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EASA Regulations & Airworthiness Directives

Browse 4771 EASA regulations with AI-powered summaries.

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EASA AD 2019-0217

SUPERSEDED BY EASA AD 2022-0105

EASA Airworthiness Directive 2019-0217 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 compliance with the updated Airbus A380 Airworthiness Limitations Section (ALS) Part 1, Revision 11, which includes safe life airworthiness limitation items and maintenance tasks. This directive ensures continued airworthiness by enforcing replacement of components before exceeding life limits and updating maintenance programs accordingly.

Sep 2, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380Airbus A380-841Airbus A380-842Airbus A380-861

EASA AD DCA-750XL-38A

Flap Assembly Screw Jack — Inspection

The Airworthiness Directive DCA/750XL/38A Flap Assembly Screw Jack – Inspection issued by the Civil Aviation Authority of New Zealand mandates inspection of flap screw jack assemblies on Pacific Aerospace Limited 750XL aircraft, specifically serial numbers 101 through 215, 220, 8001, and 8002, as well as spare parts with part numbers 11-45621-1 and 11-45622-1. This directive addresses potential incorrect assembly of the flap screw jack bearing retainer and stop, which could lead to fatigue failure. Compliance with the inspection and corrective actions outlined in Pacific Aerospace Mandatory Service Bulletin PACSB/XL/117 issue 2 is required.

Aug 30, 2019
Airworthiness DirectiveMaintenanceSafety MgmtNzskydive 750XLPacific Aerospace 750XL

EASA AD DCA-750XL-39

Fuel Condition Lever — Inspection

Airworthiness Directive DCA/750XL/39 is issued by the Civil Aviation Authority of New Zealand and applies to Pacific Aerospace Limited 750XL aircraft with serial numbers 101 through 216, 220, 8001, and 8002. This directive mandates inspection and adjustment of the fuel condition lever to prevent inadvertent movement into the cut-off position when ground idle is selected. The directive references Pacific Aerospace Mandatory Service Bulletin PACSB/XL/111 issue 1 dated 18 June 2019 for detailed instructions.

Aug 30, 2019
Airworthiness DirectiveMaintenanceSafety MgmtNzskydive 750XLPacific Aerospace 750XL

EASA AD 2019-0214

Wings — Trailing Edge Flap Track #2 and #5 Supports — Modification

EASA Airworthiness Directive 2019-0214 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 trailing edge flap track #2 and #5 supports on both left-hand and right-hand wings. The directive mandates modifications to these flap track supports to ensure continued airworthiness and safe operation of the affected aircraft.

Aug 30, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380Airbus A380-841Airbus A380-842Airbus A380-861

EASA AD US-2019-14-12

Flight Controls - Main Slat Track Assemblies - Inspection

Federal Aviation Administration Airworthiness Directive 2019-14-12 is a final rule addressing certain Boeing 737-8 and 737-9 airplanes. It mandates inspection and maintenance record checks of main slat track assemblies due to concerns about hydrogen embrittlement affecting their structural integrity. This directive aims to prevent potential slat failure that could jeopardize flight safety.

Aug 29, 2019
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 737Boeing 737-8Boeing 737-9

EASA AD 2019-0213

Hydraulic Power - Hydraulic Pumps - Inspection / Replacement

EASA Airworthiness Directive 2019-0213 is an official regulatory document addressing hydraulic pumps installed on Leonardo S.p.A. AW109SP helicopters. It mandates inspection and replacement of specific hydraulic pumps with Part Number 109-0760-42-103, which are not eligible for installation, to ensure continued airworthiness and safety of the helicopters.

Aug 29, 2019
Airworthiness DirectiveMaintenanceSafety MgmtLeonardo S.P.A. Helicopters A109Leonardo S.P.A. Helicopters A119Leonardo AW109SP

EASA AD 2019-0200R1

SUPERSEDED BY EASA AD 2023-0058

EASA Airworthiness Directive 2019-0200R1 is an amendment addressing the airworthiness limitations for Dassault Mystère-Falcon 20-( )5 series aeroplanes. It mandates compliance with updated maintenance tasks and life limits as specified in the Dassault Mystère-Falcon 20 Aircraft Maintenance Manual Chapter 5-40, Revision 13. This directive excludes aircraft that have incorporated the Dassault Mystère-Falcon 20 Supplemental Structural Inspection Program into their maintenance programs.

Aug 29, 2019
Airworthiness DirectiveMaintenanceSafety MgmtDassault Mystère-Falcon 20Dassault Mystère-Falcon 20-( )5

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