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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 2008-59R1

Turboshaft-engine Powered Rotorcraft - Engine In-Flight Shutdown due to Ice and Snow Ingestion

EASA Safety Information Bulletin 2008-59R1 is an advisory document addressing the risk of engine in-flight shutdown in turboshaft-engine powered rotorcraft caused by ice and snow ingestion. It applies to all turboshaft-engine powered rotorcraft and aligns with FAA Special Airworthiness Information Bulletin SW-08-03R4. The bulletin highlights the dangers of ice and snow accumulation in engine inlets during ground and flight operations, particularly in helicopters not approved for flight into known icing conditions.

Safety Information Bulletin

EASA SIB 2014-04

WITHDRAWNÂ - RECOMMENDATIONS NOT NEEDED ANYMORE

EASA Safety Information Bulletin SIB No. 2014-04 provides updated recommendations regarding Required Navigation Performance Approach Procedures with Barometric Vertical Navigation (RNP-APCH with APV/Baro-VNAV). It addresses operational approval criteria for aircraft operating these procedures, referencing EASA AMC 20-27, FAA AC 20-129, and FAA AC 20-138C. The bulletin is relevant for aeroplanes registered in EASA Member States conducting APV/Baro-VNAV approaches, particularly at airports with elevations above 5,000 feet mean sea level.

Safety Information Bulletin

EASA SIB 2014-03

Land and Hold Short Operations at U.S. Airports

EASA Safety Information Bulletin SIB No: 2014-03 provides guidance on Land and Hold Short Operations (LAHSO) at U.S. airports for commercial air transport operators from EASA Member States. It clarifies the distinction between "active" and "passive" participation in LAHSO, referencing relevant FAA orders and operational specifications. The bulletin applies to fixed-wing aeroplanes operating commercially in the U.S. and highlights that neither EU-OPS nor EASA-OPS currently contain specific provisions regarding LAHSO.

Safety Information Bulletin

EASA SIB NM-14-08

Cessna 500, 501, 550, S550, 551, 552 and 560 - Aerodynamic Fuselage Fairings

The Special Airworthiness Information Bulletin SAIB: NM-14-08 is an FAA advisory concerning certain Cessna Aircraft Company models 500, 501, 550, S550, 551, 552, and 560 airplanes modified by Sierra Industries, Ltd. It addresses an airworthiness concern related to radome latch covers that may allow moisture ingress. The bulletin provides information but does not mandate regulatory action.

Safety Information Bulletin

Cessna 500
Cessna 501
Cessna 550
Cessna S550
Cessna 551
Cessna 552
Cessna 560

EASA SIB CASA-2014-01

Galley or Lavatory Water Heater Overheat - FAA Supplemental Type Certificate SA696GL and SA4370SW

The document titled 'Galley or Lavatory Water Heater Overheat - FAA Supplemental Type Certificate SA696GL and SA4370SW' is a Transport Canada Civil Aviation Safety Alert issued on 2014-01-28. It addresses a safety concern involving galley and lavatory water heaters installed under FAA STCs SA696GL and SA4370SW, commonly found on aircraft such as Canadair Challenger, Gulfstream GII, GIII, GIV, and Hawker 700/800. The alert highlights incidents of water heater thermostat failures causing overheating, smoke, and heat damage.

Safety Information Bulletin

Bombardier Canadair Challenger
Gulfstream GII
Gulfstream GIII
Gulfstream GIV
Hawker 700
Hawker 800

EASA SIB NM-14-05

Beechcraft (formerly Hawker Beechcraft, Raytheon, British Aerospace) BAe.125 and Hawker Series — Wing/Aileron Oscillations

The Special Airworthiness Information Bulletin SAIB: NM-14-05 is an FAA informational bulletin addressing wing and aileron oscillations in Beechcraft BAe.125 Series 800A, 800B, 1000A, and 1000B airplanes, as well as Hawker 750, 800, 800XP, 850XP, 900XP, and 1000 models. It highlights an airworthiness concern related to wing/aileron oscillations at high altitudes and speeds, excluding airplanes modified by Aviation Partners Inc. Supplemental Type Certificate ST01411SE.

