EASA Regulations & Airworthiness Directives

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

Aircraft:AllAirbus A320286Airbus A321285Airbus A319253Airbus A350224Airbus A330221Airbus A318189Airbus A380182Boeing 737175Airbus A340141Airbus A350-941134Airbus BD-500 (A220 Series)123Airbus Helicopters AS 332119Airbus Helicopters EC 225116Airbus Helicopters SA 330116Boeing 787116Show all...

EASA AD US-2019-08-05

May 8, 2019

Hydraulic Power - Hydraulic Tubing / Check Valve / Flight Control Software - Installation

Federal Aviation Administration Airworthiness Directive 2019-08-05 is a final rule addressing certain Boeing 787-8 and 787-9 airplanes. It mandates the installation of hydraulic tubing, a pressure-operated check valve, and updated flight control software to mitigate risks associated with damage in tire/wheel threat zones. This directive aims to prevent loss of braking on one main landing gear truck, loss of nose wheel steering, and loss of directional control on the ground at low speeds.

Airworthiness Directive
  • Boeing 78789

EASA AD 2019-0100

May 7, 2019

Aircraft Flight Manual — Landing Distance Determination Procedure — Amendment

EASA Airworthiness Directive 2019-0100 is an amendment concerning the Airbus A340-541, A340-542, A340-642, and A340-643 aeroplanes. It addresses the Aircraft Flight Manual (AFM) landing distance determination procedures to correct inconsistencies in brake failure entries affecting landing performance calculations. This directive applies to all manufacturer serial numbers of the specified Airbus A340 models.

Airworthiness Directive
  • Airbus A340541542642643

EASA AD CF-2019-16

May 7, 2019

Flight Control System — Yaw Trim Runaway

Canadian Airworthiness Directive CF-2019-16 is an emergency directive addressing a yaw trim runaway issue in Bell Helicopter Textron Canada Limited model 429 helicopters, serial numbers 57001 and subsequent. It mandates revisions to the rotorcraft flight manual to mitigate risks associated with uncommanded yaw control inputs during ground operations. The directive focuses on improving pilot procedures and flight manual content to maintain helicopter control in the event of a trim runaway.

Airworthiness Directive
  • Bell 429
  • Bell Helicopter Textron Canada Limited 429

EASA AD 2018-0058R2

May 6, 2019

Flight Controls — Station Position Pick-Off Unit — Calibration Procedure

Flight Controls — Station Position Pick-Off Unit — Calibration Procedure is a technical document issued by AIRBUS S.A.S. for the Airbus A350 aircraft. It provides detailed instructions on how to properly calibrate the Station Position Pick-Off Unit, a critical component of the flight control system. This procedure ensures accurate position feedback necessary for safe and reliable aircraft operation.

Other
  • Airbus A350

EASA SIB NE-19-08

May 6, 2019

Lycoming Engines - Parallel Valve Cylinders and Head Assemblies

The FAA Special Airworthiness Information Bulletin NE-19-08 addresses cracking issues in certain Lycoming Engines equipped with Parallel Valve Cylinders and Head Assemblies shipped between September 1, 2013, and April 30, 2015. This bulletin applies to Lycoming engines excluding the 0-235 series and informs operators and maintenance personnel about the potential for cylinder cracking without mandating regulatory action. It highlights symptoms, inspection recommendations, and cautions against repairing affected cylinders.

Safety Information Bulletin

EASA AD RU-2019-322-01

May 6, 2019

Superseded by FATA AD 2020-FATA-01020A-13

Airworthiness Directive 2019-322-01 issued by the Federal Air Transportation Agency of the Russian Federation addresses the use of titanium semi-finished products of non-confirmed origin in the production of components for the RRJ-95 aircraft. The directive mandates detailed and visual inspections of various structural components including main landing gear doors, aileron root spars, flight spoilers, and pylon box parts. It applies specifically to RRJ-95 aircraft manufactured in the Russian Federation.

Airworthiness Directive
  • Irkut Corporation Jsc RRJ-95
  • RRJ-95

EASA AD 2019-0098

May 3, 2019

Fuselage — Forward Emergency Exit Door Doubler — Inspection

EASA Airworthiness Directive 2019-0098 is an airworthiness directive addressing the inspection of the forward emergency exit door doublers on Airbus A321-211, A321-212, A321-213, A321-231, and A321-232 aeroplanes. It requires a one-time detailed inspection of the internal upper doublers on both left-hand and right-hand sides of the forward emergency exit doors to detect any drill-start defects. The directive applies to specific manufacturer serial numbers listed in the document.

