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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 DCA-750XL-18B

Fin Forward Pickup — Inspection

The Airworthiness Directive DCA/750XL/18B Fin Forward Pickup – Inspection issued by the Civil Aviation Authority of New Zealand mandates inspection and maintenance actions for Pacific Aerospace 750XL aircraft, serial numbers up to 193, 195, and 197. It addresses potential fatigue cracks in the fin forward pickup component to ensure continued airworthiness and safety. The directive references Pacific Aerospace Limited Mandatory Service Bulletin PACSB/XL/068 issue 6 dated 8 January 2018 for detailed procedures.

Feb 23, 2018
Airworthiness DirectiveMaintenanceSafety MgmtNzskydive 750XLPacific Aerospace 750XL

EASA AD DCA-750XL-26

Rudder and Elevator Trim Drive Coupling - Modification

Airworthiness Directive DCA/750XL/26 Rudder and Elevator Trim Drive Coupling - Modification is issued by the Civil Aviation Authority of New Zealand and applies to Pacific Aerospace 750XL aircraft with specific serial numbers. The directive mandates modification of the rudder and elevator trim drive coupling to prevent disengagement issues. This ensures the continued safe operation of the affected aircraft by maintaining effective trim system functionality.

Feb 23, 2018
Airworthiness DirectiveMaintenanceSafety MgmtNzskydive 750XLPacific Aerospace 750XL

EASA AD DCA-750XL-22A

Ventilation Hose behind Instrument Panel - Inspection

Airworthiness Directive DCA/750XL/22A Ventilation Hose behind Instrument Panel - Inspection is issued by the Civil Aviation Authority of New Zealand and applies to all Pacific Aerospace 750XL aircraft with serial numbers up to and including 220. This directive mandates inspection and potential repair of the ventilation SCAT hose behind the instrument panel to prevent chafing damage to components and wiring. Compliance with the specified Pacific Aerospace Mandatory Service Bulletin PACSB/XL/083 issue 2 is required.

Feb 23, 2018
Airworthiness DirectiveMaintenanceSafety MgmtNzskydive 750XLPacific Aerospace 750XL

EASA AD 2018-0045

SUPERSEDED BY EASA AD 2018-0290

EASA Airworthiness Directive 2018-0045 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A350-941 aeroplanes. It addresses corrosion protection issues related to the vertical stabilizer tension bolts on these aircraft. The directive mandates a modification to improve corrosion protection and maintain structural integrity of the vertical tail plane.

Feb 22, 2018
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A350Airbus A350-941

EASA AD CF-2018-06

Floodlight Panel — Cockpit Floodlight Water Penetration

Airworthiness Directive CF-2018-06 is issued by Transport Canada and applies to Bombardier Inc. model CL-600-2B16 (650 variant) aircraft, serial numbers 6050 through 6070. This directive addresses the issue of water penetration into cockpit floodlight fixtures, which can cause electrical short circuits and potential fire hazards. It mandates the installation of gasket seals on the pilot and co-pilot floodlight fixtures to prevent fluid ingress.

Feb 21, 2018
Airworthiness DirectiveMaintenanceSafety MgmtBombardier CL-600 (Challenger)Bombardier CL-600-2B16

EASA SIB 2018-06

Incorrect Airport Surface Approaches and Landings

EASA Safety Information Bulletin No. 2018-06 is an informational document addressing the issue of incorrect airport surface approaches and landings. It highlights multiple incidents involving misaligned approaches to parallel runways and wrong runway landings reported by European operators and references similar concerns raised by the FAA. The bulletin applies to aeroplane operators, approved training organisations, air navigation service providers, air traffic controllers, and competent authorities within EASA member states.

