EASA Regulations & Airworthiness Directives

Browse 5,166 EASA regulations with AI-powered summaries.

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EASA AD 2019-0208

Aug 22, 2019

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.

Airworthiness Directive
  • Airbus Helicopters MBB-BK 117
  • Airbus Helicopters MBB-BK117 D-2

EASA AD 2008-0221-CN

Aug 20, 2019

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 It confirms that the requirements have been superseded by more recent ADs specific to each aircraft type.

Airworthiness Directive
  • Dassault Falcon 10
  • Dassault Falcon 2000
  • Dassault Falcon 7X
  • Dassault Falcon 900EX
  • Dassault Fan Jet Falcon
  • Dassault Mystère-Falcon 20
  • Dassault Mystère-Falcon 20GF
  • Dassault 200
  • Dassault Mystère-Falcon 50
  • Dassault Mystère-Falcon 900
  • Dassault Mystère-Falcon 20GF
  • Dassault Mystère-Falcon 20-( )5 series
  • Dassault Mystère-Falcon 200
  • Dassault Mystère-Falcon 50
  • Dassault Mystère-Falcon 900
  • Dassault Falcon 2000EX

EASA AD US-2019-15-06

Aug 20, 2019

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.

Airworthiness Directive
  • Engine Alliance GP7200

EASA AD 2019-0204

Aug 20, 2019

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.

Airworthiness Directive
  • Epi Europrop International Gmbh TP400-D6

EASA AD US-2019-16-01

Aug 20, 2019

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.

Airworthiness Directive
  • International Aero Engines Ag V2500-( )5

EASA AD 2019-0206

Aug 20, 2019

Fuselage – Trimmable Horizontal Stabilizer Fittings and Bearing Assembly Attachment Interface – Inspection

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.

Airworthiness DirectiveSuperseded
  • Airbus A3509411041

EASA AD 2019-0205

Aug 20, 2019

Pneumatic – Engine Bleed Air System Certification Maintenance Requirements Task – Amendment

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.

Airworthiness DirectiveSuperseded
  • Airbus A380841842861

EASA AD 2019-0201

Aug 20, 2019

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.

Airworthiness DirectiveSuperseded
  • Dassault Mystère-Falcon 20
  • Dassault Aviation Mystère-Falcon 20

EASA AD US-2019-16-04

Aug 20, 2019

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.

Airworthiness Directive
  • Engine Alliance GP7200

EASA AD US-2019-14-13

Aug 20, 2019

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.

Airworthiness Directive
  • Boeing 767200300300F400ER

EASA AD 2019-0202

Aug 19, 2019

Main Rotor — Blade Droop Stops — Removal from Service

EASA Airworthiness Directive 2019-0202 is an airworthiness directive addressing the removal from service of main rotor blade droop stops, Part Number 37.21.800.00.00, installed on PZL W-3A and W-3AS helicopters. The directive applies to all manufacturer serial numbers of these helicopter models and mandates removal of affected parts to prevent unsafe conditions.

Airworthiness Directive
  • Wsk Pzl-Swidnik PZL W-3A
  • PZL W-3A
  • PZL W-3AS

EASA AD 2019-0199

Aug 16, 2019

Tail Rotor Drive - Ti-Bolt - Inspection / Replacement

EASA Airworthiness Directive 2019-0199 is an airworthiness directive addressing the inspection and replacement of titanium (Ti) bolts, part number L535M2001203, installed on the forward tail rotor drive shaft of Airbus Helicopters Deutschland GmbH EC135 and EC635 helicopter models. The directive applies to all variants and serial numbers of these helicopters. It mandates inspection and, if necessary, replacement of affected Ti-bolts to ensure continued airworthiness.

Airworthiness Directive
  • Airbus Helicopters EC135
  • Airbus Helicopters 635
  • Airbus Helicopters EC635

EASA AD 2019-0198

Aug 15, 2019

Flight Controls — Wiring Harness — Modification

EASA Airworthiness Directive 2019-0198 is an airworthiness directive addressing wiring harness modifications for Airbus Helicopters Deutschland GmbH MBB-BK117 D-2 helicopters. It targets specific wire harness trim connector backshells with part number M85049/90-13W02 manufactured by AMPHENOL or of unknown manufacturer. The directive aims to prevent potential short circuits in yaw and pitch trim actuators that could lead to loss of helicopter control.

