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 AD 2019-0299

Dec 10, 2019

Engine — High Pressure Turbine Stage 1 Discs — Life Limit Reduction / Replacement

EASA Airworthiness Directive 2019-0299 is an airworthiness directive addressing Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20, and BR700-710C4-11 engines installed on aircraft such as Bombardier BD-700-1A10, BD-700-1A11, Gulfstream G500, and G550. The directive focuses on reducing the life limit and requiring replacement of certain high pressure turbine stage 1 discs due to a manufacturing quality issue. It mandates identification and removal of affected parts to ensure continued airworthiness and safety.

Airworthiness Directive

Rolls-Royce Deutschland Ltd & Co Kg BR700-710
Bombardier BD-700-1A10
Bombardier BD-700-1A11
Gulfstream G500
Gulfstream G550

EASA SIB CE-19-20

Dec 10, 2019

Gulfstream Aerospace Corporation G-1159A (G-III), G-IV, GIV-X, GV, GV-SP, and GVI Aeroplanes - Flight Compartment Windows

The Gulfstream Aerospace Corporation G-1159A (G-III), G-IV, GIV-X, GV, GV-SP, and GVI Aeroplanes - Flight Compartment Windows Special Airworthiness Information Bulletin (SAIB: CE-19-20) informs operators about windshield failures on these Gulfstream models. It highlights incidents involving arcing, cracking, smoke, and small fires related to the flight compartment windows and introduces a new windshield design with an improved heater terminal block for replacements.

Safety Information Bulletin

EASA SIB CE-19-19

Dec 10, 2019

Rockwell Collins TDR-94 and TDR-94D ATC/Mode S Transponders - Update of the Transponder System

The Special Airworthiness Information Bulletin SAIB: CE-19-19 informs owners and operators about detection and tracking issues with aircraft equipped with Rockwell Collins TDR-94 and TDR-94D ATC/Mode S Transponders modified by Service Bulletin TDR-94()-34-30. This bulletin addresses problems experienced by certain ground stations outside the United States, including Multilateration (MLAT) and Air Traffic Control Radar Beacon System (ATCRBS) stations. The issue does not currently warrant an airworthiness directive under 14 CFR part 39.

Safety Information Bulletin

EASA AD 2019-0273R1

Dec 9, 2019

Airplane Flight Manual — Section Normal Procedures — Amendment

EASA Airworthiness Directive 2019-0273R1 is an amendment addressing the Falcon 900EX and Falcon 2000EX aeroplanes equipped with Dassault's EASy configurations. It mandates changes to the Airplane Flight Manual normal procedures to prevent icing of angle of attack and pitot probes during take-off. This directive ensures safer operation by requiring flight crews to manually activate probe heating during line up.

Airworthiness Directive

Dassault Falcon 2000
Dassault Falcon 900EX
Dassault Falcon 2000EX

EASA SIB NE-19-16

Dec 9, 2019

Avidyne SkyTrax6XXA Software - Traffic Advisory System - Failure to Display Traffic

The Special Airworthiness Information Bulletin SAIB: NE-19-16 is an FAA informational bulletin addressing a software issue in certain Avidyne SkyTrax6XXA (TAS6XXA) traffic advisory systems used in general aviation aircraft. The affected units, identified by part number 700-00185-() with flight software P/N 510-00296-000 Revisions 00, 01, and 02 (Releases 2.0.0, 2.0.1, and 2.0.2), may intermittently fail to display traffic on interfaced RS-232 display systems. This issue is resolved in flight software Revision 03 (Release 2.0.3).

Safety Information Bulletin

EASA AD 2019-0296

Dec 9, 2019

Engine Fuel & Control — Fuel Filter Pre-Blockage Pressure Switch — Replacement

EASA Airworthiness Directive 2019-0296 is an airworthiness directive addressing SAFRAN Helicopter Engines ARRIUS 2G1 engines, commonly installed on Kamov Ka-226T helicopters. The directive mandates the replacement of certain fuel filter pre-blockage pressure switches identified by specific part and serial numbers due to potential non-conformities. This AD aims to ensure continued safe operation by preventing uncommanded engine shutdowns caused by fuel filter contamination.

Airworthiness Directive

Safran ARRIUS 2
Kamov Ka-226T

EASA AD US-2019-22-06

Dec 9, 2019

Fuel - Fuel Quantity Indicating System Tank Unit - Inspection

Federal Register Volume 84, Number 227 (November 25, 2019) - Airworthiness Directive 2019-22-06 is a final rule issued by the FAA affecting certain Boeing 737-800 series airplanes modified with split winglets per STC ST00830SE. This directive addresses inadequate clearance between the fuel quantity indicating system (FQIS) tank unit and a reinforcement angle added during the split winglet modification, which could pose a fire risk.

