintenance documentation regarding the correct orientation of the nose landing gear drag strut down-lock link. This bulletin applies to all MU-2B models listed in Type Certificate Data Sheets A2PC and A10SW.

Safety Information Bulletin

Mitsubishi Heavy Industries MU-2B

EASA SIB CE-12-36

Hawker Beechcraft Corp. Aeroplanes - Improperly Installed Ailerons

The Special Airworthiness Information Bulletin SAIB: CE-12-36 is an FAA informational bulletin addressing the issue of improperly installed ailerons on Hawker Beechcraft Corporation airplanes. Affected aircraft include Bonanza models (per TCDS A-777 and 3A15), Baron models (per TCDS 3A16 and A23CE), King Air Series, and 1900 Airliner models except 1900D (per TCDS 3A20, A14CE, A24CE, and A31CE). The bulletin informs operators and maintenance personnel about the potential for improper aileron installation and provides guidance to mitigate this issue.

Safety Information Bulletin

Hawker Beechcraft Bonanza
Hawker Beechcraft Baron
Hawker Beechcraft King Air
Hawker Beechcraft 1900 Airliner

EASA SIB CE-12-34

Hawker Beechcraft Model 76 (Duchess) Aeroplanes - MLG Cracks in A-Frame Assemblies - post-AD 97-06-10

The Special Airworthiness Information Bulletin SAIB: CE-12-34 addresses cracking issues in the main landing gear "A" frame assemblies with part numbers 105-810023-75 and 105-810023-76 on Hawker Beechcraft Model 76 (Duchess) airplanes. This bulletin provides information on the continued occurrence of cracks despite previous Airworthiness Directive 97-06-10, which allowed installation of these improved assemblies. The bulletin is informational and does not mandate new regulatory action.

Safety Information Bulletin

Hawker Beechcraft Model 76

EASA SIB 2011-24R1

European Geostationary Navigation Overlay Service (EGNOS) Availability

EASA Safety Information Bulletin SIB No: 2011-24R1 titled European Geostationary Navigation Overlay Service (EGNOS) Availability addresses the operational status and performance of the EGNOS Safety of Life service for aircraft certified to conduct RNAV/GNSS approaches to LPV or LNAV/VNAV minima in European airspace. It informs that despite improvements, EGNOS does not fully meet ICAO Annex 10 requirements for continuity and availability during APV SBAS approaches. The bulletin applies broadly to all aircraft using SBAS-based navigation approaches in Europe.

Safety Information Bulletin

EASA SIB CE-12-24R1

Cessna 336/337 and (formerly Reims) F337 Aeroplanes — Frayed Flap Extend Cables

The Special Airworthiness Information Bulletin SAIB: CE-12-24R1 is an FAA advisory regarding frayed flap extend cables on Cessna Models F337, 336, and 337 airplanes, including those formerly produced by Reims. It informs owners, operators, and maintenance personnel about the potential for cable wear and recommends inspection practices to ensure continued airworthiness. This bulletin is informational and does not mandate regulatory action under 14 CFR part 39.

Safety Information Bulletin

Cessna 336
Cessna 337
Reims F337

EASA SIB CE-12-30

Eclipse EA500 Aeroplanes — Wing Main Spar-to-Fuselage Attachment Lugs

The Special Airworthiness Information Bulletin SAIB: CE-12-30 is an FAA informational bulletin addressing corrosion concerns on the wing main spar and fuselage attachment lugs of Eclipse Aerospace EA500 model series aircraft. It provides guidance for inspection and maintenance to registered owners and operators of these aircraft. The bulletin highlights corrosion issues without mandating regulatory action but encourages compliance with Eclipse Aerospace's mandatory service bulletins.

Safety Information Bulletin

Eclipse EA500

EASA SIB SW-12-12

Sikorsky (formerly Schweizer, Hughes) 269C and 269C-1 Helicopters - Engine Failure Simulation

The Special Airworthiness Information Bulletin (SAIB) SW-12-12 provides guidance for owners and operators of Sikorsky (formerly Schweizer, Hughes) 269C and 269C-1 helicopters regarding engine failure simulation. It addresses updated instructions in the approved Pilot Flight Manual to prevent engine stoppage caused by rapid throttle reductions during practice autorotations in helicopters with air-aspirated reciprocating engines.

Safety Information Bulletin

Sikorsky 269C1

EASA SIB CE-12-31

Garmin GRS 77/77H Attitude and Heading Reference System (AHRS) Units

Special Airworthiness Information Bulletin SAIB: CE-12-31 is an FAA advisory concerning the Garmin GRS 77 and GRS 77H Attitude and Heading Reference System (AHRS) units used in Garmin G500/G500H/G600 systems and integrated flight decks such as G900X, G950, G1000, G1000H, Cirrus Perspective™, and Embraer Prodigy®. It informs operators about a potential unintentional reset of these AHRS units during sustained bank turns in certain geographic regions. This bulletin does not impose mandatory requirements but provides important safety information.

