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 2019-0162

Jul 10, 2019

Fuselage — Bottom Skin — Inspection

EASA Airworthiness Directive 2019-0162 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Fokker F28 Mark 0070 and Mark 0100 aeroplanes. It mandates inspection of the fuselage bottom skin to detect corrosion, cracks, bulges, or missing fasteners that could compromise structural integrity. The directive requires reporting inspection results to Fokker Services and applying repairs if defects are found.

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

EASA AD 2018-0076R1

Jul 10, 2019

Landing Gear — Hydraulic Line T-Union — Replacement

The document titled 'Landing Gear — Hydraulic Line T-Union — Replacement' is a service communication issued by FOKKER SERVICES concerning the F28 aircraft type. It addresses the replacement of the hydraulic line T-union component within the landing gear system to ensure continued airworthiness and safety. This document is relevant to operators and maintenance organizations responsible for F28 aircraft maintenance.

Other
  • Fokker F28

EASA AD CF-2019-25

Jul 9, 2019

Airframe — Corrosion

The Canadian Airworthiness Directive CF-2019-25 addresses corrosion inspection and control for Viking Air Ltd. DHC-2 Mk. I, Mk. II, and Mk. III aircraft. It mandates compliance with the revised Supplemental Inspection and Corrosion Control Manual (PSM 1-2-5, Revision 1) to ensure aging aircraft are properly inspected and maintained to prevent corrosion-related safety issues. This directive replaces previous corrosion-related directives for these aircraft models.

Airworthiness Directive
  • Viking Air DHC-2
  • Viking Air DHC-2 Mk. I
  • Viking Air DHC-2 Mk. II
  • Viking Air DHC-2 Mk. III

EASA AD CF-2019-24

Jul 8, 2019

Navigation — Flight Instruments — Unreliable Air Data in the Cockpit

Canadian Airworthiness Directive CF-2019-24 addresses unreliable air data in the cockpit for Bombardier Inc. BD-100-1A10 aeroplanes, serial numbers 20001 through 20688. This directive mandates updates to the Airplane Flight Manual to include procedures for handling unreliable airspeed and go-around scenarios. The directive aims to enhance flight safety by providing crews with guidance to manage air data system failures caused by high altitude icing.

Airworthiness Directive
  • Bombardier BD-1001A10

EASA AD 2019-0159

Jul 5, 2019

Aircraft Flight Manual — Fuel Quantity Indication System Procedure — Amendment ; Fuel — Fuel Quantity and Management System Software — Update

EASA Airworthiness Directive 2019-0159 addresses the fuel quantity indication system procedure and software update for Airbus A380-841, A380-842, and A380-861 aeroplanes. It mandates amendments to the Aircraft Flight Manual and updates to the Fuel Quantity and Management System software to correct fuel quantity indication discrepancies. This directive applies to all Airbus A380 aircraft except those with specific production modifications 77964 and 77965.

Airworthiness Directive
  • Airbus A380

EASA AD 2019-0160

Jul 5, 2019

Tail Rotor — Tail Rotor Dampers — Inspection

EASA Airworthiness Directive 2019-0160 is an airworthiness directive addressing the inspection of tail rotor dampers on Leonardo S.p.A. AW189 helicopters. It applies to tail rotor dampers with Part Number 4F6420V00254 up to serial number LK1229, excluding those marked with 'R' or meeting certain flight hour and installation time criteria. The directive mandates repetitive visual inspections of hydraulic fluid levels to detect leaks that could compromise tail rotor performance.

Airworthiness Directive
  • Leonardo S.P.A. Helicopters AW189
  • Leonardo AW189

EASA SIB CE-19-14

Jul 4, 2019

Rockwell Collins Pro Line Fusion Flight Management Systems

The Special Airworthiness Information Bulletin SAIB: CE-19-14 is an FAA informational bulletin regarding the Rockwell Collins Pro Line Fusion Flight Management Systems with part numbers 810-0163-2B0004, 810-0163-3B0001, and 810-0163-1F0001. It addresses a software issue where deleting a waypoint may cause the system to fly an incorrect turn direction during departures, STARs, or approaches. This bulletin does not impose mandatory actions but informs operators of the potential navigation anomaly.

