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EASA Regulations & Airworthiness Directives

Browse 4771 EASA regulations with AI-powered summaries.

Aircraft:AllAirbus A320262Airbus A321257Airbus A319229Airbus A350206Airbus A330197All177Airbus A318172Boeing 737164Airbus A380162Airbus A340136Airbus A350-941119Airbus Helicopters AS 332110Airbus Helicopters EC 225107Airbus Helicopters SA 330107Boeing 787106Show all...

EASA SIB NE-19-16

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).

Dec 9, 2019
Safety Information BulletinSafety MgmtMaintenance

EASA AD 2019-0296

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.

Dec 9, 2019
Airworthiness DirectiveMaintenanceSafety MgmtSafran ARRIUS 2Kamov Ka-226T

EASA AD US-2019-22-06

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.

Dec 9, 2019
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 737Boeing 737-800

EASA AD 2018-0142R1

SUPERSEDED BY EASA AD 2024-0100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.

Dec 9, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SA 330Airbus Helicopters AS 332Airbus Helicopters EC 225Airbus Helicopters AS 332 CAirbus Helicopters AS 332 C1Airbus Helicopters AS 332 LAirbus Helicopters AS 332 L1

EASA AD 2019-FATA-01020A-09

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.

Dec 9, 2019
Airworthiness DirectiveMaintenanceSafety MgmtIrkut Corporation Jsc RRJ-95RRJ-95

EASA AD 2019-FATA-01020A-07

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.

Dec 9, 2019
Airworthiness DirectiveMaintenanceSafety MgmtIrkut Corporation Jsc RRJ-95RRJ-95

EASA AD 2019-FATA-01020A-06

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.

Dec 9, 2019
Airworthiness DirectiveMaintenanceSafety MgmtIrkut Corporation Jsc RRJ-95RRJ-95

EASA AD 2019-0298-E

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.

Dec 9, 2019
Airworthiness DirectiveMaintenanceSafety MgmtStemme Ag ASPStemme AG ASP S15-1

EASA AD 2019-0295

SUPERSEDED BY EASA AD 2021-0222

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.

Dec 5, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SA 330Airbus Helicopters AS 332Airbus Helicopters EC 225Airbus Helicopters AS 332 CAirbus Helicopters AS 332 C1Airbus Helicopters AS 332 LAirbus Helicopters AS 332 L1

EASA SIB 2019-18

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.

Dec 4, 2019
Safety Information BulletinMaintenanceSafety Mgmt

EASA AD 2019-0293

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.

Dec 4, 2019
Airworthiness DirectiveMaintenanceSafety MgmtPilatus Aircraft PC-24Pilatus PC-24

EASA AD 2019-0292

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.

Dec 4, 2019
Airworthiness DirectiveMaintenanceSafety MgmtCeapr DR 400

EASA AD 2019-0294

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.

Dec 4, 2019
Airworthiness DirectiveMaintenanceSafety MgmtLeonardo S.P.A. Helicopters A109Leonardo S.P.A. Helicopters A119Leonardo A109SLeonardo AW109SP

EASA AD CF-2018-01R2

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.

Dec 2, 2019
Airworthiness DirectiveMaintenanceSafety MgmtDe Havilland Canada DHC-8De Havilland Aircraft of Canada Limited DHC-8-400De Havilland Aircraft of Canada Limited DHC-8-401De Havilland Aircraft of Canada Limited DHC-8-402

EASA SIB 2019-17

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.

Dec 2, 2019
Safety Information BulletinMaintenanceSafety Mgmt

EASA AD 2019-0290

Electrical Routing — Electrical Harness under Panel 295CL — Modification

EASA Airworthiness Directive 2019-0290 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting ATR 72 aeroplanes, excluding certain serial numbers and those with ATR modification 07988 embodied in production. The directive addresses an unsafe condition related to electrical wiring routing under panel 295CL on the left-hand side wing rear spar. It mandates a modification to the electrical harness clamp installation to prevent wire chafing and potential fire hazards.

Nov 29, 2019
Airworthiness DirectiveMaintenanceSafety MgmtATR ATR72ATR 72

EASA AD 2018-0095R1

Engine — Intermediate Pressure Compressor Rotor Seal — Inspection / De-Pairing Limitation

EASA Airworthiness Directive 2018-0095R1 is an updated safety directive addressing inspection and operational limitations for the intermediate pressure compressor (IPC) rotor buffer seal on Rolls-Royce Trent 1000 series engines, which power Boeing 787-8 and 787-9 aircraft. The directive mandates repetitive borescope inspections and sets operational restrictions to prevent engine power loss caused by seal cracking. It also introduces an optional modification that can terminate the inspection requirements.

Nov 29, 2019
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg TRENT 1000Boeing 787-8Boeing 787-9

EASA AD 2018-0094R1

Engine — Intermediate Pressure Compressor Rotor Seal — Inspection / De-Pairing Limitations

EASA Airworthiness Directive 2018-0094R1 is a regulatory update addressing inspection and de-pairing limitations for the intermediate pressure compressor rotor seal on Rolls-Royce Trent 1000 engines installed on Boeing 787-8 and 787-9 aircraft. The directive mandates repetitive borescope inspections and corrective actions for affected seals to prevent engine power loss. It also introduces optional terminating actions through specific Rolls-Royce service bulletins.

Nov 29, 2019
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg TRENT 1000Boeing 787-8Boeing 787-9