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EASA Regulations & Airworthiness Directives

Browse 4771 EASA regulations with AI-powered summaries.

Aircraft:AllAirbus A320262Airbus A321257Airbus A319229Airbus A350206Airbus A330197All177Airbus A318172Boeing 737164Airbus A380162Airbus A340136Airbus A350-941119Airbus Helicopters AS 332110Airbus Helicopters EC 225107Airbus Helicopters SA 330107Boeing 787106Show all...

EASA AD 2022-0109

Flight Controls — Elevator Long Pushrod — Inspection / Replacement

EASA Airworthiness Directive 2022-0109 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Sonaca S200 and S201 aeroplanes. It addresses inspection and replacement requirements for the elevator long pushrod (ELP) due to a production deviation that may cause incorrect assembly of pushrod ends. The directive mandates inspections and potential replacement of affected parts to ensure flight control integrity.

Jun 15, 2022
Airworthiness DirectiveMaintenanceSafety MgmtSonaca Aircraft S2Sonaca S200Sonaca S201

EASA AD CF-2022-32

Fire Protection — Fire Extinguishing System — Fire Extinguisher Bottle Tests Omitted (Cargo / Engine / Auxiliary Power Unit)

The Airworthiness Directive CF-2022-32 issued by Transport Canada addresses fire protection concerns related to fire extinguisher bottle tests omitted on Mitsubishi Heavy Industries RJ Aviation ULC models CL-600-2B19, CL-600-2C10, CL-600-2C11, CL-600-2D15, CL-600-2D24, and CL-600-2E25 aircraft. It mandates new maintenance tasks and interval limitations for the restoration and pressure switch testing of fire extinguisher bottles in cargo compartments, engines, and auxiliary power units (APUs).

Jun 14, 2022
Airworthiness DirectiveMaintenanceSafety MgmtMHI RJ Aviation CL-600 (Regional Jet)Mitsubishi Heavy Industries RJ Aviation ULC CL-600-2B19Mitsubishi Heavy Industries RJ Aviation ULC CL-600-2C10Mitsubishi Heavy Industries RJ Aviation ULC CL-600-2C11Mitsubishi Heavy Industries RJ Aviation ULC CL-600-2D15Mitsubishi Heavy Industries RJ Aviation ULC CL-600-2D24Mitsubishi Heavy Industries RJ Aviation ULC CL-600-2E25

EASA AD 2022-0108

SUPERSEDED BY EASA ADR 2025-0226

The document titled SUPERSEDED BY EASA ADR 2025-0226 is an explanatory statement regarding the absence of an Airworthiness Directive (AD) for Europrop International GmbH TP400-D6 engines. It clarifies that no civil service aircraft currently operate these engines, so no public AD exists. The document serves as an informational record for design approval holders and military airworthiness authorities, recommending that affected military authorities issue their own ADs.

Jun 14, 2022
OtherMaintenanceSafety MgmtEpi Europrop International Gmbh TP400-D6

EASA AD 2022-0107

SUPERSEDED BY EASA ADR 2025-0226

The document titled SUPERSEDED BY EASA ADR 2025-0226 is an explanatory statement regarding the absence of an Airworthiness Directive (AD) for Europrop International GmbH TP400-D6 engines. It clarifies that no civil service aircraft currently operate these engines, so no public AD exists. The document serves as an informational record for military authorities and design approval holders, recommending that affected military bodies issue their own ADs.

Jun 14, 2022
OtherMaintenanceSafety MgmtEpi Europrop International Gmbh TP400-D6

EASA AD CF-2019-12R1

Auto Flight System — Airplane Flight Manual Limitations and Emergency Procedures — Velocity Decay during Low Level Flight Using Altitude Capture in One Engine Inoperative Conditions

Airworthiness Directive CF-2019-12R1 is a Canadian regulatory update addressing the Auto Flight System limitations and emergency procedures related to velocity decay during low level flight using altitude capture in one engine inoperative conditions. It applies specifically to Bombardier Inc. model BD-100-1A10 aeroplanes with serial numbers 20003 through 20867. The directive mandates updates to the Airplane Flight Manual to better handle altitude capture modes during engine failure scenarios.

Jun 10, 2022
Airworthiness DirectiveFlight OpsSafety MgmtBombardier BD-100Bombardier BD-100-1A10

EASA AD CF-2022-31

Engine — High Pressure Turbine — 2nd-Stage Disk with Suspected Material Defect

Airworthiness Directive CF-2022-31 is issued by Transport Canada concerning Pratt & Whitney Canada PW307D engines installed with specific high pressure turbine (HPT) 2nd-stage disks suspected of having a material defect. The directive applies to disks with part number 30P3182-01 and serial numbers A004D8X1 and A004E9K3. This AD addresses a potential safety risk related to uncontained HPT disk failure that could lead to engine damage and compromised aircraft safety.