Safety Information Bulletin

EASA AD BR-2019-05-01

Jul 4, 2019

Superseded by ANAC AD 2022-02-01

Brazilian Airworthiness Directive 2019-05-01 issued by the Agência Nacional de Aviação Civil (ANAC) applies to Embraer S.A. ERJ 170 series airplanes with specific manufacturer serial numbers. This directive mandates revisions to the maintenance and inspection programs to incorporate updated airworthiness limitations and inspections to ensure structural integrity. It includes requirements for Certification Maintenance Requirements, Airworthiness Limitation Inspections, Fuel System Limitation Items, and Life Limited Items.

Airworthiness Directive
  • Embraer ERJ 170

EASA AD BR-2019-05-02

Jul 4, 2019

Superseded by ANAC BRAZIL AD 2023-12-02

Brazilian Airworthiness Directive AD No. 2019-05-02 issued by the Agência Nacional de Aviação Civil (ANAC) applies to Embraer S.A. ERJ 190 series airplanes, including models ERJ 190-100 STD, LR, IGW, ECJ, SR, and ERJ 190-200 STD, LR, and IGW with specified serial numbers. This directive mandates updates to maintenance and inspection programs to incorporate revised airworthiness limitations to ensure structural integrity. The AD includes an errata correcting omitted compliance time details.

Airworthiness Directive
  • Embraer ERJ 190100 STD100 LR100 IGW100 ECJ100 SR200 STD200 LR200 IGW

EASA AD 2019-0158

Jul 4, 2019

Superseded by EASA ADR 2019-0276

The document titled SUPERSEDED BY EASA ADR 2019-0276 is an explanatory statement regarding the absence of an Airworthiness Directive (AD) for the Airbus A400M aircraft. It clarifies that no publicly available AD exists because there are currently no Airbus A400M aeroplanes in civil service. The document serves as an informational record for design approval holders and military airworthiness authorities, recommending that affected military authorities issue their own ADs.

Other
  • Airbus Military A400M
  • Airbus A400M

EASA AD 2019-0155

Jul 3, 2019

Doors — Passenger / Crew / Emergency Exit Door Girt Bar Slider Mechanism — Functional Check / Lubrication

EASA Airworthiness Directive 2019-0155 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A330 and A340 aeroplanes, including all serial numbers and specific models such as A330-941 and A340-500/-600 series. The directive mandates functional checks and lubrication of the passenger, crew, and emergency exit door girt bar slider mechanisms to ensure proper locking and operation. This directive aims to maintain safe evacuation capabilities by preventing escape slide detachment during emergencies.

Airworthiness Directive
  • Airbus A330
  • Airbus A340

EASA AD 2019-0157

Jul 3, 2019

Rotor(s) — Main Rotor Hub Drag and Flapping Hinges — Inspection

Rotor(s) — Main Rotor Hub Drag and Flapping Hinges — Inspection is an airworthiness directive applicable to AIRBUS HELICOPTERS models SA 330, AS 332, and EC 225. The document mandates inspections of the main rotor hub drag and flapping hinges to ensure continued airworthiness and safety. It targets specific components critical to rotor integrity on these helicopter types.

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

EASA AD 2019-0154

Jul 3, 2019

Time Limits / Maintenance Checks – Airworthiness Limitations Section Chapter 5-40 – Amendment

EASA Airworthiness Directive 2019-0154 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all Dassault Aviation Falcon 2000EX aeroplanes. It mandates compliance with updated airworthiness limitations detailed in Chapter 5-40, Revision 12, of the Dassault Falcon 2000EX Aircraft Maintenance Manual. This directive ensures continued airworthiness by enforcing maintenance tasks and life limits for components.

