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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 AD 2018-0107

[Correction] Fuel Cell Systems — Lindstrand T30 Propane Cylinders — Removal from Service

EASA Airworthiness Directive 2018-0107 is a correction notice addressing the removal from service of Lindstrand T30 propane cylinders used in various hot air balloons. The directive applies to multiple balloon manufacturers and models listed under specific Type Certificate Data Sheets (TCDS). It mandates the replacement of affected Lindstrand T30 propane cylinders due to welding defects that could lead to propane leaks and potential fire or explosion hazards.

May 22, 2018
Airworthiness DirectiveMaintenanceSafety MgmtAerostats MA Series Hot Air BalloonsBallons Chaize CS SERIES HOT AIR BALLOONSBallons Chaize JZ SERIES HOT AIR BALLOONSBallons Chaize JZX SERIES HOT AIR BALLOONSBallons Libert Libert Hot Air BalloonsBallonservice & Technik Schoen Hot Air BalloonsCameron Balloons Cameron Special Shape Hot Air BalloonsCameron Balloons Gas BalloonsCameron Balloons Helium-Hot Air BalloonsCameron Balloons Hot Air BalloonsCameron Balloons Sky Hot Air BalloonsKubicek Factory S.R.O AB 2 Hot Air BalloonsKubicek Factory S.R.O AB 8 Hot Air BalloonsKubicek Factory S.R.O AEROTECHNIK AB Hot Air BalloonsKubicek Factory S.R.O BB Hot Air BalloonsKubicek Factory S.R.O Special Shape Hot Air BalloonsLindstrand Technologies 203T HiFlyerSchroeder Fire Balloons fire balloons GSchroeder Fire Balloons fire balloons S - Special Shape BalloonsUltramagic Hot Air BalloonsUltramagic Special Shape Hot Air Balloons

EASA AD US-2018-10-02

Equipment/Furnishings - Part Number of the Occupant Restraint System on the Standard Attendant Seats - Inspections

The Federal Aviation Administration's Airworthiness Directive 2018-10-02 addresses all Boeing Model 787-8 airplanes. It mandates inspection of the occupant restraint system part numbers on standard attendant seats and requires additional inspections and corrective actions if necessary. This directive aims to ensure the integrity of the restraint systems due to identified production issues.

May 22, 2018
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 787Boeing 787-8

EASA AD 2018-0110

Engine — Modification

EASA Airworthiness Directive 2018-0110 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A320-271N, A321-271N, A321-272N, A321-271NX, and A321-272NX aeroplanes. It addresses a software issue in the Full Authority Digital Engine Control Electronic Engine Controllers (FADEC EEC) that could prevent engine restart under certain conditions. The directive mandates modification of affected FADEC EECs to software standard FCS4.4 to ensure safe engine restart capability.

May 18, 2018
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A320Airbus A321Airbus A320-271NAirbus A321-271NAirbus A321-272NAirbus A321-271NXAirbus A321-272NX

EASA AD US-2018-10-08

Stabilizers - Vertical Stabilizer Leading Edge / Spar Cap - Inspectons

Airworthiness Directive 2018-10-08 is a final rule issued by the Federal Aviation Administration (FAA) addressing certain Boeing Model 717-200 airplanes. It mandates repetitive inspections of the vertical stabilizer leading edge skin and front spar cap for distress, cracking, and loose or missing fasteners to ensure structural integrity. This directive updates previous requirements to include new compliance times and aims to prevent potential loss of the vertical stabilizer due to structural failure.

May 18, 2018
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 717Boeing 717-200

EASA SIB CASA-2018-05

Pratt & Whitney Canada Pt6b-37a Engines with Fuel Control Units Overhauled after December 2016

The Transport Canada Civil Aviation Safety Alert CASA 2018-05 addresses a quality issue affecting Pratt & Whitney Canada PT6B-37A engines with fuel control units overhauled after December 2016. Some fuel control units may not have been calibrated to specification, potentially causing N1 fluctuations, hung starts, and inability to recover power during autorotation training. This alert is intended for owners, operators, and maintainers of the affected engines.

May 17, 2018
Safety Information BulletinMaintenanceSafety MgmtTraining

EASA AD 2018-0109

SUPERSEDED BY EASA AD 2018-0211

EASA Airworthiness Directive 2018-0109 is an airworthiness directive addressing fan blade inspections for CFM International CFM56-7B engines installed on Boeing 737-600, 737-700, 737-800, and 737-900 aircraft. It mandates ultrasonic inspections of specific affected fan blades to prevent potential fan blade failure and uncontained debris release. The directive applies to multiple CFM56-7B engine variants and specifies compliance procedures and corrective actions.