Jun 10, 2022
Airworthiness DirectiveMaintenanceSafety MgmtPratt & Whitney Canada PW307

EASA AD G-2022-0011

IPECO HOLDINGS Ltd — Pilot and Co-pilot Seats — Modification / Inspection

Civil Aviation Authority Airworthiness Directive G-2022-0011 addresses safety concerns related to IPECO HOLDINGS Limited Type 3A063 pilot and co-pilot seats installed on ATR 42 and ATR 72 aircraft. The directive mandates inspections and modifications to prevent unexpected rearward movement of flight crew seats during critical phases of flight. It applies to all serial numbers of affected seat part numbers listed in the directive.

Jun 10, 2022
Airworthiness DirectiveMaintenanceSafety MgmtATR 42ATR 72

EASA AD 2022-0106

SUPERSEDED BY EASA AD 2023-0112

EASA Airworthiness Directive 2022-0106 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 Part 2 Revision 10, which includes damage tolerant airworthiness limitation items necessary for continued safe operation of these aircraft.

Jun 10, 2022
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380Airbus A380-841Airbus A380-842Airbus A380-861

EASA AD 2022-0105

SUPERSEDED BY EASA AD 2025-0121

EASA Airworthiness Directive 2022-0105 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 updated airworthiness limitations specified in Airbus A380 Airworthiness Limitations Section (ALS) Part 1 Revision 12 to ensure continued safe operation of these aircraft.

Jun 10, 2022
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380

EASA AD 2022-0051

[Correction] Fuselage — Rear Structure Junction Frame Reinforcement Angles — Inspection

EASA Airworthiness Directive 2022-0051 is a corrective directive addressing inspection requirements for the rear structure junction frame reinforcement angles on Airbus Helicopters AS 350 and AS 355 models. It applies to specific serial numbers and affected parts, including junction frames reinforced by modification 073215 or equipped with certain reinforcement angles. The directive mandates repetitive inspections to detect cracks that could lead to tail boom loss and specifies optional modification as a terminating action.

Jun 9, 2022
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters AS 350Airbus Helicopters EC 130Airbus Helicopters AS 355

EASA AD US-2022-11-19

Fuel / Oil — Check Valves — Inspection / Replacement

Federal Register Volume 87, Number 105 (June 1, 2022) Final Rule titled "Fuel / Oil — Check Valves — Inspection / Replacement" is an FAA Airworthiness Directive (AD 2022-11-19) addressing Bell Textron Inc. Model 212, 412, 412CF, and 412EP helicopters. It targets engine oil check valve P/N 209-062-520-001 and fuel check valve P/N 209-062-607-001 manufactured by Circor Aerospace with specific markings and manufacturing dates. The directive mandates inspection and replacement procedures to mitigate risks associated with cracked check valves.

Jun 9, 2022
Airworthiness DirectiveMaintenanceSafety MgmtBell Textron Inc. (Bti) 212Bell Textron Inc. (Bti) 412Bell Textron Inc. 212Bell Textron Inc. 412Bell Textron Inc. 412CFBell Textron Inc. 412EP

EASA AD 2022-0104

Main Rotor — Mast / Screws / Cover Plate — Replacement / Inspection / Oil Sample Analysis

EASA Airworthiness Directive 2022-0104 is an airworthiness directive applicable to all Airbus Helicopters EC 225 LP helicopters. It addresses issues related to the main rotor mast (MRM), specifically the mast screws and cover plate, requiring replacement, inspection, and oil sample analysis to ensure continued airworthiness. The directive aims to prevent corrosion and potential failure of critical parts in the main gearbox caused by water ingress due to improper installation of the MRM cover plate and incorrect screws.

Jun 9, 2022
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SA 330Airbus Helicopters AS 332Airbus Helicopters EC 225Airbus Helicopters EC 225 LP

EASA AD 2022-0103

SUPERSEDED BY EASA AD 2023-0184

EASA Airworthiness Directive 2022-0103 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Pilatus PC-12, PC-12/45, PC-12/47, and PC-12/47E aeroplanes of all serial numbers. It mandates compliance with updated airworthiness limitations and maintenance tasks as specified in the Pilatus PC-12 Aircraft Maintenance Manual Chapter 04-00-00. The directive ensures continued airworthiness by enforcing new and more restrictive maintenance requirements.

