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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 SIB 2024-08

Misidentification and Erroneous Selection of Propeller Feathering Controls in Flight

EASA Safety Information Bulletin 2024-08 is issued to raise awareness about the risk of misidentification and erroneous selection of propeller feathering controls in flight on large CS-25 turboprop aeroplanes. The bulletin references an accident involving an ATR72/212A version 500 near Pokhara International Airport, where inadvertent feathering of both propellers led to total thrust loss and a fatal crash. It highlights the importance of flight crew alerts and cockpit indications in detecting such errors promptly to prevent loss of control.

Jul 23, 2024
Safety Information BulletinFlight OpsSafety Mgmt

EASA AD 2024-0145

Wings — Main Landing Gear Support Rib 5 — Inspection

EASA Airworthiness Directive 2024-0145 is an airworthiness directive affecting Airbus A300, A300-600, and A300-600ST aeroplanes with specific manufacturer serial numbers. It mandates inspections of the main landing gear support Rib 5 lower flange for cracks, focusing on parts except those with certain part numbers. This directive updates previous requirements to include additional aircraft groups and inspection procedures.

Jul 23, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A300Airbus A300-600Airbus A300-600ST (Beluga)Airbus A300-600ST

EASA AD US-2024-14-03

Auto Flight - Garmin GFC 500 Autopilot System - Software Update

The Federal Aviation Administration's Airworthiness Directive 2024-14-03 addresses various airplanes equipped with the Garmin GFC 500 Autopilot System installed under Supplemental Type Certificate No. SA01866WI. This directive mandates a software update to the Garmin GFC 500 Autopilot System to prevent un-commanded automatic pitch trim runaway events. The affected aircraft include all models specified in the directive that have the optional GSA 28 pitch trim servo installed.

Jul 22, 2024
Airworthiness DirectiveMaintenanceSafety MgmtCommander (Cpac, Inc.) 112Commander (Cpac, Inc.) 114Daher Aerospace TBMooney International Corporation M20Piper Aircraft PA-24 (Comanche)Piper Aircraft PA-28 (Archer)Piper Aircraft PA-28 (Cadet)Piper Aircraft PA-28 (Cherokee)Piper Aircraft PA-28 (Dakota)Piper Aircraft PA-28 (Warrior)Piper Aircraft PA-28R (Arrow)Piper Aircraft PA-30 (Twin Comanche)Piper Aircraft PA-32 (Cherokee Six)Piper Aircraft PA-32 (Piper 6X)Piper Aircraft PA-32 (Saratoga)Piper Aircraft PA-32R (Lance)Piper Aircraft PA-39 (Twin Comanche)Textron Aviation 172 (Skyhawk)Textron Aviation 172RGTextron Aviation 177 (Cardinal)Textron Aviation 177RG (Cardinal RG)Textron Aviation 182 (Skylane)Textron Aviation 19Textron Aviation 206Textron Aviation U206 (Super Skywagon)Textron Aviation 206H (Stationair)Textron Aviation 210 (Centurion)Textron Aviation 23 (Musketeer)Textron Aviation 24 (Sierra)Textron Aviation 33 (Bonanza)Textron Aviation 35 (Bonanza)Textron Aviation 36 (Bonanza)Textron Aviation F172Textron Aviation F177RGTextron Aviation F182Textron Aviation FR172 (Reims Rocket)Textron Aviation P172DTextron Aviation P206Textron Aviation TP206 (Super Skylane)Textron Aviation R172 (Hawk XP)

EASA AD CF-2024-26

SUPERSEDED BY TCCA AD CF-2025-61

Canadian Airworthiness Directive CF-2024-26 addresses corrosion and wear issues on the slat tracks of Airbus Canada Limited Partnership aeroplanes, specifically models BD-500-1A10 and BD-500-1A11. The directive mandates inspections, cleaning, greasing, and repairs of slat tracks to prevent potential structural damage caused by slat panel loss. It applies to aircraft with serial numbers R50001 and subsequent for BD-500-1A10, and 55001 and subsequent for BD-500-1A11.

Jul 22, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus BD-500 (A220 Series)Airbus Canada Limited Partnership BD-500-1A10Airbus Canada Limited Partnership BD-500-1A11

EASA AD 2024-0143

Stabilizers — Maintenance Instructions — Amendment

EASA Airworthiness Directive 2024-0143 is an amendment addressing maintenance instructions for stabilizers on Airbus A330 and A340 aeroplanes. It applies to all manufacturer serial numbers of specified A330 and A340 models. The directive prohibits the use of certain maintenance manual instructions that incorrectly recommend oxygen for pressure testing, which could lead to safety hazards.