Airworthiness Directive

Boeing 737800

EASA AD 2018-0142R1

Dec 9, 2019

Superseded by EASA AD 2024-0100

EASA Airworthiness Directive 2018-0142R1 is an amendment addressing Airbus Helicopters AS 332 C, C1, L, and L1 models equipped with dual hoist installations and de-icing systems. This directive focuses on mitigating a vibration issue around 12 Hz caused by specific helicopter configurations that could lead to structural failure or loss of control. It provides requirements for removal of certain dual hoist parts or the de-icing system, or alternatively, operational flight envelope limitations for AS 332 L and L1 helicopters.

Airworthiness DirectiveSuperseded

Airbus Helicopters SA 330
Airbus Helicopters AS 332
Airbus Helicopters EC 225
Airbus Helicopters AS 332 C
Airbus Helicopters AS 332 C1
Airbus Helicopters AS 332 L
Airbus Helicopters AS 332 L1

EASA AD 2019-FATA-01020A-05

Dec 9, 2019

Superseded by FATA AD 2021-FATA-01020A-07

SUPERSEDED BY FATA AD 2021-FATA-01020A-07 is an aviation regulatory document indicating that the current directive has been replaced by FATA AD 2021-FATA-01020A-07. The document does not provide details on specific affected aircraft, engines, or parts.

Airworthiness Directive

Irkut Corporation Jsc RRJ-95

EASA AD 2019-FATA-01020A-09

Dec 9, 2019

Superseded by FATA AD 2021-FATA-01020A-07

Airworthiness Directive 2019-FATA-01020A-09 issued by the Federal Air Transport Agency of the Russian Federation applies to RRJ-95 aircraft manufactured in the Russian Federation. This directive extends the validity of the previous Airworthiness Directive 2019-FATA-01020F-05 to continue mandatory inspections and corrective actions related to cracks detected in the slat hinge plates of RRJ-95 aircraft. The directive mandates ongoing inspections and replacements to ensure continued airworthiness.

Airworthiness Directive

Irkut Corporation Jsc RRJ-95
RRJ-95

EASA AD 2019-FATA-01020A-07

Dec 9, 2019

Superseded by FATA AD 2021-FATA-01020A-07

Airworthiness Directive 2019-FATA-01020A-07 issued by the Federal Air Transport Agency of the Russian Federation addresses mandatory inspections and corrective actions for RRJ-95 aircraft. It corrects references related to the one-time inspection of bearings in the links of tracks of slat section 1 on the left-hand and right-hand outer wings. The directive provides updated inspection procedures and replacement requirements to ensure continued airworthiness.

Airworthiness Directive

Irkut Corporation Jsc RRJ-95
RRJ-95

EASA AD 2019-FATA-01020A-06

Dec 9, 2019

Superseded by FATA AD 2021-FATA-01020A-07

Airworthiness Directive 2019-FATA-01020A-06 issued by the Federal Air Transport Agency of the Russian Federation addresses cracks found on the inner ring of bearings of the link of track of slat sections on RRJ-95 aircraft. This directive mandates inspections and replacements of affected track link assemblies on specific RRJ-95 aircraft with manufacturer serial numbers ranging from 95007 to 95220. The directive aims to ensure continued airworthiness and safety of the RRJ-95 fleet by timely detecting and correcting these structural issues.

Airworthiness DirectiveSuperseded

Irkut Corporation Jsc RRJ-95
RRJ-95

EASA AD 2019-0298-E

Dec 9, 2019

Wings — Outer Wing Shear Bolts — Inspection

EASA Airworthiness Directive 2019-0298-E is an emergency directive addressing the inspection of outer wing shear bolts on Stemme AG ASP S15-1 aeroplanes, specifically serial numbers ASP-031 and ASP-034 through ASP-043. The directive mandates inspection and corrective actions for outer wing shear bolts with Part Number 365058 to prevent potential wing separation. This directive applies to affected parts installed on both outer wings of the specified aircraft.