Jun 9, 2022
Airworthiness DirectiveMaintenanceSafety MgmtPilatus Aircraft PC-12Pilatus PC-12Pilatus PC-12/45Pilatus PC-12/47Pilatus PC-12/47E

EASA AD 2017-0237R1

Flight Controls — Trimmable Horizontal Stabilizer Actuator — Modification

EASA Airworthiness Directive 2017-0237R1 is a regulatory update addressing the trimmable horizontal stabilizer actuator (THSA) on Airbus A318, A319, A320, and A321 aircraft. It focuses on modifications related to the Electrical Load Sensing Device (ELSD) installation and activation to ensure proper detection of primary load path failures in the THSA. This directive applies to all manufacturer serial numbers of the specified Airbus A320 Family models.

Jun 8, 2022
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2022-0102

SUPERSEDED BY EASA 2024-0046

EASA Airworthiness Directive 2022-0102 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes. It mandates compliance with updated airworthiness limitations and maintenance tasks specified in the Airbus Airworthiness Limitations Section Part 4 Revision 08. The directive ensures continued airworthiness by requiring replacement of life-limited parts and performance of maintenance tasks within specified intervals.

Jun 8, 2022
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD CF-2022-30

Flight Controls — Flap Fail on Approach

Canadian Airworthiness Directive CF-2022-30 addresses a flap, slat, or slat-flap failure issue on approach for Bombardier BD-700-1A10 and BD-700-1A11 aircraft models. The directive mandates revisions to the Airplane Flight Manual (AFM) and Quick Reference Handbook (QRH) to modify procedures related to flap failure warnings. This AD aims to prevent unexpected stall warnings and stick shaker activation caused by resetting the slat flap control unit during flight.

Jun 7, 2022
Airworthiness DirectiveFlight OpsSafety MgmtBombardier BD-700Bombardier BD-700-1A10Bombardier BD-700-1A11

EASA AD US-2022-09-08

Stabilizers - Main Torque Box Skin Panel and Rear Spar Root Fitting - Inspection

The Federal Aviation Administration (FAA) Airworthiness Directive 2022-09-08 is a final rule addressing certain Boeing 787-8, 787-9, and 787-10 airplanes. This directive mandates inspections of the main torque box (MTB) skin panel and rear spar root fitting for cracking and delamination due to reports of a missing shim at a critical joint. The directive aims to ensure the structural integrity of these aircraft by requiring specific inspection and corrective actions.

Jun 7, 2022
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 787Boeing 787-8Boeing 787-9Boeing 787-10

EASA AD 2022-0100

Fuselage — Belly Fairing Torsion Box — Modification

EASA Airworthiness Directive 2022-0100 is an official regulatory document addressing the modification of the belly fairing torsion box on Airbus A380-841, A380-842, and A380-861 aeroplanes. It applies to specific manufacturer serial numbers and mandates changes to improve the structural integrity of affected parts. The directive ensures continued airworthiness by requiring compliance with Airbus Service Bulletin A380-53-8153.

Jun 2, 2022
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380

EASA AD 2022-0101-E

Wings — Outer Wing Connection — Inspection

EASA Airworthiness Directive 2022-0101-E is an emergency directive addressing a structural issue in Stemme AG S12 powered sailplanes, specifically affecting outer wing connections with part numbers 012403 (right-hand side) and 012402 (left-hand side). The directive mandates inspection of these outer wing connections due to a production deviation causing incorrect positioning of glass-fibre reinforced plastic blocks in the outer wing spar. This AD applies to Stemme S12 sailplanes with serial numbers 12-002 to 12-042 inclusive and 12-044.

Jun 2, 2022
Airworthiness DirectiveMaintenanceSafety MgmtStemme Ag S12

EASA AD 2022-0098

Aircraft Flight Manual — Section Limitations / Normal Procedures — Amendment; Flight Controls — Master Minimum Equipment List — Amendment / Primary Flight Control Computers — Modification (Software Update)

EASA Airworthiness Directive 2022-0098 is an amendment affecting Airbus A350-941 and A350-1041 aeroplanes equipped with certain flight control software standards. It addresses issues related to the primary flight control computers (PRIM) software that could lead to loss of elevator control. The directive mandates updates to the Aircraft Flight Manual, Master Minimum Equipment List, and installation of a software update to ensure continued safe operation.

Jun 1, 2022
Airworthiness DirectiveFlight OpsMaintenanceSafety MgmtAirbus A350Airbus A350-941Airbus A350-1041