Safety Information Bulletin

EASA SIB 2011-01R2

WITHDRAWN: TECHNICAL CONTENT COVERED IN CS-STAN, SUBPART B, CS-SC202

WITHDRAWN: TECHNICAL CONTENT COVERED IN CS-STAN, SUBPART B, CS-SC202 is an EASA Safety Information Bulletin (SIB No. 2011-01R2) issued on 2012-05-10. It provides information about the use of unleaded Aviation Gasoline UL 91 in aeroplanes powered by spark-ignited piston engines, referencing specific engine service instructions such as Rotax SI-912-016/SI-914-019 and Lycoming Service Instruction No. 1070R. The bulletin clarifies fuel standards and approvals related to unleaded Avgas UL 91 and its compatibility with engines approved for Avgas or Motor Gasoline (Mogas).

Safety Information Bulletin

EASA SIB 2012-07

Diehl Comfort Modules (formerly DASELL) Baby Nursing Tables - Hinge Replacement

EASA Safety Information Bulletin 2012-07 addresses the replacement of pivot-type hinges with piano-type hinges on Diehl Comfort Modules (formerly DASELL) baby nursing tables installed on Airbus A319, A320, A321, A300-600, A310, and A330 aircraft. The bulletin informs operators about reported incidents of finger injuries and infant entrapment caused by the folding mechanism of these nursing tables. It provides references to Airbus service bulletins and operator information telexes related to design improvements and safety measures.

Safety Information Bulletin

Airbus A319
Airbus A320
Airbus A321
Airbus A300-600
Airbus A310
Airbus A330

EASA SIB 2008-49R1

Rolls-Royce Deutschland BR700-710 Engines — Re-use of Potentially Damaged Engine Parts and Components

EASA Safety Information Bulletin 2008-49R1 addresses the re-use of potentially damaged parts and components from Rolls-Royce Deutschland BR700-710 engines, specifically serial numbers 12533 and 12534. These engines are installed on aircraft such as the Bombardier BD-700 Global Express and Gulfstream GV and GV-SP series, including G500 and G550 variants. The bulletin informs operators and manufacturers about the risks associated with re-using parts from these engines following an incident that subjected them to loads beyond certified limits.

Safety Information Bulletin

Bombardier BD-700
Gulfstream GVSP
Gulfstream G500
Gulfstream G550

EASA SIB 2012-08

Rockwell Collins TDR-94/TDR-94D Transponders — Erroneous Vertical Rate Information

EASA Safety Information Bulletin SIB No. 2012-08 addresses an issue with Rockwell Collins TDR-94 and TDR-94D Mode S transponders that transmit erroneous vertical rate information when interfaced with Air Data Computers using ARINC 575 inputs. This affects transponders with specific part numbers installed on various aircraft certificated under FAR, JAR, or CS Parts 23, 25, 27, or 29. The bulletin informs operators about the incorrect processing of vertical rate data which may impact Mode S Enhanced Surveillance capabilities.

Safety Information Bulletin

EASA SIB NM-12-25

Hawker Beechcraft 400/400A and Learjet 60 Aeroplanes — Rockwell Collins Altitude Awareness Panel 115VAC Power Transient Failures

The Special Airworthiness Information Bulletin SAIB: NM-12-25 is an FAA informational bulletin addressing 115VAC power transient failures in Rockwell Collins Altitude Awareness Panels installed on Hawker Beechcraft 400/400A and Learjet 60 airplanes. It informs operators about issues related to the AAP-850 and AAP-851 altitude awareness panels that may cause smoke in the cockpit due to a varistor protection device failure. The bulletin provides guidance but does not mandate corrective action.

Safety Information Bulletin

Hawker Beechcraft 400
Hawker Beechcraft 400A
Learjet 60

EASA SIB NE-12-26

General Electric GE90 Engines - Fan Blade Root and Blade Dovetail Inspections

The Special Airworthiness Information Bulletin SAIB: NE-12-26 provides updated inspection guidance for fan blade root and blade dovetail inspections on General Electric GE90-76, GE90-85, GE90-90, and GE90-94B series turbofan engines installed on Boeing 777 aircraft. This bulletin informs operators and maintenance personnel about focused inspections to detect delaminations in the fan blade dovetail area. The document clarifies that the issue does not constitute an unsafe condition requiring mandatory regulatory action.

Safety Information Bulletin

Boeing 777

EASA SIB SW-12-23

Sikorsky S-92A Helicopters — Fuselage Cabin Structure Inspection

The FAA Special Airworthiness Information Bulletin SW-12-23 provides guidance for Sikorsky Aircraft Corporation Model S-92A helicopters regarding inspection of the fuselage cabin structure. It alerts operators to follow Sikorsky Alert Service Bulletin No. 92-53-007 for recurring visual inspections of cabin structure at stations STA 328 and STA 361 to detect cracks. This bulletin is informational and does not mandate regulatory action under 14 CFR part 39.

Safety Information Bulletin

Sikorsky S-92A

EASA SIB 2012-05

WITHDRAWNÂ - REPLACED BY EASA AD 2019-0144

EASA Safety Information Bulletin 2012-05 addresses the issue of water freezing in pitot lines on Piaggio Aero Industries P.180 aeroplanes, including all serial numbers of the Avanti and Avanti II models. The bulletin highlights reported cases of airspeed indication mismatches and loss of air data computer airspeed information due to water accumulation and freezing in pitot lines. It provides information on the cause, contributing factors, and recommendations to mitigate this issue.

Safety Information Bulletin

Piaggio Aero Industries P.180