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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 NM-13-34

O2 Corporation Low Pressure Flexible Oxygen Hoses

The FAA Special Airworthiness Information Bulletin SAIB: NM-13-34 addresses an airworthiness concern involving low pressure flexible oxygen hoses manufactured by O2 Corporation, used in various aircraft oxygen systems. The bulletin highlights issues with hoses becoming brittle and failing, potentially compromising oxygen delivery to masks. It applies to hoses with base part numbers O2C20T1, O2C20T3, O2C20T5, O2C20T13, O2C20T14, O2C20T15, and O2C20T16, regardless of manufacture date.

Safety Information Bulletin

EASA SIB 2013-06

Evacuation of Infants

EASA Safety Information Bulletin SIB No: 2013-06 titled 'Evacuation of Infants' provides guidance on the recommended methods for evacuating infants and small children from aircraft equipped with inflatable slides and hatch-type over wing exits. It references FAA studies and advisory circulars on emergency evacuations involving infants, focusing on techniques to minimize delays and ensure safety during evacuation. The bulletin applies broadly to all aircraft with such evacuation equipment and aims to raise awareness among crew, operators, and national aviation authorities.

Safety Information Bulletin

EASA SIB CE-13-07R1

Cessna T206H Aeroplanes — Engine Exhaust Tailpipe V-band Couplings

The FAA Special Airworthiness Information Bulletin SAIB: CE-13-07R1 addresses the risk of in-flight fire caused by failure of the engine exhaust tailpipe V-band couplings on Cessna T206H airplanes. It highlights issues with the V-band clamps securing the tailpipe to the turbocharger or wastegate components and provides guidance on inspection and replacement procedures for these parts. The bulletin specifically references Cessna part number S1921-1 and approved replacement parts for Model T206H aircraft from 1998 and later.

Safety Information Bulletin

Textron Aviation 206H (Stationair)
Cessna T206H

EASA SIB NE-13-32

Hartzell Propeller Spinner Assemblies P/N 835-54(P) and P/N 835-58(P) — Potential for Cracking of the Spinner Dome

The FAA Special Airworthiness Information Bulletin SAIB: NE-13-32 informs owners, operators, and repair facilities of Piper PA-24, Piper PA-28R-180, Piper PA-28R-200, and Mooney M20 airplanes (except Mooney M20(J)) equipped with Hartzell Propeller spinner assemblies P/N 835-54(P) and P/N 835-58(P) about the potential for cracking in the spinner dome. This cracking could lead to spinner failure and separation during flight. The bulletin provides safety information but does not mandate regulatory action under 14 CFR part 39.

Safety Information Bulletin

Piper PA-24
Piper PA-28R-180
Piper PA-28R-200
Mooney M20

EASA SIB NE-13-31

Pratt & Whitney PW4000 Engines — Scavenge Oil Tube Coking and Proper Cleaning at Overhaul

The Special Airworthiness Information Bulletin (SAIB) NE-13-31 issued by the FAA on May 9, 2013, addresses potential scavenge oil tube coking and nozzle blockage in Pratt & Whitney PW4000 series turbofan engines. This issue affects engines installed on aircraft such as the Airbus A300, A310, A330, Boeing 747-400, 767, 777, and McDonnell Douglas MD-11. The bulletin provides guidance on proper cleaning and inspection procedures during engine overhaul to prevent reduced oil flow and possible engine damage.

Safety Information Bulletin

Airbus A300
Airbus A310
Airbus A330
Boeing 747-400
Boeing 767
Boeing 777
McDonnell Douglas MD-11

EASA SIB 2011-20R1

Rockwell Collins TPR 901 Mode S Transponder - Incorrect —Downlink Aircraft Identification— and Incorrect Operation with Airport Ground Tracking Systems

EASA Safety Information Bulletin SIB No. 2011-20R1 addresses issues with the Rockwell Collins TPR 901 Mode S transponder, Part Number 822-1338-003, installed on various aircraft including Boeing 747-400 series modified under FAA STC ST01202WI-D and its European validation. The bulletin highlights problems with incorrect downlink aircraft identification and improper operation with airport ground tracking systems caused by certain transponder modifications. It provides information on service bulletins and recommended corrective actions to resolve these anomalies.

Safety Information Bulletin

Boeing 747-400

EASA SIB 2011-23R1

Koito Industries Seats — EASA Airworthiness Directive (AD) 2011-0098 — Compliance Information

EASA Safety Information Bulletin 2011-23R1 provides compliance guidance for EASA Airworthiness Directive 2011-0098 concerning seats manufactured by Koito Industries installed on Airbus, Boeing, Fokker, and McDonnell Douglas aircraft. It details acceptable methods for demonstrating compliance using similarity concepts and outlines procedures for obtaining approval of certification programs and test plans. The bulletin includes updated seat model clusters and critical part numbers relevant to static and dynamic strength testing.

