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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 2024-0045

Fuel — Fuel Filter — Inspection

EASA Airworthiness Directive 2024-0045 is an airworthiness directive affecting Airbus Helicopters AS 332 C, C1, L, L1, L2 and EC 225 LP models delivered before 15 February 2024. It mandates inspection of fuel filters, specifically part number 4020P25-5, for cracks on both outer and inner surfaces to prevent potential dual engine shutdowns. The directive updates previous inspection requirements to enhance safety related to fuel filter bowl cracking.

Feb 16, 2024
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 AS 332 L2Airbus Helicopters EC 225 LP

EASA AD 2024-0048

SUPERSEDED BY EASA AD 2024-0057

EASA Airworthiness Directive 2024-0048 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A321-251NX, A321-252NX, A321-253NX, A321-271NX, and A321-272NX aeroplanes. It addresses a potential unsafe condition related to the escape slide and offwing slide inflation reservoir venting holes, specifically concerning certain orifice fittings installed on these reservoirs. The directive mandates inspection and possible replacement of affected parts to ensure continued airworthiness.

Feb 16, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A321Airbus A321-251NXAirbus A321-252NXAirbus A321-253NXAirbus A321-271NXAirbus A321-272NX

EASA AD CF-2024-05

Engine — Second-Stage Power Turbine (PT2) Blade Failure

Canadian Airworthiness Directive CF-2024-05 is an emergency directive addressing second-stage power turbine (PT2) blade failures in Pratt & Whitney Canada PT6A and PT6E engine models. It applies to multiple PT6A-64 through PT6E-66XT variants equipped with suspect PT2 blades, part number 3056693-01. The directive mandates removal and replacement of affected blades to prevent potential engine power loss or in-flight shutdown.

Feb 15, 2024
Airworthiness DirectiveMaintenanceSafety MgmtPratt & Whitney Canada PT6A-67Pratt & Whitney Canada PT6A-68

EASA AD 2024-0044-E

Fire Protection — Engine Fire Extinguishing System — Inspection

EASA Airworthiness Directive 2024-0044-E is an emergency directive addressing the inspection of the engine fire extinguishing system on ATR 42 and ATR 72 aeroplanes. It specifically targets two-way valves with Part Number 446078 and certain serial numbers that may have incorrect marking and assembly. The directive mandates functional checks and corrective actions to ensure proper operation of the fire extinguishing system.

Feb 15, 2024
Airworthiness DirectiveMaintenanceSafety MgmtATR ATR42ATR ATR72ATR 42ATR 72

EASA AD 2024-0043

Wings — Outer Wing Stringers and Stringer Joint Pieces — Inspection

EASA Airworthiness Directive 2024-0043 is an airworthiness directive addressing inspection requirements for the outer wing stringers and stringer joint pieces on Fokker F28 Mark 0070 and Mark 0100 aeroplanes. It mandates a one-time special detailed inspection using high frequency eddy current techniques to detect cracks in specific wing areas. The directive applies to all serial numbers of these aircraft models with 34,000 or more flight cycles since entry into service.

Feb 15, 2024
Airworthiness DirectiveMaintenanceSafety MgmtFokker F28Fokker F28 Mark 0070Fokker F28 Mark 0100

EASA AD 2018-0140R1

Equipment & Furnishings - Hoist - Removal; Cabin Sliding Plug Doors / Emergency Jettisoning System - Rotorcraft Flight Manual Amendment / Placard Installation

EASA Airworthiness Directive 2018-0140R1 is an amendment addressing safety concerns on Airbus Helicopters AS 332 and EC 225 models. It focuses on the removal of the hoist arm and modifications related to the right-hand side lateral sliding plug door and its emergency jettisoning system. The directive applies to all serial numbers of the AS 332 C, C1, L, L1, L2, and EC 225 LP helicopters.

Feb 14, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SA 330Airbus Helicopters AS 332Airbus Helicopters EC 225

EASA AD US-2024-03-04

Flight Controls - Aft Rudder Quadrant - Inspection

Airworthiness Directive 2024-03-04 is a final rule issued by the Federal Aviation Administration (FAA) addressing certain Boeing 737-8, 737-8200, and 737-9 airplanes. It mandates a one-time inspection of the aft rudder quadrant due to a reported missing washer and nut and a migrated bolt, which could compromise rudder control. The directive aims to ensure continued safe flight by correcting this unsafe condition.

