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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 2017-0092R1

Propellers — Removal from Service / Modification

The document titled 'Propellers — Removal from Service / Modification' with type designation DUC, SOCIETE:FLAIR-2 addresses the removal from service and modification procedures for specific propeller components. Although specific aircraft types or engine models are not detailed due to content extraction failure, the document focuses on ensuring continued airworthiness through proper handling of propeller parts.

Duc, Societe FLAIR-2

EASA AD US-2018-09-04

[Correction] Landing Gear - Main Landing Gear Actuator Attachment Fitting - Inspection / Maintenance Program Revision

Correction to Airworthiness Directive 2018-09-04 issued by the Federal Aviation Administration (FAA) affecting Gulfstream Aerospace Corporation Model G-IV and GIV-X airplanes. The correction addresses a typographical error in the referenced Customer Bulletin number related to the inspection and maintenance program for the main landing gear actuator attachment fitting. The directive mandates inspection cycles and maintenance program revisions to prevent fatigue cracks in the main landing gear actuator attachment fitting.

Airworthiness Directive

Gulfstream Aerospace Corporation GIVX
Gulfstream Aerospace Corporation G-IV

EASA AD 2018-0118R1

Doors – Auxiliary Wing Landing Gear Doors – Inspection

EASA Airworthiness Directive 2018-0118R1 is an updated safety directive addressing inspection and maintenance requirements for the auxiliary wing landing gear doors on Airbus A380-841, A380-842, and A380-861 aircraft. It mandates repetitive inspections of specific hinge fittings prone to fatigue cracking and outlines corrective actions to maintain structural integrity. This directive applies to all manufacturer serial numbers of the affected Airbus A380 models.

Airworthiness DirectiveSuperseded

Airbus A380

EASA AD 2018-0127

Fuel Hoses — Inspection / Replacement / Life Limit

EASA Airworthiness Directive 2018-0127 is an airworthiness directive addressing fuel hoses on DG-Flugzeugbau GmbH powered sailplanes, specifically the DG-808C, DG-1000T, LS8-t, LS9, and LS10-st models. It mandates inspections, replacements, and life limits for polyurethane fuel hoses installed in the airframe fuel system and engine compartment to ensure continued airworthiness and safety.

Airworthiness Directive

Dg Aviation Gmbh DG-1000
Dg Aviation Gmbh DG-800
Dg Aviation Gmbh LS10
Dg Aviation Gmbh LS8
Dg Aviation Gmbh LS9
DG-Flugzeugbau DG-808C
DG-Flugzeugbau DG-1000T
DG-Flugzeugbau LS8-t
DG-Flugzeugbau LS9
DG-Flugzeugbau LS10-st

EASA AD US-2018-10-07

Superseded by FAA AD 2019-19-12

FAA Airworthiness Directive 2018-10-07 is a final rule addressing Sikorsky Aircraft Corporation Model S-76C helicopters equipped with Turbomeca Arriel 2S1 or 2S2 engines having engine collective position transducer (CPT) part number 76900-01821-104 installed. This directive requires inspections of the CPT to detect wear that has caused several momentary One Engine Inoperative (OEI) incidents. The AD aims to prevent unsafe conditions related to CPT wear that could lead to emergency landings.

Airworthiness Directive

Sikorsky S-76
Sikorsky S-76C

EASA AD 2018-0117R1

Exhaust — Inner J-Ring and V-Groove Interface — Inspection

EASA Airworthiness Directive 2018-0117R1 is an amendment addressing inspection requirements for the inner J-ring and V-groove interface on Airbus A380-861 aeroplanes powered by GP7200 engines. It mandates repetitive detailed inspections of the inner J-ring to detect wear damage that could compromise the structural integrity of the engine thrust reverser unit and fan exhaust cowl. The directive applies to all manufacturer serial numbers of the Airbus A380-861 and references Airbus Service Bulletin A380-78-8012 for inspection procedures.

