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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 CE-16-04

M7 Aerospace (formerly Fairchild, Swearingen) SA226 and SA227 Aeroplanes — Engine Power Lever

The Special Airworthiness Information Bulletin SAIB: CE-16-04 informs owners and operators of M7 Aerospace LLC Models SA226 and SA227 series airplanes about an airworthiness concern related to the engine power lever control cable support bracket in the cockpit pedestal. The bulletin provides inspection procedures and maintenance actions for the affected part number 26-21505. This information bulletin is advisory and does not mandate regulatory action under FAA regulations.

Safety Information Bulletin

EASA SIB NM-15-23

Beechcraft (formerly Hawker) 4000 Aeroplanes — Aerodynamic Fairing Interference with Nose Landing Gear Doors

The Beechcraft (formerly Hawker) 4000 Aeroplanes — Aerodynamic Fairing Interference with Nose Landing Gear Doors is a Special Airworthiness Information Bulletin issued by the FAA to inform owners, operators, and maintenance technicians about a potential interference issue between the radome and the nose landing gear doors on Beechcraft Model 4000 airplanes. This interference can prevent the nose landing gear from extending properly. The bulletin does not mandate corrective action but provides important safety information.

Safety Information Bulletin

EASA SIB CE-16-03

Cessna (incl. formerly Reims Aviation) 150/152 Aeroplanes — Aft Fin Attachment Fitting

The Special Airworthiness Information Bulletin SAIB: CE-16-03 is an FAA informational bulletin addressing concerns about cracked aft fin attachment fittings on Cessna (including formerly Reims Aviation) 150/152 aeroplanes produced from 1966 to 1986. It specifically references part numbers 0431009-1, -2, and -3 affecting various Cessna 150 and 152 model series. The bulletin provides updated inspection guidance but does not mandate regulatory action.

Safety Information Bulletin

EASA SIB 2015-02R2

CANCELLED. Current information on conflict zones at: https://www.easa.europa.eu/en/domains/air-operations/czibs

EASA Safety Information Bulletin 2015-02R2 is an informational document addressing the status of Pakistan airspace. It references guidance from the French DGAC and the UK Civil Aviation Authority regarding operations in this airspace. The bulletin does not specify affected aircraft or engines but is relevant to all operators and national aviation authorities overseeing flights in or near Pakistan airspace.

Safety Information Bulletin

EASA SIB 2015-17R1

Unreliable Airspeed Indication at High Altitude/ Manual Handling at High Altitude

EASA Safety Information Bulletin 2015-17R01 is an operations bulletin addressing unreliable airspeed indication and manual handling challenges at high altitude for aeroplanes with maximum cruising altitudes above FL300. It highlights risks associated with pitot blockage due to high altitude icing and the resulting autopilot and autothrottle disconnections, particularly affecting fly-by-wire aircraft. The bulletin emphasizes pilot awareness and training to maintain safe flight control under these conditions.

Safety Information Bulletin

EASA SIB 2015-21

Notification of Unapproved Parts

EASA Safety Information Bulletin 2015-21 is a notification regarding unapproved spare parts related to Iacobucci HF Aerospace Spa (IHFA) trolleys, specifically part numbers MK667-44, MK667-4401, MK667-4402, MK708-4401, MK708-4402, MK708-4403, MK708-4404, and MK708-4405. These trolleys are installed on aircraft including Airbus A380 and Boeing 777. The bulletin informs about parts manufactured and sold by Iacobucci Equipment and Service (IES) Srl, which is not approved under EU regulations and is not affiliated with the original manufacturer IHFA.

Safety Information Bulletin

EASA SIB 2015-18

Potential Adverse Effect of Anti-Icing Fluids during Take-off

EASA Safety Information Bulletin 2015-18 is an informational bulletin addressing the potential adverse effects of thickened anti-icing fluids (type II and IV) on airplane control during take-off. It primarily concerns aircraft with unpowered elevator controls and low to medium take-off rotation speeds, highlighting increased control forces and delayed rotation caused by fluid contamination on the horizontal stabiliser and elevator surfaces. The bulletin shares research findings from wind tunnel tests and provides guidance to operators and pilots on assessing and mitigating these effects.