Feb 14, 2024
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 737Boeing 737-8Boeing 737-8200Boeing 737-9

EASA AD 2024-0042

SUPERSEDED BY EASA AD 2006-0005

EASA Airworthiness Directive 2024-0042 is issued for all SAAB SF340A and 340B aeroplanes. It mandates compliance with the updated Airworthiness Limitation Manual (ALM) Revision 2, which includes new and more restrictive maintenance tasks and life limits. This directive ensures continued airworthiness by updating maintenance requirements for these aircraft models.

Feb 13, 2024
Airworthiness DirectiveMaintenanceSafety MgmtSaab Ab 340SAAB SF340ASAAB SF340B

EASA AD 2024-0041

Time Limits / Maintenance Checks — Time Limits Manual / Maintenance Programme — Amendment

The document titled 'Time Limits / Maintenance Checks — Time Limits Manual / Maintenance Programme — Amendment' pertains to the Rolls-Royce Deutschland Ltd & Co KG Trent 7000 engine. It provides updated guidance and requirements related to the maintenance time limits and checks for this specific engine model. The amendment aims to ensure continued airworthiness and reliability of the Trent 7000 engine through revised maintenance protocols.

Feb 9, 2024
AMC/GMMaintenanceRolls-Royce Deutschland Ltd & Co Kg TRENT 7000

EASA AD 2024-0040-E

SUPERSEDED BY EASA AD 2024-0194

EASA Airworthiness Directive 2024-0040-E is an emergency directive addressing a potential unsafe condition in GE Aviation Czech M601 series engines installed on various aircraft including the LET L-410, Air Tractor AT series, Grumman G-164, and others. The directive mandates inspection of the centrifugal compressor case for cracks and restricts installation of affected parts. It applies to engines with specific part numbers M601-154.55 and M601-154.65 unless previously inspected and cleared.

Feb 8, 2024
Airworthiness DirectiveMaintenanceSafety MgmtGe Aviation Czech M601LET L-410Air Tractor AT seriesGrumman G-164

EASA AD 2024-0039

SUPERSEDED BY EASA AD 2025-0069

EASA Airworthiness Directive 2024-0039 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Rolls-Royce Deutschland Ltd & Co KG RB211 Trent 900 and Trent 970 series engines, commonly installed on Airbus A380 aircraft. This directive mandates compliance with updated airworthiness limitations and maintenance tasks as specified in the Rolls-Royce Trent 900 Time Limits Manual Revision 65 dated 01 October 2023. It ensures continued airworthiness by enforcing life limits and mandatory inspections for critical engine components.

Feb 8, 2024
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg RB211 TRENT 900Airbus A380

EASA AD US-2024-01-11

SUPERSEDED BY FAA AD 2024-20-04

FAA Airworthiness Directive 2024-01-11 is a final rule addressing an unsafe condition in certain Pacific Scientific Company rotary buckle assemblies installed on various helicopters. The affected buckles, part numbers 1111475 (all dash numbers) and 1111548-01, were manufactured between January 2012 and September 2012 and contain screws susceptible to hydrogen embrittlement, risking buckle failure during occupant restraint. This directive applies specifically to helicopters and requires inspection and possible replacement of the buckles or screws to ensure safety.

Feb 8, 2024
Airworthiness DirectiveMaintenanceSafety Mgmt

EASA AD US-2024-01-04

Engine Exhaust - Inner Fixed Structure and Thrust Reverser - Inspection / Replacement

Airworthiness Directive 2024-01-04 is a final rule issued by the Federal Aviation Administration addressing Boeing 787-8, 787-9, and 787-10 airplanes powered by Rolls-Royce Trent 1000 engines. It focuses on inspections and replacement of the inner fixed structure forward upper fire seal and thermal insulation blankets in the thrust reverser area to prevent damage and potential fire hazards. This directive mandates inspection and replacement of specific upper splitter fairing assemblies to enhance engine fire safety.