Airworthiness Directive
  • Airbus A321

EASA AD 2019-0095

Apr 30, 2019

Equipment / Furnishings — Lavatory Waste Bins / Fire Extinguishers — Inspection / Modification / Replacement

EASA Airworthiness Directive 2019-0095 is an airworthiness directive addressing Fokker F28 Mark 0070 and Mark 0100 aeroplanes. It focuses on the inspection, modification, and replacement of lavatory waste bins and fire extinguishers to prevent interference that could cause fire extinguisher failure. The directive applies to specific lavatory waste bin part numbers and fire extinguishers with certain part numbers installed on these aircraft.

Airworthiness Directive
  • Fokker F28
  • Fokker F28 Mark 0070
  • Fokker F28 Mark 0100

EASA AD 2019-0097

Apr 30, 2019

Superseded by EASA ADR 2020-0098

The document titled SUPERSEDED BY EASA ADR 2020-0098 is an explanatory statement regarding the absence of an Airworthiness Directive (AD) for the Airbus A400M aeroplane in civil service. It clarifies that no publicly available AD exists because the Airbus A400M is not currently operated in civil aviation. The document serves as an informational record for design approval holders and military airworthiness authorities.

OtherSuperseded
  • Airbus Military A400M
  • Airbus A400M

EASA AD 2019-0096

Apr 30, 2019

Wings — Landing Flap Support Arms — Inspection

EASA Airworthiness Directive 2019-0096 is an airworthiness directive affecting Dornier 328-100 aeroplanes with serial numbers 3032 to 3086 inclusive. It addresses the inspection of landing flap support arms due to missing rivets that could compromise the structural integrity of the flap arms. The directive requires inspections and corrective actions to ensure continued airworthiness of the affected aircraft.

Airworthiness Directive
  • Deutsche Aircraft Gmbh Dornier 328
  • Dornier 328-100

EASA AD CF-2019-15

Apr 29, 2019

Tail Rotor System — Incorrect Assembly

Canadian Airworthiness Directive CF-2019-15 is an emergency directive addressing an incorrect assembly issue in the tail rotor system of Bell Helicopter Textron Canada Limited model 429 helicopters, serial numbers 57001 through 57363. The directive focuses on the improper installation of the Curvic Coupling Part Number 429-012-120-101, which can lead to loosening of the tail rotor assembly and loss of drive to the outboard tail rotor blades. This condition affects the helicopter's directional control and safety.

Airworthiness Directive
  • Bell 429
  • Bell Helicopter Textron Canada Limited 429

EASA AD CF-2016-19R2

Apr 26, 2019

Cold Weather Operations — Introduction of Low Temperature Ground Wing Anti-Ice System

The Canadian Airworthiness Directive CF-2016-19R2 addresses cold weather operations for Bombardier Inc. model CL-600-2B19 aeroplanes, serial numbers 7003 and subsequent. It mandates the installation of a Low Temperature Ground Wing Anti-Ice System to prevent wing contamination during ground operations in cold weather. This directive updates previous revisions and includes maintenance and flight manual changes to enhance take-off safety.

Airworthiness Directive
  • MHI RJ Aviation CL-600 (Regional Jet)
  • Bombardier CL-600-2B19

EASA AD 2019-0093

Apr 26, 2019

Flight Controls – Slat Geared Rotary Actuators – Repair / Replacement

EASA Airworthiness Directive 2019-0093 is an airworthiness directive issued for certain Airbus A330 models, specifically A330-202, A330-243, A330-243F, A330-302, A330-323, and A330-343 with specific manufacturer serial numbers. It addresses an unsafe condition related to cracks found in the ring gears of slat geared rotary actuators (SGRA) with part number 926C0000-01. The directive mandates inspection and replacement of affected parts to ensure continued airworthiness.

Airworthiness DirectiveSuperseded
  • Airbus A330

EASA AD 2019-0092

Apr 26, 2019

Fuel – Engine Fuel Supply Hoses – Inspection

EASA Airworthiness Directive 2019-0092 is an airworthiness directive issued for Airbus Helicopters EC 225 LP models. It addresses a safety concern involving the left hand side engine fuel supply hose, part number 704A34416087, which may become twisted and restrict fuel flow, potentially causing engine power loss during flight. The directive mandates inspection and corrective actions to ensure continued airworthiness.