Feb 19, 2018
Safety Information BulletinFlight OpsTrainingSafety Mgmt

EASA AD 2018-0046

Tail Rotor Drive — Tail Gear Box — Inspection / Replacement

EASA Airworthiness Directive 2018-0046 is an airworthiness directive issued by the European Union Aviation Safety Agency concerning Airbus Helicopters Deutschland GmbH MBB-BK 117 series helicopters. It mandates inspection and possible replacement or repair of the tail gear box (TGB) bellcrank attachment arm on affected MBB-BK117 A-1, A-3, A-4, B-1, B-2, C-1, and C-2 helicopters to address detected cracks. The directive applies to TGB parts with specific part numbers and aims to prevent potential loss of helicopter control.

Feb 19, 2018
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters MBB-BK 117

EASA AD US-2018-01-01

Fuel - Tail Fuel Tank Transfer Pump Wire Assemblies - Inspection

Airworthiness Directive 2018-01-01 is a final rule issued by the Federal Aviation Administration addressing certain Boeing Model MD-11 and MD-11F airplanes. It mandates a one-time inspection of the wire assemblies of the tail fuel tank transfer pumps to verify the installation of metallic transitions at wire harness breakouts, with required corrective actions if deficiencies are found. This directive aims to mitigate risks associated with potential ignition sources inside the tail fuel tank.

Feb 14, 2018
Airworthiness DirectiveMaintenanceSafety MgmtBoeing MD-11Boeing MD-11F

EASA SIB CE-18-11

M7 Aerospace LLC SA226 and SA227 Airplanes - Flight Controls / Elevator Control System

The Special Airworthiness Information Bulletin SAIB: CE-18-11 is an FAA informational bulletin addressing flight control concerns specifically related to the elevator control system on M7 Aerospace LLC Models SA226-AT/-TC/-T(B)/T and SA227-AC(C-26A)/-AT/-BC(C-26A)/-CC/-DC(C-26B)/-TT airplanes. It provides inspection procedures and maintenance recommendations for elevator quadrant bearings and bores to address corrosion issues. This bulletin is not a mandatory directive but serves to inform operators of potential airworthiness concerns.

Feb 14, 2018
Safety Information BulletinMaintenanceSafety Mgmt

EASA AD 2018-0042

SUPERSEDED BY EASA AD 2018-0248

EASA Airworthiness Directive 2018-0042 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus Helicopters AS 332 C, AS 332 C1, AS 332 L, AS 332 L1, and SA 330 J models. It mandates inspections of the tail rotor blade flapping hinges to detect damage that could lead to failure and loss of helicopter control. The directive applies to all manufacturer serial numbers of these helicopter models.

Feb 14, 2018
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 L1Airbus Helicopters SA 330 J

EASA AD 2018-0040

Reciprocating Engine — Valve Push Rod Assembly — Inspection / Replacement

EASA Airworthiness Directive 2018-0040 is an airworthiness directive addressing the inspection and replacement of valve push rod assemblies on SportStar RTC aeroplanes equipped with Rotax 912 ULS engines. It targets specific valve push-rod assemblies, rocker arms, and related parts that may have manufacturing defects leading to engine power loss. The directive mandates inspection and possible replacement of affected parts to ensure continued safe operation.

Feb 13, 2018
Airworthiness DirectiveMaintenanceSafety MgmtEvektor, Spol. S R.O. SportStar RTCSportStar RTC

EASA SIB 2018-05

Penny & Giles Aerospace Limited - Multi-Purpose Flight Recorders

EASA Safety Information Bulletin No. 2018-05 is an informational bulletin concerning Penny & Giles Aerospace Limited multi-purpose flight recorders (MPFRs) installed on helicopters. It addresses corrosion issues found on memory device pins in certain second generation "GEN2" memory modules manufactured between 06 April 2006 and 02 January 2013. The bulletin clarifies that this corrosion issue does not currently require mandatory airworthiness or operational directives.

