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EASA Regulations & Airworthiness Directives

Browse 4995 EASA regulations with AI-powered summaries.

Aircraft:AllAirbus A320280Airbus A321276Airbus A319246Airbus A350214Airbus A330210All194Airbus A318185Airbus A380171Boeing 737170Airbus A340140Airbus A350-941125Airbus BD-500 (A220 Series)116Airbus Helicopters AS 332116Airbus Helicopters EC 225113Airbus Helicopters SA 330113Show all...

EASA AD US-2019-16-15

Engine - High-Pressure Compressor Front Hub - Revision of the Airworthiness Limitations Section and the Continued Airworthiness Maintenance Programs

The document titled "Engine - High-Pressure Compressor Front Hub - Revision of the Airworthiness Limitations Section and the Continued Airworthiness Maintenance Programs" is a final rule airworthiness directive issued by the FAA affecting Pratt & Whitney PW1519G, PW1521G, PW1521GA, PW1524G, PW1525G, PW1521G-3, PW1524G-3, PW1525G-3, PW1919G, PW1921G, PW1922G, PW1923G, and PW1923G-A model turbofan engines. It addresses corrosion issues found on the high-pressure compressor front hub that could lead to premature cracking. The directive mandates revisions to the Airworthiness Limitations Section and continued airworthiness maintenance programs to incorporate new or more restrictive life limits for the HPC front hub.

Aug 28, 2019
Airworthiness DirectiveMaintenanceSafety MgmtPratt & Whitney PW1500GPratt & Whitney PW1900G

EASA AD US-2019-13-05

Fuselage - Main Transmission Forward and Aft Frame Assemblies and Adjacent Skins - Inspections

Federal Aviation Administration Airworthiness Directive 2019-13-05 is a final rule addressing certain Sikorsky Aircraft Corporation Model S-92A helicopters. It mandates inspections of the main transmission forward and aft frame assemblies and adjacent skins for cracks and loose fasteners, and establishes life limits for specific frame assemblies to ensure continued airworthiness.

Aug 28, 2019
Airworthiness DirectiveMaintenanceSafety MgmtSikorsky S-92Sikorsky S-92A

EASA AD US-2019-14-15

Fuselage - Stub Beams - Inspection

Airworthiness Directive 2019-14-15 issued by the Federal Aviation Administration (FAA) addresses inspection requirements for the stub beams of the fuselage on all Boeing 737-100, -200, -200C, -300, -400, and -500 series airplanes. This directive mandates repetitive inspections for cracking in the webs and chords of the stub beams at specified fuselage stations, including new inspection locations, and requires applicable on-condition corrective actions to maintain airworthiness.

Aug 28, 2019
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 737Boeing 737-100Boeing 737-200Boeing 737-200CBoeing 737-300Boeing 737-400Boeing 737-500

EASA SIB 2019-11

SAAB SF340A and SAAB 340B Aeroplanes - Fuel Tank Conduits Wiring Protection — Heat Shrinkable Tubes

EASA Safety Information Bulletin 2019-11 is an airworthiness bulletin addressing fuel tank conduits wiring protection on SAAB SF340A and SAAB 340B aeroplanes. It focuses on the use of heat shrinkable tubes for wiring protection as specified in SAAB Service Bulletin 340-28-026. The bulletin highlights compliance issues related to the qualification standards of the heat shrinkable tubes installed on these aircraft.

Aug 28, 2019
Safety Information BulletinMaintenanceSafety Mgmt

EASA AD 2019-0211

Engine — Thermostatic Oil Cooler Bypass Valve — Inspection / Installation

EASA Airworthiness Directive 2019-0211 is an airworthiness directive addressing certain CEAPR DR 400 aeroplanes equipped with Lycoming engines. It mandates inspection and possible installation of a thermostatic oil cooler bypass valve on affected aircraft models including DR 400/100 through DR 400/200 I with serial numbers 2654 to 2721. The directive aims to ensure engine cooling system integrity to prevent overheating.

Aug 27, 2019
Airworthiness DirectiveMaintenanceSafety MgmtCeapr DR 400

EASA AD 2019-0212

Fuel — Motorised Fuel Valve — Inspection

EASA Airworthiness Directive 2019-0212 is an airworthiness directive addressing inspection requirements for motorised fuel valves Part Number 7923227F installed on Airbus Defence and Space CN-235 and C-295 aeroplanes. The directive mandates repetitive inspections and operational checks to detect fuel leakage and prevent potential fuel system malfunction or fire hazards. It applies to all manufacturer serial numbers of the affected aircraft models.