May 17, 2018
Airworthiness DirectiveMaintenanceSafety MgmtCFM International CFM56-7BBoeing 737-600Boeing 737-700Boeing 737-800Boeing 737-900

EASA SIB 2018-09

Non Recognition of Aeroplanes by Advanced Visual Docking Systems at Aerodromes

EASA Safety Information Bulletin No. 2018-09 is an informational bulletin addressing the issue of advanced visual docking guidance systems (A-VDGS) failing to recognize aeroplanes, particularly those with dark-colored exteriors, at aerodromes. The bulletin highlights occurrences involving various A-VDGS types where aeroplanes were not identified, leading to safety concerns such as collisions with passenger bridges. This bulletin is relevant to aerodrome operators and competent authorities but does not specify particular aircraft or engine models.

May 16, 2018
Safety Information BulletinSafety Mgmt

EASA AD 2018-0108

Door — Passenger Doors Frameside Fittings — Modification

EASA Airworthiness Directive 2018-0108 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A350-941 aeroplanes. It addresses a corrosion protection issue related to the passenger door frameside fittings on these aircraft. The directive mandates a modification to improve sealing and prevent water ingress in the door joints.

May 15, 2018
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A350Airbus A350-941

EASA AD US-2018-09-08

Fuselage - Frame Web of Air-Conditioning Support Brackets - Inspection

The Federal Aviation Administration's Airworthiness Directive 2018-09-08 addresses certain Boeing 737-200, -300, -400, and -500 series airplanes. This directive mandates inspections of the fuselage frame web near the air-conditioning support brackets to detect cracks that could compromise structural integrity. It aims to prevent potential rapid decompression and structural failure due to frame web cracking.

May 15, 2018
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 737Boeing 737-200Boeing 737-300Boeing 737-400Boeing 737-500

EASA AD 2018-0106

Rotors Flight Control — Collective Controls / Protective Cover — Modification

EASA Airworthiness Directive 2018-0106 is issued for Airbus Helicopters EC 225 LP models to address a safety issue with the protective cover of the "SHEAR" control pushbutton on pilot and copilot collective sticks. The directive mandates modification of the protective cover to an improved design to prevent mechanical deformation that could lead to unintended shearing of the hoist cable. This AD applies to all serial numbers of the EC 225 LP helicopter.

May 10, 2018
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SA 330Airbus Helicopters AS 332Airbus Helicopters EC 225Airbus Helicopters EC 225 LP

EASA AD US-2018-03-03R1

Wings - Lower Forward Carry Through Spar Cap - Inspection / Replacement

The Federal Aviation Administration's Airworthiness Directive 2018-03-03 R1 revises the original AD 2018-03-03 for certain Textron Aviation Inc. Models 401, 401A, 401B, 402, 402A, 402B, 402C, 411, 411A, 414, 414A, 421, 421A, 421B, 421C, and 425 airplanes. This directive addresses the inspection and replacement of the left and right forward lower carry through spar caps to detect and correct cracks caused by metal fatigue. The AD aims to prevent potential failure of the spar cap during flight, which could lead to loss of control.

May 9, 2018
Airworthiness DirectiveMaintenanceSafety MgmtTextron Aviation 401Textron Aviation 402Textron Aviation 411Textron Aviation 414Textron Aviation 421Textron Aviation 425 (Conquest)Textron Aviation 401ATextron Aviation 401BTextron Aviation 402ATextron Aviation 402BTextron Aviation 402CTextron Aviation 411ATextron Aviation 414ATextron Aviation 421ATextron Aviation 421BTextron Aviation 421CTextron Aviation 425

EASA AD 2018-0105

Electric / Electronic Common Installation — Electrical Harness Brackets and Wire Bundles — Inspection

EASA Airworthiness Directive 2018-0105 is an official safety directive addressing inspection requirements for electrical harness brackets and wire bundles on ATR 42 and ATR 72 aeroplanes. It applies specifically to certain manufacturer serial numbers of ATR 42-500 and ATR 72-212A models. The directive mandates inspections to detect missing brackets and potential wire damage that could lead to system failures.

May 8, 2018
Airworthiness DirectiveMaintenanceSafety MgmtATR ATR42ATR ATR72ATR 42-500ATR 72-212A

EASA AD 2014-0114R2

Fuselage — Tail Boom / Fenestron Junction Frame — Inspection / Repair

EASA Airworthiness Directive 2014-0114R2 is an updated regulatory requirement addressing inspection and repair of the tail boom and Fenestron junction frame on Airbus Helicopters EC 130 B4 models. It applies to all serial numbers except those with specific reinforcement modifications or approved repairs. The directive mandates repetitive inspections to detect cracks that could lead to structural failure and potential loss of helicopter control.