Airworthiness Directive

Airbus A380

EASA AD US-2018-10-12

Wings - Fuselage Keel Beam Upper Chords / Aft Vertical Stiffeners - Inspection

Airworthiness Directive 2018-10-12 is a final rule issued by the Federal Aviation Administration addressing all Boeing Company Model 737-100, -200, -200C, -300, -400, and -500 series airplanes. It mandates repetitive high frequency eddy current and detailed inspections for cracking in aft vertical stiffeners and keel beam upper chords, along with applicable on-condition corrective actions. This directive aims to ensure structural integrity by detecting and mitigating fatigue cracks in critical wing fuselage components.

Airworthiness Directive

Boeing 737100200200C300400500

EASA AD 2018-0125

Engine — Turbocharger Waste Gate Controller and Control Rod Circlip — Life Limit / Modification

EASA Airworthiness Directive 2018-0125 addresses the turbocharger waste gate controller and control rod circlip life limits and modifications for Austro Engine GmbH E4 and E4P engines. These engines are commonly installed on Diamond Aircraft Industries models DA 40 NG, DA 42 NG, DA 42 M-NG, and DA 62. The directive mandates modifications to prevent failures that could lead to engine power loss and reduced aircraft control.

Airworthiness Directive

Austro Engine Gmbh E4
Diamond Aircraft Industries DA 40 NG
Diamond Aircraft Industries DA 42 NG
Diamond Aircraft Industries DA 42 M-NG
Diamond Aircraft Industries DA 62

EASA AD 2018-0124

Aircraft Flight Manual - Amendment

EASA Airworthiness Directive 2018-0124 is an amendment addressing safety concerns for Leonardo S.p.A. A119 and AW119MKII helicopters equipped with certain Pratt & Whitney Canada PT6B engine Fuel Control Units (FCU). The directive mandates updates to the Aircraft Flight Manual and installation of cockpit placards to prohibit intentional autorotation for helicopters with affected FCUs.

Airworthiness Directive

Leonardo S.P.A. Helicopters A109
Leonardo S.P.A. Helicopters A119
Leonardo A119
Leonardo AW119MKII

EASA AD 2018-0123

Fuselage — Tail Cone Balancer Fitting Anchor Nuts and Fasteners — Modification

EASA Airworthiness Directive 2018-0123 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 tail cone balancer fitting anchor nuts and fasteners on these aircraft. The directive mandates a modification to improve corrosion resistance on specific parts of the tail cone structure.

Airworthiness Directive

Airbus A350941

EASA AD 2018-0112R1

Main Rotor — Main Rotor Damper — Inspection / Replacement

The document titled 'Main Rotor — Main Rotor Damper — Inspection / Replacement' applies to LEONARDO S.p.A. HELICOPTERS models AB139 and AW139. It provides instructions for inspecting and replacing the main rotor damper to ensure continued airworthiness and safe operation of these helicopter models. The directive focuses on maintaining the integrity of the main rotor system components.

Airworthiness Directive

Leonardo S.P.A. Helicopters AB139
Leonardo S.P.A. Helicopters AW139

EASA AD 2018-0122

Placards and Markings — Auxiliary Power Unit Air Intake — Introduction

EASA Airworthiness Directive 2018-0122 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Fokker F28 Mark 0070 and Mark 0100 aeroplanes. It addresses safety concerns related to the auxiliary power unit (APU) air intake, specifically to prevent uncontained APU turbine rotor rim failures during de-/anti-icing operations. The directive mandates installation of specific placards and markings near the APU air intake to warn ground personnel.

Airworthiness Directive

Fokker F28
Fokker F28 Mark 0070
Fokker F28 Mark 0100

EASA AD 2018-0030R1

Wings — Wing Front Attachments — Inspection / Modification / Replacement

EASA Airworthiness Directive 2018-0030R1 addresses inspection, modification, and replacement requirements for wing front attachments on SOCATA TB 9, TB 10, and TB 200 aeroplanes. It mandates repetitive inspections and reinforcement of wing front attachments on both wing and fuselage sides to ensure structural integrity. The directive applies to all manufacturer serial numbers of these aircraft models.

