EASA Regulations & Airworthiness Directives

Browse 5,166 EASA regulations with AI-powered summaries.

Aircraft:AllAirbus A320286Airbus A321285Airbus A319253Airbus A350224Airbus A330221Airbus A318189Airbus A380182Boeing 737175Airbus A340141Airbus A350-941134Airbus BD-500 (A220 Series)123Airbus Helicopters AS 332119Airbus Helicopters EC 225116Airbus Helicopters SA 330116Boeing 787116Show all...

EASA SIB NM-17-09

Mar 10, 2017

Boeing 767 Aeroplanes - Inboard Spoiler Power Control Actuators

The FAA Special Airworthiness Information Bulletin SAIB: NM-17-09 provides information for owners and operators of Boeing 767-200, -300, -300F, and -400ER series airplanes regarding inspection and maintenance procedural changes for certain inboard spoiler power control actuators (PCAs). This bulletin addresses a hydraulic fluid leakage issue linked to specific inboard spoiler PCAs on Model 767 airplanes with line numbers 1 through 1108. The document is informational and does not mandate regulatory action.

Safety Information Bulletin

EASA SIB 2017-03

Mar 6, 2017

Helicopter Stabilised Hover Checks Before Departure

EASA Safety Information Bulletin No. 2017-03 is a safety information bulletin addressing helicopter stabilized hover checks before departure. It applies to all rotorcraft operators and highlights safety concerns related to loss-of-control incidents during take-off, based on analyses by both the FAA and EASA. The bulletin references FAA SAFO 16016 and recommends procedures to enhance safety during helicopter take-off.

Safety Information BulletinSuperseded

EASA SIB 2017-02

Feb 28, 2017

WITHDRAWN - SEE FAA AD 2020-18-20

EASA Safety Information Bulletin 2017-02 is an informational document addressing inspection of main rotor blade abrasion strips on MD Helicopters, Inc. models 369D, 369E, 369F, 36D9FF, 500N, and 600N. It highlights reports of delamination and disbonding on low-time main rotor blades and references related service letters and mandatory service bulletins from MD Helicopters and Helicopter Technology Company. The bulletin is issued pending potential FAA Airworthiness Directive action and is not mandatory.

Safety Information Bulletin

EASA SIB 2016-20R1

Feb 21, 2017

ATR Flight Controls — Crew Resource Management — Avoiding Dual and Opposite Flight Control Inputs

EASA Safety Information Bulletin 2016-20R1 is an airworthiness bulletin addressing flight control issues on ATR42 and ATR72 aircraft. It focuses on Crew Resource Management to avoid dual and opposite flight control inputs that can cause structural damage, especially involving the pitch uncoupling mechanism and elevator controls. The bulletin provides updated operational guidance and references ATR service bulletins and operator messages for affected aircraft.

Safety Information Bulletin

EASA SIB NM-17-07

Jan 27, 2017

AmSafe, Inc. Restraint System Assemblies — End Release Buckle

The FAA Special Airworthiness Information Bulletin SAIB: NM-17-07 advises owners, operators, and manufacturers of Normal, Utility, Acrobatic, Commuter Category Aircraft, and Transport Category Airplanes about a potential failure in the end release buckle of certain AmSafe, Inc. restraint system assemblies installed on passenger seats. This bulletin highlights a manufacturing defect in buckle assemblies produced between November 2010 and November 2015 that could cause inadvertent release of restraints under load. The bulletin is informational and does not mandate regulatory action.

Safety Information Bulletin

EASA SIB NM-17-06

Jan 18, 2017

Boeing 737 Aeroplanes - Fuselage Skin Panels at the Chem-mill Steps

The Special Airworthiness Information Bulletin SAIB: NM-17-06 is an FAA informational bulletin addressing inspection procedures for fuselage skin panels at the chem-mill steps on Boeing 737-200, -200C, -300, -400, and -500 series airplanes. It informs operators about a new inspection procedure published by Boeing to detect cracking using an improved ultrasonic phased array method. This bulletin provides guidance but does not impose mandatory requirements.