Safety Information Bulletin

EASA SIB 2015-20

WITHDRAWN - RECOMMENDATIONS NOT NEEDED ANYMORE

EASA Safety Information Bulletin No. 2015-20 is an informational document addressing the potential disruption of Instrument Landing System (ILS) signals caused by aircraft positioned within ILS critical areas at runway-holding positions. It highlights a specific incident where the Glide Path signal was disrupted during an ILS Category I approach, leading to a missed approach. The bulletin applies to National Aviation Authorities, aerodrome operators, and Air Navigation Services providers and does not target specific aircraft or engine models.

Safety Information Bulletin

EASA SIB 2015-19

WITHDRAWN - REPLACED BY EASA SIB 2025-03

EASA Safety Information Bulletin No. 2015-19 is an informational bulletin addressing the transport of lithium batteries as cargo by air. It applies to all operators transporting lithium-ion and lithium-metal batteries on passenger and freighter aircraft, highlighting safety concerns related to fire risks and cargo compartment fire protection limitations. The bulletin references guidance from Airbus and Boeing and international regulatory bodies but does not mandate new regulations.

Safety Information BulletinSuperseded

EASA SIB CE-15-22

Beechcraft 33, 35, 36, 55 and 58 Aeroplanes - Wing Leading Edge Hinge-Pin Corrosion

The Special Airworthiness Information Bulletin SAIB: CE-15-22 is an FAA informational bulletin addressing potential corrosion on the wing leading edge hinge-pin of Beechcraft 33, 35, 36, 55, and 58 series airplanes, including Debonair, Bonanza, and Baron models. The corrosion is linked to deicing fluid accumulation and affects specific models such as the 35-33, G36, B55, and others. This bulletin does not mandate regulatory action but raises awareness of the issue.

Safety Information Bulletin

Beechcraft 33
Beechcraft 35
Beechcraft 36
Beechcraft 55
Beechcraft 58

EASA SIB CE-14-11R1

Cessna 310, 335, 340, 401, 402, 404, 414, 411, 414, 421, 425 and 441 series Aeroplanes — Nose Landing Gear Trunnions

The FAA Special Airworthiness Information Bulletin SAIB: CE-14-11R1 addresses an airworthiness concern for Cessna 300 and 400 series airplanes, specifically models 310, 335, 340, 401, 402, 404, 411, 414, 421, 425, and 441. It alerts owners, operators, and maintenance personnel to inspect the nose landing gear trunnions for cracks to prevent potential failure during landing, which could cause significant damage and occupant injury. This bulletin is informational and does not mandate regulatory action.

Safety Information Bulletin

Cessna 310
Cessna 335
Cessna 340
Cessna 401
Cessna 402
Cessna 404
Cessna 411
Cessna 414
Cessna 421
Cessna 425
Cessna 441

EASA SIB 2006-01R1

WITHDRAWN - REPLACED BY EASA AD 2024-0111

EASA Safety Information Bulletin 2006-01R1 is an airworthiness bulletin addressing non-conformance in maintenance of Lycoming and Continental Motors reciprocating engines overhauled or repaired by B.C. Aero Engines Ltd. between February 2002 and July 2004. It informs stakeholders about the intent to adopt Transport Canada AD CF-2005-40, which concerns maintenance errors rather than type design issues. This bulletin applies to engines potentially affected by inadequate maintenance practices performed in Canada.

Safety Information Bulletin

EASA SIB 2015-15

Large Transport Aeroplanes — Fan Cowl Door Loss Prevention

EASA Safety Information Bulletin No. 2015-15 is a safety information bulletin addressing fan cowl door loss prevention on large transport aeroplanes powered by turbojet or turbofan engines. It highlights incidents primarily involving Airbus A320 family aircraft with CFM56 or V2500 engines, as well as similar events on Boeing, Bombardier, Embraer, and Sukhoi aeroplanes. The bulletin focuses on the risk of fan cowl doors becoming unsecured and lost during take-off due to improper latching or unlocking.