Jul 19, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A330Airbus A340

EASA AD 2023-0154R1

Stabilizers — Vertical Upper Fin Assembly — Inspections

EASA Airworthiness Directive 2023-0154R1 is an updated safety directive addressing inspections of the vertical upper fin assembly on Airbus Helicopters AS 355 series (E, F, F1, F2, N, NP). It mandates cleaning and repetitive inspections of the right-hand upper fin spar to detect structural cracks that could lead to in-flight separation of the fin and potential loss of control. The directive also references installation of a reinforced upper fin assembly as a terminating action for inspections.

Jul 19, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters AS 355

EASA AD 2024-0144

Tail Rotor Drive — Shaft-Line — Check / Measurement / Modification

EASA Airworthiness Directive 2024-0144 is issued for Airbus Helicopters EC 130 T2 models equipped with specific tail rotor drive shaft components. It addresses the inspection, measurement, and modification requirements for the tail rotor drive shaft, sliding flange, and equipped splined sleeve to prevent potential failures. The directive mandates repetitive vibration checks and modifications to certain helicopter groups to ensure continued airworthiness.

Jul 19, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters AS 350Airbus Helicopters EC 130Airbus Helicopters EC 130 T2

EASA AD 2012-0257-CN

CANCELLED: Tail Rotor — Laminated Half-Bearings — Inspection / Replacement

EASA Airworthiness Directive Cancellation Notice 2012-0257-CN cancels the previous EASA Emergency AD 2012-0257-E concerning inspection and replacement of laminated half-bearings on the tail rotors of Airbus Helicopters AS 350 and AS 355 models. This cancellation affects all serial numbers of AS 350 B, BA, BB, B1, B2, D, and most B3 helicopters except those with modification 075601, as well as AS 355 E, F, F1, F2, N, and NP helicopters. The directive addresses safety concerns related to premature failure of laminated half-bearings that could lead to tail rotor failure and loss of control in flight.

Jul 17, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters AS 350Airbus Helicopters EC 130Airbus Helicopters AS 355

EASA AD 2024-0142

Fuselage — Rear MGB Suspension Bar Fittings Attachment Screws — Replacement

EASA Airworthiness Directive 2024-0142 is an airworthiness directive addressing Airbus Helicopters AS332 L2 and EC225 LP models. It mandates the replacement of rear main gearbox (MGB) suspension bar fittings attachment screws, specifically part number 332A22-3644-20, due to identified overlength and deformation issues. The directive applies to helicopters with Airbus Helicopters modification 07.28496 or those that have incorporated specific Alert Service Bulletins in service.

Jul 17, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SA 330Airbus Helicopters AS 332Airbus Helicopters EC 225Airbus Helicopters AS332 L2Airbus Helicopters EC225 LP

EASA AD US-2024-13-02

Oxygen - Passenger Service Unit Oxygen Generators - Inspection

The Federal Aviation Administration's Airworthiness Directive 2024-13-02 addresses a safety issue affecting all Boeing 737-8, 737-9, 737-8200, 737-700, 737-800, and 737-900ER series airplanes. This directive mandates inspections of passenger service unit (PSU) oxygen generator installations due to reports of oxygen generators shifting out of position caused by retention strap failures. The AD aims to ensure the functionality of supplemental oxygen systems during depressurization events.

Jul 17, 2024
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 737Boeing 737-8Boeing 737-9Boeing 737-8200Boeing 737-700Boeing 737-800Boeing 737-900ER

EASA AD 2024-0141

SUPERSEDED BY EASA AD 2025-0074

EASA Airworthiness Directive 2024-0141 is issued for Airbus A380-841, A380-842, and A380-861 aeroplanes. It mandates repetitive inspections of the main landing gear attachment rib 9 fittings on both left-hand and right-hand wings to detect cracks and sealant condition. This directive addresses potential structural integrity risks due to corrosion and cracking in these critical components.

Jul 16, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380Airbus A380-841Airbus A380-842Airbus A380-861

EASA AD 2024-0140

Flight Controls — Angle of Attack Probes — Replacement

Flight Controls — Angle of Attack Probes — Replacement is a regulatory document concerning the ATR42 and ATR72 aircraft models. It addresses the replacement requirements for angle of attack probes used in the flight control systems of these aircraft. The document aims to ensure continued airworthiness and safety by specifying necessary maintenance actions.

Jul 12, 2024
Airworthiness DirectiveMaintenanceSafety MgmtATR ATR42ATR ATR72ATR 42ATR 72

EASA AD BR-2024-04-01

NOT ELIGIBLE FOR ADOPTION - EASA POSITION ATTACHED

The document titled NOT ELIGIBLE FOR ADOPTION - EASA POSITION ATTACHED outlines EASA's position on various foreign Airworthiness Directives (ADs) related to potential 5G C-Band Wireless Broadband Interference affecting aircraft equipped with radio (radar) altimeters. These foreign ADs, issued by authorities such as the FAA, Transport Canada Civil Aviation, and ANAC Brazil, apply to multiple transport and commuter category airplanes but are not eligible for adoption by EASA. EASA has not identified an unsafe condition warranting mandatory action but continues coordination with design approval holders.