May 8, 2018
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters AS 350Airbus Helicopters EC 130Airbus Helicopters EC 130 B4

EASA SIB 2018-08

WITHDRAWN - RECOMMENDATIONS NOT NEEDED ANYMORE. Refer to CAT.OP.MPA.185

EASA Safety Information Bulletin 2018-08 is an informational document addressing in-flight fuel management and the phraseology used for fuel-related communications between pilots and air traffic control. It applies to all aeroplane operators, pilots, air traffic service providers, and controllers, emphasizing the correct use of the MINIMUM FUEL declaration as per ICAO standards and European regulations. The bulletin clarifies that the MINIMUM FUEL declaration is not an emergency but a warning that an emergency may occur if further delays happen.

May 8, 2018
Safety Information BulletinFlight OpsSafety Mgmt

EASA AD CF-2018-12

Engine — Material Anomaly for Certain High Pressure (HP) Centrifugal Impellers

The Canadian Airworthiness Directive CF-2018-12 addresses a material anomaly in certain Pratt & Whitney Canada PW150A engine high pressure (HP) centrifugal impellers. This directive applies to impellers with specific serial numbers listed in P&WC Service Bulletin 35331 Revision 1. It aims to prevent severe engine and aircraft damage caused by potential impeller failure due to a microstructure anomaly.

May 7, 2018
Airworthiness DirectiveMaintenanceSafety MgmtPratt & Whitney Canada PW150

EASA AD 2018-0101

SUPERSEDED BY EASA AD 2018-0277

EASA Airworthiness Directive 2018-0101 is an airworthiness directive issued by the European Aviation Safety Agency affecting all Dassault Aviation Falcon 7X aeroplanes, including all configurations such as mod M1000 (F8X). This directive mandates compliance with updated airworthiness limitations and maintenance tasks as specified in Chapter 5-40 of the Dassault Falcon 7X Aircraft Maintenance Manual Revision 5.

May 3, 2018
Airworthiness DirectiveMaintenanceSafety MgmtDassault Falcon 7X

EASA AD US-2018-09-01

Wings - Main Landing Gear Beam Forward Support Fitting - Inspection

The Federal Aviation Administration Airworthiness Directive 2018-09-01 addresses all Boeing 737-100, -200, -200C, -300, -400, and -500 series airplanes. It mandates repetitive inspections of the main landing gear beam forward support fitting due to reported cracks that could compromise structural integrity. This directive aims to prevent potential fuel leaks, structural failures, or main landing gear collapse.

May 3, 2018
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 737Boeing 737-100Boeing 737-200Boeing 737-200CBoeing 737-300Boeing 737-400Boeing 737-500

EASA AD CF-2018-13

Equipment/Furnishing - Passenger Seats — Unsecured Passenger Safety Lap Belts

The Canadian Airworthiness Directive CF-2018-13 addresses unsecured passenger safety lap belts on Diamond Aircraft model DA 62 aeroplanes, specifically affecting numerous serial numbers including 62.009 through 62.C004. This directive mandates inspection and corrective actions to ensure lap belts are properly secured to the seat structure to maintain occupant safety. It includes operational limitations and maintenance requirements to mitigate risks associated with unsecured lap belts.

May 2, 2018
Airworthiness DirectiveMaintenanceSafety MgmtDiamond Aircraft Industries, DA 62Diamond DA 62

EASA AD CF-2018-14

Fuselage - Belly Fairing - Blocked Drainage Holes

Canadian Airworthiness Directive CF-2018-14 addresses a safety issue on Bombardier Inc. BD-700-1A10 and BD-700-1A11 aircraft models. The directive mandates inspection and removal of sealant blocking drainage holes on the belly fairing forward and middle access panels to ensure proper fluid drainage. This measure is critical to prevent accumulation of flammable fluids or vapors in the belly fairing area.

May 2, 2018
Airworthiness DirectiveMaintenanceSafety MgmtBombardier BD-700Bombardier BD-700-1A10Bombardier BD-700-1A11

EASA AD 2018-0103

Flight Controls — Aileron Bellcrank Support Bracket — Inspection / Replacement

EASA Airworthiness Directive 2018-0103 is an airworthiness directive issued by EASA concerning SAAB 2000 aeroplanes. It addresses a manufacturing defect in the aileron bellcrank support brackets, specifically those with part numbers 7327993-813 and 7327993-814, which may have insufficient lug thickness attaching the bracket to the wing rear spar. The directive mandates inspection, possible repetitive inspections, reporting, and replacement of affected support brackets to ensure continued safe flight control operation.

Apr 30, 2018
Airworthiness DirectiveMaintenanceSafety MgmtSaab Ab 2000SAAB 2000