Safety Information Bulletin

Beechcraft BAe.125 Series 800A
Beechcraft BAe.125 Series 800B
Beechcraft BAe.125 Series 1000A
Beechcraft BAe.125 Series 1000B
Beechcraft Hawker 750
Beechcraft Hawker 800
Beechcraft Hawker 800XP
Beechcraft Hawker 850XP
Beechcraft Hawker 900XP
Beechcraft Hawker 1000

EASA SIB CE-14-07

[Correction] Piper PA-31 Series — Main Wing Spar Lower Cap Cracks

The FAA Special Airworthiness Information Bulletin SAIB: CE-14-07 addresses cracking found in the main wing spar lower cap of Piper Aircraft Models PA-31, PA-31-300, PA-31-325, and PA-31-350. It provides inspection guidance for the wing main spar lower cap at the centerline spar splice plate to detect fatigue and stress corrosion cracks. This bulletin is informational and does not mandate regulatory action.

Safety Information Bulletin

Piper PA-31300325350

EASA SIB 2014-02

WITHDRAWN _ SEE FAA SAIB NM-14-21

EASA Safety Information Bulletin SIB No. 2014-02 addresses frequency interference caused by spurious transmissions from Honeywell RTA-44D Very High Frequency (VHF) transceivers. The affected transceivers, identified by part numbers 064-50000-0202 and 064-50000-0505 without MOD 22 incorporated, are installed on Airbus A318, A319, A320, and A321 aircraft. This bulletin informs operators about the issue and provides recommendations to mitigate the interference.

Safety Information Bulletin

Airbus A318
Airbus A319
Airbus A320
Airbus A321

EASA SIB 2014-01

Cessna — Supplemental (Structural) Inspection Programmes

EASA Safety Information Bulletin SIB No. 2014-01 provides guidance on the incorporation of Cessna Supplemental Inspection Documents (SIDs) into the approved Aircraft Maintenance Programme (AMP) for Cessna 100 and 200 Series aeroplanes manufactured until 1986. The bulletin addresses structural inspections aimed at detecting fatigue cracking and corrosion, focusing on critical components such as the wing lower spar cap, foam-filled elevator and trim tab, and rudder pedal torque tube. It clarifies that these inspections are recommendations and not currently mandated by an Airworthiness Directive.

Safety Information Bulletin

Cessna 100 Series
Cessna 200 Series

EASA SIB 2013-23

WITHDRAWN - REPLACED BY EASA AD 2021-0195

EASA Safety Information Bulletin 2013-23 is an informational document addressing uncommanded engine power loss, rotor speed fluctuations, or in-flight shutdown caused by Electronic Engine Control Unit (EECU) failure in Turboméca ARRRIEL 2D engines. These engines are installed on helicopters such as the Eurocopter AS 350 B3 and EC 130 T2. The bulletin describes the failure mode involving a tantalum capacitor short-circuit leading to fuel flow regulation loss and provides safety information for operators.

Safety Information Bulletin

Eurocopter AS 350 B3
Eurocopter EC 130 T2

EASA SIB 2013-22

WITHDRAWN - Suspected Unapproved Parts Notification — 10 Person Life Raft part number (P/N) 6491010414, serial numbers (S/N) 0251 and 0254, and P/N 64910-10214, S/N 0249.

EASA Safety Information Bulletin SIB No. 2013-22 is a notification regarding suspected unapproved 10 Person Life Rafts with part numbers 64910-10414 (serial numbers 0251 and 0254) and 64910-10214 (serial number 0249). These life rafts were released with counterfeit FAA Form 8130-3 certificates under the name Zodiac Services Europe, a European Part 145 approved maintenance organization. The document clarifies that these parts are unapproved and not eligible for installation on aircraft.

Safety Information Bulletin

EASA SIB 2013-21

WITHDRAWN - SEE Annex to EASA ED Decision 2014/029/R

The EASA Safety Information Bulletin 2013-21 titled 'WITHDRAWN - SEE Annex to EASA ED Decision 2014/029/R' provides guidance on the use of Portable Electronic Devices (PEDs) during commercial air transport operations. It addresses the regulatory framework under Regulation (EU) No. 965/2012, focusing on the safe use of non-transmitting and transmitting PEDs on board aircraft. The bulletin is applicable to commercial air transport operators and National Aviation Authorities overseeing these operations.

Safety Information Bulletin

EASA SIB 2011-27R1

Suspect (Bogus - Counterfeit) Electronic Components

EASA Safety Information Bulletin SIB No. 2011-27R1 addresses the issue of suspect, bogus, or counterfeit electronic components, particularly integrated circuits (ICs) and other electronic parts used by manufacturing and maintenance organizations. The bulletin highlights cases involving counterfeit Xilinx FPGA XC4006E-4PC84I and Vishay MOSFET SI4850EY-T1-E3 components, which can lead to equipment failures and reduced reliability. This document provides information relevant to aviation professionals involved in component procurement and maintenance.