Jul 12, 2024
OpinionSafety Mgmt

EASA AD 2024-0139

Stabilizers — Vertical Fin — Inspection / Modification / Placards and Markings — Interior Placards — Installation / Aircraft Flight Manual / Airspeed Limitations — Amendment

EASA Airworthiness Directive 2024-0139 is an amendment addressing inspection, modification, and placard installation requirements for the vertical fin stabilizers of Airbus Helicopters AS 350 and AS 355 models. It applies to all serial numbers of AS 355 E, F, F1, F2, N, NP helicopters and AS 350 B3 helicopters except those with modification 073148 embodied in production. The directive mandates inspections, cleaning, flight manual amendments, placard installations, and introduces a reinforced upper fin assembly modification.

Jul 12, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters AS 350Airbus Helicopters EC 130Airbus Helicopters AS 355

EASA AD 2024-0097R2

SUPERSEDED BY EASA AD 2025-0189

EASA Airworthiness Directive 2024-0097R2 is a regulatory update addressing inspection and maintenance requirements for Airbus A318, A319, A320, and A321 aircraft. It focuses on the main landing gear (MLG) door hinge and actuator fittings on the keel beam to detect and prevent cracks that could lead to in-flight detachment of MLG doors. The directive applies to both Current Engine Option (CEO) and New Engine Option (NEO) variants, specifying inspection methods and intervals.

Jul 12, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2024-0138

Equipment/Furnishings — Seat Rails - Inspection

EASA Airworthiness Directive 2024-0138 is an airworthiness directive issued for Tecnam P-Mentor aeroplanes, specifically serial numbers 1003 through 1056, 1064 through 1075, 1078 through 1082, 1089, 1090, 1118, 1119, 1124, 1125, and 1126, excluding those with Tecnam modification MOD2002/339 or Service Bulletin SB-748-CS embodied. The directive addresses inspection requirements for the seat rails of pilot and co-pilot seats due to a reported failure of the pilot seat locking mechanism. It mandates repetitive inspections and corrective actions to prevent in-flight unlocking of the pilot seat.

Jul 11, 2024
Airworthiness DirectiveMaintenanceSafety MgmtTecnam P2002Tecnam P-Mentor

EASA AD 2024-0137

Landing Gear — Nose Landing Gear Uplock Bracket — Inspection

EASA Airworthiness Directive 2024-0137 is an airworthiness directive addressing the inspection of the Nose Landing Gear Uplock Bracket Assembly, part number 001A322D3100002, on Dornier 328-100 and Dornier 328-300 aeroplanes. This directive mandates a one-time detailed inspection to detect cracking in the affected part to prevent uncommanded nose landing gear extension. It applies to all manufacturer serial numbers of these aircraft models.

Jul 11, 2024
Airworthiness DirectiveMaintenanceSafety MgmtDeutsche Aircraft Gmbh Dornier 328Dornier 328-100Dornier 328-300

EASA AD 2024-0136

Time Limits / Maintenance Checks — Time Limits Manual / Maintenance Programme — Amendment

EASA Airworthiness Directive 2024-0136 is an amendment concerning the Rolls-Royce Deutschland BR700-725A1-12 engines, commonly installed on Gulfstream G650 aircraft. This directive mandates compliance with the updated Time Limits Manual (TLM) Revision 27, which contains mandatory airworthiness limitations and maintenance tasks. The directive ensures continued airworthiness by enforcing updated maintenance schedules and life limits for engine components.

Jul 11, 2024
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg BR700-710Gulfstream G650

EASA AD 2024-0092R1

Doors — Main Deck Cargo Door Actuator Bearing Fittings — Inspection

EASA Airworthiness Directive 2024-0092R1 is an updated regulatory document addressing inspection requirements for the main deck cargo door actuator bearing fittings on Airbus A300, A300-600, and A310 freighter aircraft. The directive mandates inspections to detect cracks caused by fatigue in these actuator fittings to prevent potential unsafe conditions during cargo door operations. It applies to all affected aircraft serial numbers, including those modified by specific EASA Supplemental Type Certificates.

Jul 10, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A300Airbus A300-600Airbus A310

EASA AD US-2024-12-04

Engine - High-Pressure Turbine 2nd Stage Blade Assemblies - Inspections

The Federal Register document titled "Engine - High-Pressure Turbine 2nd Stage Blade Assemblies - Inspections" is a final rule airworthiness directive issued by the FAA affecting Pratt & Whitney Model PW2037, PW2037M, and PW2040 engines. It addresses an unsafe condition caused by fractures in the high-pressure turbine 2nd stage turbine hub assembly lugs that led to in-flight shutdowns and fires. The directive mandates inspections and potential replacement of affected turbine hub and blade assemblies.

Jul 10, 2024
Airworthiness DirectiveMaintenanceSafety MgmtPratt & Whitney PW2000