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

EASA AD 2019-0094

Apr 26, 2019

Pneumatic — Bleed Monitoring Computer — Modification / Replacement

EASA Airworthiness Directive 2019-0094 is an airworthiness directive affecting Airbus A320-251N, A320-271N, A321-251N, A321-253N, A321-271N, and A321-272N aeroplanes. It addresses issues with the Bleed Monitoring Computer (BMC) software that regulate pneumatic bleed temperature on these aircraft models. The directive mandates modification or replacement of affected BMC software to ensure safe operation.

Airworthiness Directive
  • Airbus A320251N271N
  • Airbus A321251N253N271N272N

EASA AD 2019-0090

Apr 26, 2019

Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 2 – Damage Tolerant Airworthiness Limitation Items – Implementation

EASA Airworthiness Directive 2019-0090 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all certified models and serial numbers of Airbus A300-600 aeroplanes. It mandates compliance with the Damage Tolerant Airworthiness Limitation Items as specified in the Airbus A300-600 Airworthiness Limitations Section Part 2, Revision 03. This directive ensures continued airworthiness by updating maintenance tasks and intervals.

Airworthiness DirectiveSuperseded
  • Airbus A300-600

EASA AD 2019-0091

Apr 26, 2019

Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 2 – Damage Tolerant Airworthiness Limitation Items – Implementation

EASA Airworthiness Directive 2019-0091 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all certified models of Airbus A310 aeroplanes. It mandates compliance with the updated Damage Tolerant Airworthiness Limitation Items as specified in Airbus A310 Airworthiness Limitations Section Part 2 Revision 03 and Variation 3.1. This directive ensures the continued airworthiness of Airbus A310 aircraft by enforcing updated maintenance tasks and intervals.

Airworthiness DirectiveSuperseded
  • Airbus A310

EASA AD 2019-0089

Apr 25, 2019

Engine Controls – Push-Pull Control and Beta Switch – Inspection /; Replacement

EASA Airworthiness Directive 2019-0089 is an airworthiness directive issued by the European Union Aviation Safety Agency addressing safety concerns in GE Aviation Czech H80-200 and H85-200 engines installed on Aircraft Industries L 410 UVP-E20, L 410 UVP-E20 CARGO, and L 410 NG aircraft with Avia Propeller AV-725 propellers. The directive mandates inspections, adjustments, and modifications of the engine push-pull control and Beta Switch components to prevent inadvertent propeller pitch changes that could lead to loss of aircraft control.

Airworthiness DirectiveSuperseded
  • Ge Aviation Czech H75, H80, H85
  • Aircraft Industries L 410 UVP-E20
  • Aircraft Industries L 410 UVP-E20 CARGO
  • Aircraft Industries L 410 NG

EASA AD US-2019-06-02

Apr 24, 2019

[Correction] Engine Fuel - Fuel Nozzle - Replacement

Correction to Airworthiness Directive 2019-06-02 issued by the Federal Aviation Administration (FAA) addresses certain Pratt & Whitney Division PW4158 turbofan engines. This directive targets engines with specific serial numbers and requires replacement of fuel nozzles and fuel nozzle supply manifold assemblies due to high cycle fatigue cracks. It also mandates installation of new brackets and clamps on the fuel nozzle supply manifold assemblies to ensure continued airworthiness.

Airworthiness Directive
  • Pratt & Whitney PW4000

EASA AD DCA-750XL-37

Apr 24, 2019

Engine Fuel Lines and Electrical Wiring — Inspection

Airworthiness Directive DCA/750XL/37 Engine Fuel Lines and Electrical Wiring – Inspection is issued by the Civil Aviation Authority of New Zealand and applies to Pacific Aerospace Limited 750XL aircraft, serial numbers 101 through 215, 220, 8001, and 8002 fitted with or configured for an air conditioner and/or a standby alternator. This directive mandates inspection of engine fuel feed line hoses and electrical wiring forward of the engine firewall to detect chafing that could cause fuel leaks and fire. It references Pacific Aerospace Mandatory Service Bulletin PACSB/XL/113 issue 2 for inspection and corrective actions.

Airworthiness Directive
  • Nzskydive 750XL
  • Pacific Aerospace 750XL