Airworthiness Directive

Stemme Ag ASP
Stemme AG ASP S15-1

EASA AD 2019-0295

Dec 5, 2019

Fuselage – Main Gearbox Suspension Bar Attachment Fittings and Screws – Inspection

EASA Airworthiness Directive 2019-0295 is an airworthiness directive issued by the European Union Aviation Safety Agency concerning Airbus Helicopters AS 332 C, C1, L, and L1 models. It addresses corrosion found on the main gearbox suspension bar attachment fittings and screws, which could lead to structural failure and detachment of the suspension bars. The directive mandates inspections and corrective actions to ensure continued airworthiness.

Airworthiness DirectiveSuperseded

Airbus Helicopters SA 330
Airbus Helicopters AS 332
Airbus Helicopters EC 225
Airbus Helicopters AS 332 C
Airbus Helicopters AS 332 C1
Airbus Helicopters AS 332 L
Airbus Helicopters AS 332 L1

EASA SIB 2019-18

Dec 4, 2019

CFM International CFM 56-7B Engines - Fan blades — Life Limitation

EASA Safety Information Bulletin 2019-18 is an informational document addressing fan blade life limitations for CFM International CFM56-7B engines, which are installed on Boeing 737-600, 737-700, 737-800, and 737-900 aircraft. The bulletin discusses reported fan blade failures due to fatigue fractures and references related service bulletins and EASA Airworthiness Directive 2019-0018. It provides recommendations to enhance safety by implementing fan blade life limits but does not impose mandatory requirements.

Safety Information Bulletin

EASA AD 2019-0293

Dec 4, 2019

Equipment and Furnishings — Emergency Exits / Grommets — Replacement

EASA Airworthiness Directive 2019-0293 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Pilatus Aircraft Ltd PC-24 aeroplanes. It addresses the replacement of vinyl grommets used in the emergency exits, which may become rigid after exposure to low temperatures. The directive applies to all PC-24 aircraft serial numbers and mandates replacing affected grommets to ensure emergency exits function properly during evacuation.

Airworthiness Directive

Pilatus Aircraft PC-24
Pilatus PC-24

EASA AD 2019-0292

Dec 4, 2019

Stabilizers — Stabilator — Inspection

EASA Airworthiness Directive 2019-0292 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting CEAPR DR 400 aeroplanes, including multiple DR 400 variants up to serial number 2723. The directive mandates inspection of the stabilator attachment to detect potential deformation and incorrect positioning of internal wedges in the false spar. This inspection aims to prevent possible detachment of the stabilator, which could lead to loss of control of the aircraft.

Airworthiness Directive

Ceapr DR 400

EASA AD 2019-0294

Dec 4, 2019

Stabilizers — Vertical Fin Vibration Absorber — Inspection / Removal

EASA Airworthiness Directive 2019-0294 is an official regulatory document addressing the inspection and removal of the vertical fin vibration absorber on Leonardo S.p.A. A109S and AW109SP helicopters. It mandates inspections and corrective actions to address cracks and damage found on the vertical fin vibration absorber and surrounding structure. This directive applies to all serial numbers of the affected helicopter models and aims to ensure continued airworthiness and structural integrity.

Airworthiness Directive

Leonardo S.P.A. Helicopters A109
Leonardo S.P.A. Helicopters A119
Leonardo A109S
Leonardo AW109SP

EASA AD CF-2018-01R2

Dec 2, 2019

Landing Gear — Nose Landing Gear Drag Strut Lock Link Wear

The Airworthiness Directive CF-2018-01R2 addresses wear issues in the nose landing gear (NLG) drag strut lock link on De Havilland Aircraft of Canada Limited DHC-8-400, -401, and -402 models, serial numbers 4001 through 4585 and 4587. It mandates inspections and corrective actions to prevent NLG collapse caused by worn or loose bushings in the locking mechanism. This directive updates previous versions to clarify supersession and compliance requirements.

Airworthiness Directive

De Havilland Canada DHC-8
De Havilland Aircraft of Canada Limited DHC-8-400
De Havilland Aircraft of Canada Limited DHC-8-401
De Havilland Aircraft of Canada Limited DHC-8-402

EASA SIB 2019-17

Dec 2, 2019

Possible Improper Maintenance by Xtra Aerospace, LLC

EASA Safety Information Bulletin No. 2019-17 is an airworthiness bulletin addressing possible improper maintenance by Xtra Aerospace, LLC. It informs the European aviation community about the FAA's revocation of Xtra Aerospace's Part 145 certificate due to systemic approval of maintenance articles not listed on their operations specifications. This bulletin applies broadly to aircraft owners, operators, manufacturers, maintenance organizations, parts suppliers, and distributors, but does not target specific aircraft or engine models.

Safety Information BulletinSuperseded