Airworthiness Directive
  • Airbus Helicopters MBB-BK 117
  • Airbus Helicopters MBB-BK117 D-2

EASA AD 2019-0196

Aug 14, 2019

Fuselage — Cabin, Cargo Compartment and Airframe Parts — Inspection / Replacement [Improper Heat Treatment]

EASA Airworthiness Directive 2019-0196 is an airworthiness directive addressing improper heat treatment of certain structural parts in Airbus A318, A319, A320, and A321 aircraft. It mandates inspections and possible replacement of affected cabin, cargo compartment, and airframe parts to ensure structural integrity. The directive applies to specific manufacturer serial numbers and references Airbus Service Bulletins for inspection procedures.

Airworthiness Directive
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD CF-2019-29

Aug 13, 2019

Flight Controls — Multi-Function Spoiler Jam

Canadian Airworthiness Directive CF-2019-29 addresses a flight control issue involving the multi-function spoiler (MFS) jam on Bombardier Inc. model BD-100-1A10 aircraft, serial numbers 20003 through 20788. The directive mandates updates to the Airplane Flight Manual procedures to manage uncommanded spoiler deployment that can cause high crew workload during roll control. This AD aims to enhance flight safety by providing revised non-normal procedures for affected aircraft.

Airworthiness Directive
  • Bombardier BD-1001A10

EASA AD 2019-0195

Aug 13, 2019

Tail Rotor – Hub Assembly – Inspection / Replacement

EASA Airworthiness Directive 2019-0195 is an airworthiness directive issued by the European Union Aviation Safety Agency concerning Airbus Helicopters AS 332 and SA 330 models. It addresses inspection and replacement requirements for tail rotor hub assembly components, specifically flapping hinge components and spindle bolts, to prevent potential failures that could lead to loss of helicopter control.

Airworthiness DirectiveSuperseded
  • Airbus Helicopters SA 330
  • Airbus Helicopters AS 332
  • Airbus Helicopters EC 225

EASA AD US-2019-16-02

Aug 12, 2019

Engine Fuel Control - Fuel Pump Metering Unit - Replacement

The Federal Register Volume 84, Number 154 (August 9, 2019) final rule titled "Engine Fuel Control - Fuel Pump Metering Unit - Replacement" is an Airworthiness Directive issued by the FAA for all GE Honda Aero Engines HF120 model turbofan engines equipped with fuel pump metering unit (FPMU) assembly part number 24100-Q0A-F000. This directive addresses damage found on the permanent magnetic alternator drive gear within the FPMU assembly that could lead to engine failure. The AD mandates replacement of the affected FPMU assembly with approved parts to ensure continued airworthiness and safety.

Airworthiness Directive
  • Ge Honda Aero Engines, HF120

EASA AD 2019-0086R1

Aug 9, 2019

Flight Controls — Active Technology Load Alleviating System — Deactivation / Modification ; Airplane Flight Manual Supplement — Amendment

The document titled 'Flight Controls — Active Technology Load Alleviating System — Deactivation / Modification ; Airplane Flight Manual Supplement — Amendment' is an EASA Supplemental Type Certificate (STC) amendment issued for the CRANFIELD AEROSPACE SOLUTIONS Ltd. and TEXTRON AVIATION INC. CitationJet model 525 aircraft. It addresses modifications related to the deactivation or alteration of the Active Technology Load Alleviating System (ATLAS) flight control system. This amendment includes updates to the Airplane Flight Manual Supplement to reflect these changes.

Agency Decision
  • Textron Aviation 525 (CitationJet)
  • Textron Aviation CitationJet 525

EASA AD 2019-0194-E

Aug 9, 2019

Tail Rotor – Tail Rotor Duplex Bearing and Plug – Inspection

EASA Airworthiness Directive 2019-0194-E is an emergency directive addressing safety concerns for Leonardo S.p.A. A119 and AW119MKII helicopters, specifically those with manufacturer serial numbers up to 14966, excluding certain serial numbers. The directive mandates inspections and corrective actions related to the tail rotor duplex bearing and plug to prevent potential loss of helicopter control.

Airworthiness DirectiveSuperseded
  • Leonardo S.P.A. Helicopters A109
  • Leonardo S.P.A. Helicopters A119
  • Leonardo A119
  • Leonardo AW119MKII