Safety Information Bulletin

Airbus
Boeing
Fokker
McDonnell Douglas

EASA SIB 2008-19R2

Catalytic Oxidation of Aircraft Carbon Brakes due to Runway De-Icers

EASA Safety Information Bulletin 2008-19R2 addresses the catalytic oxidation of aircraft carbon brakes caused by runway de-icers, specifically affecting all large aeroplanes equipped with carbon brakes operating at airports using such chemicals. The bulletin highlights the risk posed by organic salt-based runway de-icers, such as potassium formate and acetate, which can penetrate brake components and accelerate carbon brake degradation. It also notes additional corrosion and electrical wiring issues linked to these de-icers, particularly on older aircraft.

Safety Information Bulletin

EASA SIB NM-13-25

Gulfstream Aerospce Corporation Model GVI Airplanes - Landing Gear - Nose Wheel Steering

The Special Airworthiness Information Bulletin SAIB: NM-13-25 is an FAA informational bulletin addressing a nose wheel steering issue on Gulfstream Aerospace Corporation Model GVI airplanes. It informs operators about a potential loss of nose wheel steering function after landing, triggered by a "Steer by Wire Fail" caution message. The bulletin provides details on the failure mode and interim operational guidance.

Safety Information Bulletin

Gulfstream GVI

EASA SIB CE-13-22

W31 series Switch Style Circuit Breakers (SSCB) manufactured by Tyco or Potter Brumfield

The FAA Special Airworthiness Information Bulletin SAIB: CE-13-22 addresses airworthiness concerns related to W31 series switch style circuit breakers (SSCB) manufactured by Tyco or Potter Brumfield. These SSCBs are installed on various Cessna models including 401, 402, 404, 411, 414, 421, 425, and 441, as well as Beechcraft models such as F33 Series, G33, V35B, A36, B36TC, and others. The bulletin highlights failure modes that can cause power loss or overheating, potentially leading to smoke or fire hazards.

Safety Information Bulletin

Cessna 401
Cessna 402
Cessna 404
Cessna 411
Cessna 414
Cessna 421
Cessna 425
Cessna 441
Beechcraft F33 Series
Beechcraft G33
Beechcraft V35B
Beechcraft A36
Beechcraft B36TC

EASA SIB NE-13-21

Goodrich — P/N 3E1150-10 and P/N 3E1150-12 Propeller De-Ice Timer Failures

The FAA Special Airworthiness Information Bulletin NE-13-21 addresses failures in Goodrich Corporation propeller de-ice timers, part numbers 3E1150-10 and 3E1150-12, which are installed on various propeller-driven aircraft with Goodrich electrical propeller de-ice systems. The bulletin informs owners and operators about the risk of loss of propeller ice protection due to circuit board corrosion in these timers. This information bulletin is advisory and does not mandate regulatory action under 14 CFR part 39.

Safety Information Bulletin

EASA SIB NM-13-19

Hawker Beechcraft 400, 400A and 400T Aeroplanes — Airfoil Anti/De-ice System

Special Airworthiness Information Bulletin SAIB: NM-13-19 is an FAA informational bulletin addressing an airworthiness concern with the Metal Oxide Semiconductor Field Effect Transistor (MOSFET) contactors used in the horizontal stabilizer de-ice system on Hawker Beechcraft 400, 400A, and 400T aeroplanes. The affected aircraft include Hawker 400 models with serial numbers RJ-1 through RJ-65, Hawker 400A models with serial numbers RK-1 through RK-379, and Hawker 400T models with serial numbers TX-1 through TX-13. This bulletin provides guidance on inspection and replacement procedures for the MOSFET contactors to prevent overheating and failure.

Safety Information Bulletin

Hawker Beechcraft 400
Hawker Beechcraft 400A
Hawker Beechcraft 400T

EASA SIB NM-13-20

Hawker Beechcraft Hawker 750 Aeroplanes — Communications System Wiring

Special Airworthiness Information Bulletin SAIB: NM-13-20 is an FAA informational bulletin addressing a wiring issue in Hawker Beechcraft Hawker 750 airplanes with specific serial numbers. The bulletin highlights an airworthiness concern related to under-gauge wiring in the Aircell cabin phone system. It applies to Hawker 750 aircraft with serial numbers HB-1 through HB-9, HB-11 through HB-14, HB-17 through HB-26, HB-28 through HB-32, HB-34, HB-36 through HB-40, HB-43, HB-63, HB-67 through HB-69, and HB-71.

Safety Information Bulletin

Hawker Beechcraft Hawker 750

EASA SIB NE-13-15

Continental Motors, Inc. (formerly Teledyne Continental) Throttle and Mixture Control Levers.