Airworthiness Directive

Daher Aerospace TB
SOCATA TB 9
SOCATA TB 10
SOCATA TB 200

EASA AD 2018-0121

Engine — Low Pressure Turbine Blades — Replacement

EASA Airworthiness Directive 2018-0121 is an official directive addressing the replacement of low pressure turbine blades on Rolls-Royce RB211 Trent 970-84, 972-84, and 972E-84 engines, commonly installed on Airbus A380 aircraft. The directive mandates inspection and replacement of affected turbine blades that were subject to cleaning with OMat 198 during overhaul. This AD aims to prevent engine failures caused by internal corrosion leading to uncommanded in-flight engine shutdowns.

Airworthiness Directive

Rolls-Royce Deutschland Ltd & Co Kg RB211 TRENT 900
Airbus A380

EASA AD 2018-0111R1

Water/Waste — Forward Fuselage Shrouded Pipe T-Boxes and Clamps — Replacement

EASA Airworthiness Directive 2018-0111R1 is an updated regulatory requirement addressing the replacement of potable water shrouded pipe T-Boxes and clamps on Airbus A350-941 aeroplanes. This directive applies to all serial numbers except those with Airbus modifications 111435 or 111440 incorporated during production. It mandates corrective action to prevent water ingress into the avionics bay caused by cracks and clamp torque loss.

Airworthiness Directive

Airbus A350941

EASA AD GA8-9-Amdt1

Wing Strut and Wing Strut Fittings - Inspection and Replacement

The Commonwealth of Australia Civil Aviation Safety Authority Airworthiness Directive AD/GA8/9 Amendment 1 addresses inspection and replacement requirements for wing struts and wing strut fittings on all GippsAero GA8 and GA8-TC 320 aeroplanes. It mandates inspections of specific GippsAero part numbers for cracks, corrosion, and damage, and requires replacement of affected parts based on serial numbers identified in GippsAero Service Bulletin SB-GA8-2017-174 Issue 2. The directive aims to ensure continued airworthiness and safety of these aircraft components.

Airworthiness Directive

Ga8 Airvan Pty Ltd (Gippsaero) GA8
GippsAero GA8TC 320

EASA AD 2018-0120-E

Fuselage – Baggage Fairings – Modification

EASA Airworthiness Directive 2018-0120-E is an emergency directive affecting Leonardo S.p.A. A109S and AW109SP helicopters. It addresses a safety issue related to wire chafing that could cause fire and smoke in the baggage compartment, posing a risk of loss of control. The directive mandates modifications to the baggage fairing assembly and temporary operational restrictions until the modification is completed.

Airworthiness DirectiveSuperseded

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

EASA AD 2018-0116

Stabilizers – Inboard and Outboard Elevator Hinges / Actuator Fittings – Inspection

EASA Airworthiness Directive 2018-0116 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all Airbus A380-841, A380-842, and A380-861 aeroplanes. It mandates inspections of the inboard and outboard elevator hinges and actuator fittings to detect bushing migration and other potential structural issues. The directive aims to ensure the continued structural integrity and safe control of the aircraft elevators.

Airworthiness DirectiveSuperseded

Airbus A380841842861

EASA AD 2018-0119

Wings — Outboard Flaps Skin — Inspection

EASA Airworthiness Directive 2018-0119 is an airworthiness directive issued by EASA concerning Airbus A380-841, A380-842, and A380-861 aeroplanes. It mandates inspection of the outboard flaps skin, specifically the upper and lower skin surfaces between certain ribs on both left-hand and right-hand outer flaps. The directive addresses potential structural issues related to incorrect repair zoning in the aircraft's Structural Repair Manual.

Airworthiness Directive

Airbus A380

EASA AD US-2018-11-05

Superseded by FAA AD 2018-21-13

FAA Airworthiness Directive 2018-11-05 is a final rule superseding AD 2018-06-10 and applies to certain Honda Aircraft Company LLC Model HA-420 airplanes. It addresses an unsafe condition related to faulty power brake valves that can cause degraded braking performance and reduced directional control during ground operations and landing deceleration. This AD corrects a typographical error in the serial number applicability from the previous AD and retains the required actions including inserting a temporary revision into the airplane flight manual and replacing defective power brake valves.

Airworthiness Directive

Honda Aircraft Company HA-420