Aug 27, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Defence & Space C-295Airbus Defence & Space CN-235Airbus Defence and Space CN-235Airbus Defence and Space C-295

EASA AD US-2019-14-02

Hydraulic Power - Pressure Module Check Valves - Inspection

Federal Register Volume 84, Number 141 (Tuesday, July 23, 2019) - Airworthiness Directive 2019-14-02 is a final rule issued by the Federal Aviation Administration (FAA) addressing all Boeing Company Model 737 series airplanes. This directive requires inspection of the hydraulic power pressure module check valves, specifically targeting certain aluminum check valves prone to structural fatigue cracks. The affected parts include Parker pressure module check valves, part number H61C0552M1.

Aug 26, 2019
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 737

EASA AD 2019-0210

SUPERSEDED BY EASA AD 2024-0220

EASA Airworthiness Directive 2019-0210 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A350-941 and A350-1041 aeroplanes. It mandates inspection of cabin oxygen containers and adjacent panel fasteners to ensure proper installation and prevent oxygen mask deployment failure. The directive applies to specific manufacturer serial numbers as listed in Airbus Alert Operators Transmission A35P015-19.

Aug 26, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A350Airbus A350-941Airbus A350-1041

EASA AD 2019-0209

Power Plant — Control and Monitoring Harness — Identification / Replacement

EASA Airworthiness Directive 2019-0209 addresses an unsafe condition in SAFRAN HELICOPTER ENGINES MAKILA 1A and 1A1 turboshaft engines, commonly installed on Airbus Helicopters AS 332 C, C1, L, and L1 models. The directive mandates identification and replacement of certain control and monitoring harnesses that were found to be incorrectly manufactured, potentially causing in-flight activation of the "85% NG" backup law. This AD ensures continued airworthiness by requiring corrective actions on affected parts.

Aug 23, 2019
Airworthiness DirectiveMaintenanceSafety MgmtSafran MAKILA 1Airbus Helicopters AS 332 CAirbus Helicopters AS 332 C1Airbus Helicopters AS 332 LAirbus Helicopters AS 332 L1

EASA AD 2019-0208

Integrated Modular Avionics — Aircraft Management Computer Software — Update

EASA Airworthiness Directive 2019-0208 is an update concerning the Aircraft Management Computer software for Airbus Helicopters Deutschland GmbH MBB-BK117 D-2 helicopters. It addresses a software issue in the Integrated Modular Avionics system that caused erroneous low rotor RPM indications during One Engine Inoperative conditions. This directive applies to all serial numbers of the MBB-BK117 D-2 helicopter model.

Aug 22, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters MBB-BK 117Airbus Helicopters MBB-BK117 D-2

EASA AD 2008-0221-CN

CANCELLED: Time Limits / Maintenance Checks — Airworthiness Limitations Section Chapter 5-40 — Amendment

EASA Airworthiness Directive 2008-0221-CN is a cancellation notice issued by the European Union Aviation Safety Agency affecting various Dassault Aviation aircraft models including Falcon 10, Fan Jet Falcon, Mystère-Falcon 20GF, Mystère-Falcon 20-( )5 series, Mystère-Falcon 200, Mystère-Falcon 50, Mystère-Falcon 900, Falcon 900EX, Falcon 2000, Falcon 2000EX, and Falcon 7X. This document cancels the previous AD 2008-0221 related to time limits and maintenance checks in the Airworthiness Limitations Section Chapter 5-40. It confirms that the requirements have been superseded by more recent ADs specific to each aircraft type.

Aug 20, 2019
Airworthiness DirectiveMaintenanceSafety MgmtDassault Falcon 10Dassault Falcon 2000Dassault Falcon 7XDassault Falcon 900EXDassault Fan Jet FalconDassault Mystère-Falcon 20Dassault Mystère-Falcon 20GFDassault 200Dassault Mystère-Falcon 50Dassault Mystère-Falcon 900Dassault Mystère-Falcon 20GFDassault Mystère-Falcon 20-( )5 seriesDassault Mystère-Falcon 200Dassault Mystère-Falcon 50Dassault Mystère-Falcon 900Dassault Falcon 2000EX

EASA AD US-2019-15-06

Engine - High Pressure Compressor Stages 2-5 Spool - Inspection

Airworthiness Directive 2019-15-06 is a final rule issued by the Federal Aviation Administration (FAA) addressing Engine Alliance GP7270, GP7272, and GP7277 model turbofan engines. It mandates inspections of the high-pressure compressor (HPC) stages 2-5 spool for cracks and the stage 6 seal ring for correct installation to prevent unsafe conditions. The directive includes repetitive inspections and a mandatory terminating in-shop inspection to ensure continued airworthiness.