Safety Information Bulletin

EASA SIB 2014-32R1

Jan 11, 2017

Alleged Examination Fraud at Part-147 Maintenance Training Organisation, Hellenic Aviation Training Academy

EASA Safety Information Bulletin 2014-32R1 addresses alleged examination fraud at the Part-147 Maintenance Training Organisation, Hellenic Aviation Training Academy (HATA). This bulletin affects all holders of Part-66 licences issued or amended based on HATA Certificates of Recognition (CoRs) for basic knowledge examinations in technical modules. It highlights safety concerns that some licence holders may lack sufficient knowledge to exercise their privileges safely.

Safety Information Bulletin

EASA SIB 2016-19R1

Jan 9, 2017

Honeywell Mode S Transponders: Enhanced Surveillance Parameters not provided to Mode S Ground Stations

EASA Safety Information Bulletin 2016-19R1 is an airworthiness bulletin addressing an issue with certain Honeywell Mode S transponders installed on aircraft such as Textron Aviation, Embraer, Gulfstream, and Learjet models. The bulletin clarifies that these transponders do not provide Enhanced Surveillance (EHS) parameters to Mode S ground stations, affecting compliance with European surveillance requirements. The affected transponders include models XS-852E, XS-852F, XS-857A, and XS-858A incorporated in specific Primus II and Primus EPIC communication units.

Safety Information Bulletin

EASA SIB 2016-21

Dec 23, 2016

WITHDRAWN - RECOMMENDATIONS NOT NEEDED ANYMORE

EASA Safety Information Bulletin No. 2016-21 is a safety information bulletin addressing a visual check on the Main Gearbox (MGB) and the flared housing for Airbus Helicopters SA365 / AS365 C, C1, C2, C3, N, N1, N2, N3, and EC155 B and B1 models. The bulletin informs about a non-conforming assembly of the MGB housing that may reduce lubrication but does not constitute an unsafe condition requiring an Airworthiness Directive. It provides guidance for operators to verify proper assembly through alignment of specific red markings on the MGB and flared housing.

Safety Information Bulletin

EASA SIB CE-17-03

Dec 21, 2016

Air Tractor AT-602, AT-802 and AT-802A Aeroplanes - Rudder Pedal Attach Assembly

The Special Airworthiness Information Bulletin SAIB CE-17-03 is an FAA informational bulletin addressing a flight control concern for Air Tractor Models AT-602, AT-802, and AT-802A airplanes. It highlights inspection procedures and maintenance recommendations for the rudder pedal attachment assembly to ensure continued airworthiness. This bulletin does not mandate regulatory action but provides guidance to prevent potential rudder pedal detachment.

Safety Information Bulletin

EASA SIB CE-17-04

Dec 20, 2016

M7 Aerospace (formerly Fairchild, Swearingen) SA226 and SA227 Aeroplanes - Main Landing Gear (MLG) Yoke Torque Link Lug and Shaft

The Special Airworthiness Information Bulletin SAIB: CE-17-04 is an FAA informational bulletin addressing an airworthiness concern for M7 Aerospace SA226 and SA227 series airplanes, specifically models SA226-T/-T(B)/-AT/-TC and SA227-TT/-AT/-AC/-BC/-CC/-DC. It focuses on inspection procedures and maintenance actions related to the main landing gear yoke torque link lug and shaft, which are critical components for directional ground control.

Safety Information Bulletin

EASA SIB CE-17-05

Dec 20, 2016

Piper PA-31 Floor-mounted Circuit Breaker (CB) Panel

The Special Airworthiness Information Bulletin SAIB: CE-17-05 is an FAA informational bulletin addressing an airworthiness concern for Piper Aircraft models PA-31T, PA-31T1, PA-31T2, PA-31T3, and PA-31P-350. It highlights potential wiring issues at the floor-mounted circuit breaker panel area that could lead to chafing, thermal stress, or arcing, posing a fire risk. The bulletin provides guidance on inspection and maintenance practices to mitigate these risks.