Feb 7, 2024
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 787Boeing 787-8Boeing 787-9Boeing 787-10

EASA SIB 2024-03R1

Incorrect Processing of the Integrity Information Message by Collins Aerospace Satellite Based Augmentation Systems Receivers

EASA Safety Information Bulletin 2024-03R1 addresses an issue with Collins Aerospace Satellite Based Augmentation Systems receivers models GPS-4000S, GLU-2100, GLUS-2100, and GLUS-2100A. The bulletin highlights incorrect processing of the integrity information message (Message Type 6) under certain conditions, potentially affecting the notification of compromised GNSS position integrity. This issue was exposed following an update to the EGNOS ground system in November 2023 and applies to specific hardware and software part numbers listed in the bulletin.

Feb 7, 2024
Safety Information BulletinSafety MgmtMaintenance

EASA AD 2024-0037R1

Engine — Main Bearing / Studs — Replacement

The document titled 'Engine — Main Bearing / Studs — Replacement' issued by AUSTRO ENGINE GMBH for the E4 engine model addresses the replacement requirements for main bearing studs. It provides guidance and regulatory instructions for maintaining engine integrity and safety. This document is relevant to operators and maintenance organizations working with the AUSTRO ENGINE GMBH E4 engine.

Feb 6, 2024
OtherMaintenanceSafety MgmtAustro Engine Gmbh E4

EASA AD US-2024-01-01

SUPERSEDED BY FAA AD 2026-02-10

FAA Airworthiness Directive 2024-01-01 is a final rule addressing certain Boeing Model 787-8, 787-9, and 787-10 airplanes. It mandates repetitive visual inspections under all lavatory washbasins to detect intermittent and active water leaks from the faucet control module (FCM), which could migrate below the passenger floor and into electronic equipment bays. The directive aims to prevent damage to flight-critical equipment caused by these leaks.

Feb 6, 2024
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 787Boeing 787-8Boeing 787-9Boeing 787-10

EASA AD US-2024-01-06

Fuselage - Skin Repairs at Stringer S—17 - Repetitive Inspections

Federal Aviation Administration Airworthiness Directive 2024-01-06 is a final rule addressing certain Boeing 737-600, 737-700, and 737-800 series airplanes. It mandates repetitive inspections of fuselage skin repairs at Stringer S-17 to detect cracks and requires corrective actions if necessary. This directive aims to ensure continued airworthiness by preventing fatigue cracking that could compromise structural integrity.

Feb 5, 2024
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 737Boeing 737-600Boeing 737-700Boeing 737-800

EASA AD BR-2024-02-01

Kidde Aerospace & Defense - Overheat Detection System Sensing Elements - Inspection / Replacement

Brazilian Airworthiness Directive AD No. 2024-02-01 issued by the Agência Nacional de Aviação Civil (ANAC) mandates inspection and possible replacement of Kidde Aerospace & Defense Overheat Detection System (ODS) sensing elements on Embraer S.A. ERJ 190-300 and ERJ 190-400 aircraft. The directive addresses potential failures in ODS sensing elements produced before January 31, 2021, which could lead to undetected thermal bleed leaks and pose fire risks. It requires operators to inspect specific bleed lines and wing anti-ice and bleed system sensing elements to ensure flight safety.

Feb 5, 2024
Airworthiness DirectiveMaintenanceSafety MgmtEmbraer ERJ 190Embraer ERJ 190-300Embraer ERJ 190-400

EASA AD 2024-0038

SUPERSEDED BY EASA AD 2025-0068

EASA Airworthiness Directive 2024-0038 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes. It addresses inspection and modification requirements for forward-facing galley parts with specific part numbers to prevent damage that could lead to trolley detachment during emergency landings. This directive applies to all manufacturer serial numbers of the listed aircraft models.

Feb 5, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2024-0031

SUPERSEDED BY EASA AD 2025-0030

EASA Airworthiness Directive 2024-0031 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes. It mandates compliance with updated Damage Tolerance Airworthiness Limitations Items specified in the Airbus Airworthiness Limitations Section Part 2 Revision 10. This directive ensures continued airworthiness by requiring operators to follow new and/or more restrictive maintenance tasks.

Feb 1, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321