Aug 20, 2019
Airworthiness DirectiveMaintenanceSafety MgmtEngine Alliance GP7200

EASA AD 2019-0204

Engine — Propeller Gear Box — Input Pinion Plug — Inspection

The document titled Engine — Propeller Gear Box — Input Pinion Plug — Inspection is an informational Airworthiness Directive record issued by EASA concerning the Europrop International GmbH TP400-D6 engine. It clarifies that no civil aircraft currently operate this engine model, so no public AD exists. The document serves as a recommendation for military authorities responsible for aircraft equipped with TP400-D6 engines to issue their own applicable ADs.

Aug 20, 2019
Airworthiness DirectiveMaintenanceSafety MgmtEpi Europrop International Gmbh TP400-D6

EASA AD US-2019-16-01

Engine - Turbine Exhaust Case - Inspection

The Federal Aviation Administration's Airworthiness Directive 2019-16-01 addresses all International Aero Engines AG V2525-D5 and V2528-D5 turbofan engines. This directive mandates inspections of turbine exhaust cases due to reports of cracks, aiming to prevent engine failure and potential loss of the airplane. It requires initial and repetitive inspections and replacement of affected parts if cracks are found.

Aug 20, 2019
Airworthiness DirectiveMaintenanceSafety MgmtInternational Aero Engines Ag V2500-( )5

EASA AD 2019-0205

SUPERSEDED BY EASA AD 2019-0251

EASA Airworthiness Directive 2019-0205 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A380-841, A380-842, and A380-861 aeroplanes. It addresses the engine bleed air system, specifically the Certification Maintenance Requirements task related to the pneumatic system. The directive mandates inspections and functional tests to ensure continued airworthiness of the affected aircraft.

Aug 20, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380Airbus A380-841Airbus A380-842Airbus A380-861

EASA AD 2019-0206

SUPERSEDED BY EASA AD 2021-0141

EASA Airworthiness Directive 2019-0206 is an airworthiness directive issued for Airbus A350-941 and A350-1041 aeroplanes, excluding those with certain production modifications. It addresses inspection and maintenance requirements for the trimmable horizontal stabilizer fittings and bearing assembly attachment interface to prevent potential corrosion and structural issues.

Aug 20, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A350Airbus A350-941Airbus A350-1041

EASA AD 2019-0201

SUPERSEDED BY EASA AD 2023-0062

EASA Airworthiness Directive 2023-0062 is an airworthiness directive concerning the Dassault Aviation Mystère-Falcon 20 aircraft. This directive replaces previous regulatory requirements to ensure continued safety and compliance for the specified aircraft type. It addresses necessary inspections, modifications, or operational limitations to maintain airworthiness standards.

Aug 20, 2019
Airworthiness DirectiveMaintenanceSafety MgmtDassault Mystère-Falcon 20Dassault Aviation Mystère-Falcon 20

EASA AD US-2019-16-04

SUPERSEDED BY FAA AD 2019-18-08

FAA Airworthiness Directive 2019-16-04 is a final rule affecting Engine Alliance GP7270 and GP7277 model turbofan engines equipped with a specific engine fan hub assembly. It mandates inspections and possible replacement of the engine fan hub blade lock assembly to address potential uncontained failures. This directive updates previous requirements to enhance safety measures for these engine models.

Aug 20, 2019
Airworthiness DirectiveMaintenanceSafety MgmtEngine Alliance GP7200

EASA AD US-2019-14-13

SUPERSEDED BY FAA AD 2025-01-06

FAA Airworthiness Directive 2019-14-13 is a final rule affecting all Boeing 767-200, -300, -300F, and -400ER series airplanes. It addresses uncommanded fore/aft movements of the Captain's and First Officer's seats by requiring identification of seat part and serial numbers, detailed inspections, repetitive checks of the horizontal movement system, and applicable corrective actions. An optional terminating action is provided for certain airplanes to end repetitive checks.

Aug 20, 2019
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 767Boeing 767-200Boeing 767-300Boeing 767-300FBoeing 767-400ER