Airworthiness DirectiveSuperseded
  • Dassault Falcon 2000
  • Dassault Falcon 2000EX

EASA AD 2019-0153

Jul 3, 2019

Time Limits / Maintenance Checks – Airworthiness Limitations Section Chapter 5-40 – Amendment

EASA Airworthiness Directive 2019-0153 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all Dassault Aviation Mystère-Falcon 200 aeroplanes. It mandates compliance with the updated airworthiness limitations section in the Dassault Mystère-Falcon 200 Aircraft Maintenance Manual Chapter 5-40, Revision 18. This directive ensures continued airworthiness by enforcing maintenance tasks and life limits for components.

Airworthiness DirectiveSuperseded
  • Dassault Mystère-Falcon 20GF
  • Dassault 200
  • Dassault Mystère-Falcon 200

EASA AD US-2019-12-12

Jul 1, 2019

Airplane Flight Manual - Update / Placard Installation

The Airplane Flight Manual - Update / Placard Installation is a final rule airworthiness directive issued by the FAA affecting Piper Aircraft, Inc. Model PA-46-600TP (M600) airplanes. It mandates inserting a ground operations limitation into the airplane flight manual and installing a placard limiting ground operations due to understrength rivets found in the bulkhead assembly. The directive also offers an optional terminating action involving rivet replacement to reinforce the bulkhead.

Airworthiness Directive
  • Piper Aircraft PA-46 (Malibu)
  • Piper PA-46-600TP

EASA AD US-2019-11-02

Jul 1, 2019

Wings - Underwing Longerons - Inspection

Airworthiness Directive 2019-11-02 is a final rule issued by the Federal Aviation Administration (FAA) addressing The Boeing Company Model 777 airplanes. It mandates inspections of the left and right side underwing longerons to detect cracks and requires related investigative and corrective actions to ensure structural integrity and prevent fuel leakage. This directive updates previous requirements to enhance safety for affected aircraft.

Airworthiness Directive
  • Boeing 777

EASA AD 2019-0150

Jun 28, 2019

Engine – Rotating Air High Pressure Turbine Front Seal – Replacement

EASA Airworthiness Directive 2019-0150 is an airworthiness directive addressing certain CFM International CFM56-5B, CFM56-5C, and CFM56-7B engines installed on various Airbus A318, A319, A320, A321, A340 and Boeing 737-600, 737-700, 737-800, and 737-900 aircraft. The directive mandates replacement of specific rotating air high pressure turbine (HPT) front seals identified by part numbers 1795M36P01 and 1795M36P02 due to risk of cracks leading to uncontained engine failure. It provides detailed affected serial numbers and compliance requirements for operators and maintenance organizations.

Airworthiness DirectiveSuperseded
  • CFM International CFM56-5B
  • CFM International CFM56-5C
  • CFM International CFM56-7B
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321
  • Airbus A340
  • Boeing 737-600
  • Boeing 737-700
  • Boeing 737-800
  • Boeing 737-900

EASA AD 2019-0151-E

Jun 28, 2019

Landing Gear — Main Landing Gear Sliding Tubes — Inspection

EASA Airworthiness Directive 2019-0151-E is an emergency directive addressing inspection requirements for the main landing gear sliding tubes on Airbus A319 and A320 aeroplanes with specific manufacturer serial numbers. It mandates repetitive magnetic particle inspections and one-time detailed inspections of affected sliding tubes with part number 201371304 to detect cracks or defects. The directive aims to prevent potential landing gear axle fractures that could lead to landing gear collapse and possible injury.

Airworthiness Directive
  • Airbus A319
  • Airbus A320

EASA AD 2019-0152-E

Jun 28, 2019

Main Rotor Drive – Main Gearbox – Replacement; Placards and Markings – ENG1 Training Idle Switch – Installation /; Operational Restriction

EASA Airworthiness Directive 2019-0152-E is an emergency directive addressing Airbus Helicopters EC 225 LP models equipped with certain main gearboxes (MGB) identified by specific part numbers. The directive mandates inspection and replacement of affected MGBs and installation of operational restrictions related to the ENG1 Training Idle switch. It aims to prevent reduced power transfer capacity in one-engine inoperative scenarios due to detected wear and damage in the main gearbox components.

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