The FAA Special Airworthiness Information Bulletin NE-13-15 provides information regarding throttle and mixture control levers manufactured by Continental Motors, Inc. (formerly Teledyne Continental) for certain continuous flow, fuel injected engines excluding FADEC-equipped models. Affected engines include IO-240, IO-360, LTSIO-360, TSIO-360, IO-346, IO-470, GIO-470, TSIO-470, IO-520, GTSIO-520, LIO-520, TSIO-520, IO-550, GIO-550, TSIO-550, and TSIOL-550. The bulletin addresses an airworthiness concern related to bronze throttle and mixture control levers that may loosen during service, potentially causing loss of throttle or mixture control.

Safety Information Bulletin

EASA SIB CE-13-16

Cessna 172RG, R182, 210 and T303 Aeroplanes — Hydraulic Power Pack / Landing Gear System

The Special Airworthiness Information Bulletin SAIB: CE-13-16 is an FAA advisory concerning the hydraulic power pack and landing gear system on Cessna Aircraft Company Models 172RG, R182, TR182, FR182, 210N, T210N, 210R, T210R, P210N, P210R, and T303 airplanes. It addresses an airworthiness concern related to potential fire hazards originating from the landing gear hydraulic power pack system due to improper installation and wiring issues. This bulletin provides safety information but does not mandate regulatory action.

Safety Information Bulletin

Cessna 172RG
Cessna R182
Cessna TR182
Cessna FR182
Cessna 210N
Cessna T210N
Cessna 210R
Cessna T210R
Cessna P210N
Cessna P210R
Cessna T303

EASA SIB 2013-03

Seat Track Monument Fittings Replacement

EASA Safety Information Bulletin SIB No: 2013-03 titled 'Seat Track Monument Fittings Replacement' addresses concerns related to seat track lower attachment fittings Part Number ABS1262C010 installed on Airbus A318, A319, A320, A321, A330-243, and A330-343 aircraft. The bulletin informs operators about engineering static load test failures indicating these fittings may not meet required load specifications. It highlights that while Airbus-installed fittings comply with certification requirements, fittings installed via Supplemental Type Certificate modifications may pose a safety risk.

Safety Information Bulletin

Airbus A318
Airbus A319
Airbus A320
Airbus A321
Airbus A330-243
Airbus A330-343

EASA SIB 2013-02

Stall and Stick Pusher Training

EASA Safety Information Bulletin SIB No. 2013-02 titled "Stall and Stick Pusher Training" provides recommendations for fixed-wing aeroplane manufacturers, operators, and training organisations on best practices for stall warning, aerodynamic stall, and stick pusher activation training. The document references FAA Advisory Circular 120-109 and includes a stall recovery template developed by major manufacturers such as Airbus, ATR, Boeing, Bombardier, and Embraer. It aims to improve pilot recognition and response to stall events to enhance overall flight safety.

Safety Information Bulletin

EASA SIB 2013-01

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. 2013-01 notifies aviation stakeholders about unapproved parts due to theft reported by Ente Nazionale Aviazione Civile (ENAC) Italy. The bulletin lists specific stolen aviation products, parts, and equipment including King ADF receivers and indicators, Mid Continent turn coordinator, Electrosystem alternator, Hartzell propeller, and Prestolite starter. These parts are considered unapproved and should not be installed on any aircraft.

Safety Information Bulletin

EASA SIB CE-12-44

Piper PA-23-250 Aeroplanes with Lycoming IO-540-C4B5 Engines (Exhaust systems)

The Special Airworthiness Information Bulletin SAIB: CE-12-44 is an FAA informational bulletin concerning the exhaust systems of Piper PA-23-250 (Aztec) aircraft equipped with Lycoming IO-540-C4B5 engines. It addresses airworthiness concerns related to the engines' crossover exhaust assemblies, highlighting potential durability and functional issues without mandating regulatory action. The bulletin provides guidance for inspection and maintenance to prevent exhaust system failures.

Safety Information Bulletin

Piper PA-23-250

EASA SIB 2012-19R1

Uncommanded Engine In-Flight Shutdown triggered by the Tachometer Box

EASA Safety Information Bulletin SIB No. 2012-19R1 addresses uncommanded engine in-flight shutdowns triggered by the tachometer box on Turboméca ARRIEL 1E2 and ARRIEL 1S1 engines. These engines are installed on Eurocopter Deutschland MBB-BK 117 C-1 and C-2 helicopters, as well as Sikorsky S-76A and S-76C series helicopters. The bulletin provides information on the issue and recommends modifications to improve tachometer box reliability and mitigate shutdown risks.

Safety Information Bulletin

Eurocopter Deutschland MBB-BK 117 C-1
Eurocopter Deutschland MBB-BK 117 C-2
Sikorsky S-76A
Sikorsky S-76C