Safety Information Bulletin

Airbus A320
Boeing
Bombardier
Embraer
Sukhoi

EASA SIB SAFO15008

IAE V2500 Engines — Fan Blades Overhauled outside Blade Repair Limits

SAFO 15008 is a Safety Alert for Operators issued by the FAA concerning IAE V2500 engines. It addresses the issue of fan blades that were overhauled and issued FAA Form 8130-3 release certificates but may not meet the required VRS1003 blade repair limits for sidewall thickness. The alert specifically identifies affected V2500 fan blade part numbers and serial numbers.

Safety Information Bulletin

EASA SIB NE-15-21

Pratt & Whitney Canada PT6 Engines — Wencor Engineering Fuel Nozzle Sheath (PMA part)

The FAA Special Airworthiness Information Bulletin SAIB: NE-15-21 addresses a design issue with the Wencor Engineering fuel nozzle sheath, part number 3119920-01WE, used on Pratt & Whitney Canada PT6 engine models. The bulletin informs operators, repair stations, and maintenance personnel that this PMA fuel nozzle sheath may interfere with proper installation and engine performance. Affected PT6 engine models include various PT6A series such as PT6A-38, PT6A-41, PT6A-42, and others listed under TCDS E4EA and E26NE.

Safety Information Bulletin

EASA SIB SW-15-20

Helicopters modified by Air Comm Corp. STC - Air Conditioning System Wiring

The FAA Special Airworthiness Information Bulletin SAIB: SW-15-20 provides information regarding potential overheating and melting of connectors in the air conditioning wiring of helicopters modified by Air Comm Corporation Supplemental Type Certificates (STCs). Affected helicopter models include Bell Helicopter 206, Bell 407, Bell 427, Agusta A119, Airbus AS350, Airbus EC120, and Airbus EC130. This bulletin alerts operators to possible wiring issues related to Molex connectors installed per Air Comm STCs.

Safety Information Bulletin

Bell 206
Bell 407
Bell 427
Agusta A119
Airbus AS350
Airbus EC120
Airbus EC130

EASA SIB 2014-07R1

Unexpected Autopilot Behaviour on Instrument Landing System (ILS) Approach

EASA Safety Information Bulletin 2014-07R1 addresses unexpected autopilot behavior during Instrument Landing System (ILS) approaches, specifically when intercepting the glide slope (G/S) signal from above. The bulletin highlights incidents involving Boeing 737-800 and Airbus A340 aircraft where false glide slope signals caused sudden pitch-up maneuvers, risking stall conditions. It raises awareness among operators, Air Navigation Service Providers (ANSPs), and training organizations about this safety concern.

Safety Information Bulletin

Boeing 737-800
Airbus A340

EASA SIB 2015-13

Safety Management of Flight Operations in Adverse Convective Weather and the Inter-Tropical Convergence Zone

EASA Safety Information Bulletin No. 2015-13 provides guidance on the safety management of flight operations in adverse convective weather and the Inter-Tropical Convergence Zone (ITCZ). It addresses the risks of loss of control in flight (LOC-I) associated with thunderstorms, turbulence, icing, and other hazards typical in the ITCZ, emphasizing the need for comprehensive risk mitigation strategies. The bulletin is applicable to National Aviation Authorities and Commercial Air Transport operators conducting multi-pilot operations.

Safety Information Bulletin

EASA SIB 2015-14

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. 2015-14 is a notification regarding suspected unapproved aircraft parts linked to the company Aviation Support Europe, based in Belgium. The bulletin applies to aircraft components and alerts aviation professionals about a judicial investigation involving this company. No specific aircraft types or engine models are mentioned in this document.

Safety Information Bulletin

EASA SIB CE-15-18

Piper PA-46 Aeroplanes — Wing Main Spar Lower Cap Cracks

The Special Airworthiness Information Bulletin SAIB: CE-15-18 is an FAA informational bulletin addressing fatigue cracking in the wing main spar lower cap near wing station 79 on Piper Aircraft Models PA-46-310P, PA-46-350P, PA-46R-350T, and PA-46-500TP airplanes. It highlights the discovery of a fatigue crack during routine inspection and provides guidance on recommended inspections and repairs. This bulletin is advisory and does not mandate regulatory action under 14 CFR part 39.

Safety Information Bulletin

Piper PA-46-310P
Piper PA-46-350P
Piper PA-46R-350T
Piper PA-46-500TP