Safety Information Bulletin

EASA SIB CE-17-02

Dec 16, 2016

Piper PA-46 Aeroplanes — Alternative Method of Compliance (Optional Terminating Action) for FAA AD 2015-13-09

The document titled Piper PA-46 Aeroplanes — Alternative Method of Compliance (Optional Terminating Action) for FAA AD 2015-13-09 is a Special Airworthiness Information Bulletin (SAIB) issued by the FAA. It addresses Piper Models PA-46-350P and PA-46-500TP airplanes subject to FAA Airworthiness Directive 2015-13-09 concerning a cabin altitude encoder issue. The bulletin informs operators of an approved alternative method of compliance involving a permanent modification to resolve the issue.

Safety Information Bulletin

EASA SIB CASA-2016-13

Dec 16, 2016

Pratt & Whitney PW545 Series Engines - Oil Systems Servicing

The Transport Canada Civil Aviation Safety Alert CASA 2016-13 addresses oil system servicing issues on Pratt & Whitney PW545A, PW545B, and PW545C series engines. It highlights problems related to improper oil servicing that can lead to alert warnings and in-flight engine shutdowns. The document provides safety information and references Pratt & Whitney service information letter PW500-065 for further details.

Safety Information Bulletin

EASA SIB CASA-2016-11

Nov 24, 2016

Bell Helicopter Textron Canada 206L helicopters - Inspection and Replacement of Engine Mount Legs

The Transport Canada Civil Aviation Safety Alert CASA 2016-11 addresses the inspection and replacement of engine mount legs on Bell Helicopter Textron Canada 206L-series helicopters, including models 206L, 206L-1, 206L-3, and 206L-4. It highlights the importance of thoroughly inspecting these engine mount legs for corrosion and cracking, and replacing deteriorated parts to maintain airworthiness and safety.

Safety Information Bulletin

EASA SIB 2016-17

Nov 17, 2016

WITHDRAWN - SEE FAA AD 2017-08-07

EASA Safety Information Bulletin 2016-17 is an informational bulletin addressing potential skin corrosion under the oxygen line fairing on the upper fuselage of Learjet Inc. Model 60 aeroplanes, serial numbers 60-002 to 60-430 inclusive. The bulletin references Learjet Service Bulletin 60-53-19 for inspection procedures and highlights that the FAA is considering Airworthiness Directive action on this issue. This bulletin is not mandatory but serves to inform operators and maintainers of the safety concern.

Safety Information Bulletin

EASA SIB CE-16-27

Nov 3, 2016

Air Tractor AT-250, AT-300, AT-400, AT-500, AT-600 and AT-800 Series Aeroplanes - Wing Trailing Edge Flap Control System

The Special Airworthiness Information Bulletin SAIB: CE-16-27 is an FAA informational bulletin addressing a flap torque tube airworthiness concern for Air Tractor AT-250, AT-300, AT-400, AT-500, AT-600, and AT-800 series aeroplanes. It highlights inspection procedures and maintenance actions related to the trailing edge flap control system, specifically focusing on weld cracks in the flap torque tube actuator brackets. This bulletin applies to multiple Air Tractor models under Type Certificate Data Sheets A9SW, A17SW, and A19SW.

Safety Information Bulletin

EASA SIB SAFO16012

Oct 27, 2016

Braille Battery, Inc. - Lithium Ion Battery Shipments

Braille Battery, Inc. - Lithium Ion Battery Shipments is a Safety Alert for Operators (SAFO 16012) issued by the FAA to alert air carriers about lithium ion battery shipments from Braille Battery, Inc. that may not comply with Hazardous Materials Regulation (49 CFR §173.185) and ICAO Technical Instructions. The alert highlights the risk posed by lithium ion batteries that have not passed UN Manual of Tests and Criteria part III, sub-section 38.3, which are unsafe for air transport. This SAFO is relevant to all air carriers operating under 14 CFR parts 121, 129, and 135.

Safety Information Bulletin