Safety Information Bulletin

EASA SIB 2013-20

WITHDRAWN - RECOMMENDATIONS NOT NEEDED ANYMORE

EASA Safety Information Bulletin No. 2013-20 is an informational document addressing bounced landing recognition and recovery training for aeroplane manufacturers, operators, training organisations, and flight crews. It references an incident involving an ATR72-202 and highlights the importance of proper training to manage bounced landings, which can lead to runway excursions and aircraft damage. The bulletin provides guidance on training content and recovery techniques but does not mandate any regulatory requirements.

Safety Information Bulletin

ATR 72-202

EASA SIB 2013-19

Non-stabilized Approach followed by Runway Overrun at Lyon —Saint ExupÃ©ry— Airport

EASA Safety Information Bulletin SIB No. 2013-19 addresses a runway overrun incident involving an Airbus A321 equipped with CFM56 engines at Lyon Saint Exupéry Airport. The incident was caused by a non-stabilized instrument landing system (ILS) approach during night and rainy conditions, combined with an auto thrust system misbehavior leading to an unexpected thrust increase. The bulletin applies to Airbus A319, A320, and A321 aircraft with CFM56 or IAE V2500 engines.

Safety Information Bulletin

Airbus A319
Airbus A320
Airbus A321

EASA SIB CASA-2013-06

Bombardier CL-600-2B19 Aeroplanes - Potential Jam of the Manual Landing Gear Release Cable

Transport Canada Civil Aviation Safety Alert CASA 2013-06 addresses a potential jamming issue of the manual landing gear release cable on Bombardier CL-600-2B19 aeroplanes. The alert highlights a condition where the manual gear release system can become inoperative due to a cable dislodging and jamming under the flight deck floor area. This issue arises from a mis-rigged manual gear release system caused by distortion of a cable turnbuckle near the forward avionic bay floor panel.

Safety Information Bulletin

Bombardier CL-600-2B19

EASA SIB CASA-2013-07

Pratt & Whitney Canada PT6A Engines — Importance of Compressor and Turbine Washes

The Transport Canada Civil Aviation Safety Alert CASA 2013-07 is a safety advisory focused on Pratt & Whitney Canada PT6A engines. It emphasizes the critical importance of performing compressor and turbine washes to prevent corrosion and sulphidation, which can degrade engine performance and lead to component failure. The alert targets owners, operators, and maintenance specialists of PT6A engines.

Safety Information Bulletin

EASA SIB 2012-06R2

Defective Standard Hardware — MS21042, NAS1291 and LN9338 Self-Locking Nuts, and NAS626 Bolts

EASA Safety Information Bulletin 2012-06R2 addresses defective standard hardware, specifically MS21042, NAS1291, and LN9338 self-locking nuts, as well as NAS626 bolts. These defective parts have been installed on various rotorcraft, aeroplanes, appliances, and engines, including Gulfstream 200, GALAXY (Israel Aircraft Industries), and AgustaWestland A109 helicopters. The bulletin provides information on reported occurrences of cracked nuts and broken bolts and highlights ongoing investigations by EASA and other aviation authorities.

Safety Information Bulletin

Gulfstream 200
Israel Aircraft Industries GALAXY
AgustaWestland A109

EASA SIB 2013-18

Laundering of Scrapped Jet Engine Parts

EASA Safety Information Bulletin SIB No: 2013-18 addresses the laundering of scrapped jet engine parts, specifically engine blades and vanes identified in FAA SAFO 11005. The bulletin warns that parts reintroduced into service by Shelby Enterprises and associated brokers may have been improperly processed and could pose safety risks. This information is relevant to aircraft registered in EASA Member States but does not mandate Airworthiness Directive action.

Safety Information Bulletin

EASA SIB 2013-17

Cessna U206F Aeroplanes — Elevator Trim Tab Actuator Corrosion

EASA Safety Information Bulletin SIB No: 2013-17 addresses corrosion concerns in the elevator trim tab actuator of Cessna U206F aeroplanes. The bulletin references Transport Canada Civil Aviation Safety Alert CASA 2011-06 and Cessna Single-Engine Service Letter SE73-25, highlighting a safety issue involving the failure of the threaded rod end of the elevator trim tab actuator leading to elevator jamming and tailplane damage. This information bulletin is intended to inform owners, operators, and maintainers of affected aircraft registered in EASA Member States.

Safety Information Bulletin

Cessna U206F