Feb 8, 2018
Safety Information BulletinMaintenanceSafety Mgmt

EASA SIB SAFO18001

Textron (Beech) King Air 90-Series Airplanes - Boost Pump Failure and CROSSFEED

The Safety Alert for Operators SAFO 18001 provides important safety information regarding Textron (Beech) King Air 90-Series airplanes. It addresses the risk of dual engine failure caused by improper fuel management during BOOST PUMP failure and CROSSFEED valve operation. The document highlights operational considerations to prevent engine flameout related to fuel starvation and imbalance.

Feb 8, 2018
Safety Information BulletinFlight OpsSafety Mgmt

EASA AD 2018-0036

Fuselage / Stabilizers — Interfay Sealant in Hybrid Joints — Modification

EASA Airworthiness Directive 2018-0036 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A350-941 aeroplanes. It addresses the application of interfay sealant in hybrid joints on the fuselage and stabilizers to prevent corrosion and maintain structural integrity. The directive applies to all serial numbers except those with specific Airbus production modifications already embodied.

Feb 7, 2018
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A350Airbus A350-941

EASA AD 2018-0037

SUPERSEDED BY EASA AD 2019-0206

EASA Airworthiness Directive 2018-0037 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A350-941 aeroplanes. It mandates repetitive inspections of the trimmable horizontal stabilizer fittings and bearing assembly attachment interface to detect damage or corrosion. The directive aims to ensure continued airworthiness by preventing potential loss of attachment of the stabilizer to the fuselage.

Feb 7, 2018
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A350Airbus A350-941

EASA AD 2018-0023

[Correction] Doors — Main Landing Gear Fixed Fairing Assembly - Inspection

EASA Airworthiness Directive 2018-0023 is a corrective directive addressing inspection requirements for the main landing gear fixed fairing assembly on Airbus A318, A319, A320, and A321 aircraft. It applies to all manufacturer serial numbers of these models and focuses on preventing in-flight loss of the main landing gear fixed and hinged fairings due to fatigue cracking and corrosion. The directive mandates inspections, replacements, and modifications to ensure continued airworthiness and safety.

Feb 5, 2018
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2018-0033

SUPERSEDED BY ADR 2021-0109

The document titled SUPERSEDED BY ADR 2021-0109 is an explanatory statement issued by EASA regarding the absence of an Airworthiness Directive (AD) for the Airbus A400M aeroplane. Since there are currently no Airbus A400M aircraft in civil service, no public AD document exists. This record serves only as an informational advisory directed at military airworthiness authorities and design approval holders.

Feb 2, 2018
OtherSafety MgmtAirbus Military A400MAirbus A400M

EASA AD 2018-0032

Flight Controls — Air Brake Control Handle — Inspection / Modification

EASA Airworthiness Directive 2018-0032 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting DG Flugzeugbau GmbH LS 4-b sailplanes. It mandates inspection and modification of the air brake control handle to ensure the integrity of the air brake junction and rivets. The directive applies to all serial numbers of the LS 4-b sailplane model.

Feb 1, 2018
Airworthiness DirectiveMaintenanceSafety MgmtDg Aviation Gmbh LS4DG Flugzeugbau LS 4-b

EASA AD US-2018-02-08

Main Rotor - Blades - Cleaning / Inspection / Repair / Replacement

Federal Register Volume 83, Number 11 (January 17, 2018) is a final rule airworthiness directive (AD 2018-02-08) issued by the FAA for Bell Helicopter Textron Model 204B, 205A, and 205A-1 helicopters equipped with Helicopter Technology Company (HTC) main rotor blade part number 204P2100-101. The directive mandates cleaning, visual inspection, and depending on findings, repair or replacement of the main rotor blades to address fatigue cracks in the grip plate and doublers near the blade retention bolt hole. This AD aims to prevent potential blade failure and loss of helicopter control.

Feb 1, 2018
Airworthiness DirectiveMaintenanceSafety MgmtBell Textron Inc. (Bti) 204BBell Textron Inc. (Bti) 205Bell 204BBell 205ABell 205A-1