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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 US-2025-05-02

Engine - Stage 1 Turbine Forward Cooling Plate and Stage 2 Turbine Aft Cooling Plate - Replacement

The document titled 'Engine - Stage 1 Turbine Forward Cooling Plate and Stage 2 Turbine Aft Cooling Plate - Replacement' is a regulatory directive concerning the replacement of specific turbine cooling plates in aircraft engines. It addresses maintenance and replacement procedures for the Stage 1 turbine forward cooling plate and the Stage 2 turbine aft cooling plate components. The directive is relevant to aviation maintenance professionals responsible for engine upkeep and safety compliance.

Apr 2, 2025
Airworthiness DirectiveMaintenanceSafety MgmtGeneral Electric CT7-5General Electric CT7-7General Electric CT7-9

EASA AD US-2025-06-10

Stabilizers - Horizontal Stabilizer Pivot Pin Assemblies - Inspection

Federal Aviation Administration Airworthiness Directive 2025-06-10 is a final rule addressing certain Boeing 787-8, 787-9, and 787-10 airplanes. It mandates inspection of the left and right horizontal stabilizer pivot pin assemblies for misalignment and incorrect gapping. The directive aims to ensure the integrity of the pivot pin lockring, outer pivot pin, and outboard spacer to prevent unsafe conditions.

Apr 2, 2025
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 787

EASA AD 2025-0071

Fuselage — Central Windshield Frame — Inspection

EASA Airworthiness Directive 2025-0071 is an airworthiness directive addressing inspection requirements for the central windshield frame on Airbus A330 aeroplanes. It applies to multiple A330 variants with affected part numbers F531-23012-200 or F531-23011-200 installed. The directive mandates repetitive inspections to detect potential cracks due to incorrect shot peening applied during production starting in 2008.

Mar 31, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A330

EASA AD CF-2025-19

Stabilizers — Elevator Power Control Unit (PCU) Bracket and Elevator Front Spar Cracks

Canadian Airworthiness Directive CF-2025-19 addresses cracks found in the Elevator Power Control Unit (PCU) bracket and elevator front spar on De Havilland Aircraft of Canada Limited DHC-8-401 and DHC-8-402 aeroplanes, specifically serial numbers 4001 and 4003 through 4633. The directive mandates inspections and modifications to prevent elevator jamming and potential loss of pitch control. It includes updated design solutions and inspection procedures to enhance structural integrity of the horizontal stabilizer and elevator assemblies.

Mar 31, 2025
Airworthiness DirectiveMaintenanceSafety MgmtDe Havilland Canada DHC-8

EASA AD 2025-0072

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

EASA Airworthiness Directive 2025-0072 is an amendment concerning the Rolls-Royce RB211 Trent 800 series engines installed on Boeing 777 aircraft. It mandates compliance with the updated Time Limits Manual (TLM) Revision 59 dated 07 February 2025, which defines mandatory maintenance tasks and life limits for critical engine parts. This directive ensures continued airworthiness by enforcing updated maintenance requirements for these engines.

Mar 31, 2025
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg RB211 TRENT 800

EASA AD 2025-0067

Fuselage — Centre Fuselage Frame Foot Joint — Inspection

EASA Airworthiness Directive 2025-0067 is an airworthiness directive addressing the Airbus A321-251NX, A321-252NX, A321-253NX, A321-271NX, and A321-272NX aeroplanes up to manufacturer serial number 09287 with Airbus modification 160286. It mandates inspections of the centre fuselage frame foot joint fastener holes to detect potential cracks that could affect structural integrity. The directive provides inspection intervals and corrective actions to maintain airworthiness.

Mar 28, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A321

EASA AD 2025-0066

Fuselage — Pressure Panel at Centre Wing Box — Inspection

EASA Airworthiness Directive 2025-0066 is an airworthiness directive issued by EASA concerning Airbus A319, A320, and A321 aeroplanes with specific modifications embodied in production. It mandates inspections of the pressure panel at the centre wing box to detect potential fatigue-related cracks. The directive applies to various Airbus A319, A320, and A321 models up to manufacturer serial number 09287, excluding certain CEO aeroplanes with specific mods.

Mar 28, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A319Airbus A320Airbus A321

EASA AD 2025-0068

SUPERSEDED BY EASA AD 2026-0017

EASA Airworthiness Directive 2025-0068 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes. It addresses inspection and modification requirements for forward-facing galleys with specific part numbers to prevent damage-related failures that could compromise galley integrity during emergency landings. The directive mandates inspections and corrective actions to ensure galley safety and compliance.

Mar 28, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2025-0069

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

The Time Limits / Maintenance Checks — Engine Time Limits Manual — Amendment is an update concerning the RB211 Trent 900 engine model manufactured by ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG. This document addresses time limits and maintenance check requirements for these engines, which are commonly used on certain wide-body aircraft. It provides revised guidance to ensure continued airworthiness and operational safety.

Mar 28, 2025
AmendmentMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg RB211 TRENT 900

EASA AD 2025-0070

Wings — Inboard Upper Wing Skin Under Engine Nacelle — Inspection

EASA Airworthiness Directive 2025-0070 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus Defence and Space S.A. C-212 aeroplanes, specifically models C-212-CB through C-212-VA. The directive mandates inspections of the inboard upper wing skin under the engine nacelle, part number 212-13103-05.3, due to detected intergranular corrosion. This corrosion poses a risk to the structural integrity of the affected aircraft.

Mar 28, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Defence & Space C-212

EASA AD US-2025-04-03

Exhaust - Primary Exhaust Nozzle - Inspection / Installation

The document titled "Exhaust - Primary Exhaust Nozzle - Inspection / Installation" is a regulatory guideline focused on the inspection and installation procedures for primary exhaust nozzles in aircraft engines. It addresses maintenance standards to ensure the integrity and proper functioning of exhaust components, which are critical for engine performance and safety. The document is intended for aviation maintenance professionals and operators involved with engine upkeep.

Mar 27, 2025
OtherMaintenanceSafety MgmtBoeing 737

EASA AD 2025-0065

Fuselage — Angle Fitting Connection to Side Skin Panel and Transition Angle — Inspection

The document titled 'Fuselage — Angle Fitting Connection to Side Skin Panel and Transition Angle — Inspection' is an inspection directive applicable to the Airbus A320 aircraft. It addresses the structural integrity of the angle fitting connections between the side skin panel and the transition angle on the fuselage. The directive aims to ensure continued airworthiness by mandating specific inspection procedures.

Mar 27, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A320

EASA AD US-2025-04-01

Powerplant - Inlet Cowl Aft Bulkhead Fasteners - Inspection / Replacement

Powerplant - Inlet Cowl Aft Bulkhead Fasteners - Inspection / Replacement is a regulatory document addressing the inspection and replacement requirements for the fasteners located on the aft bulkhead of the inlet cowl in aircraft powerplants. The document aims to ensure the structural integrity and safety of these components, although specific aircraft types or engine models are not clearly identified in the text provided.

Mar 27, 2025
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 737

EASA AD US-2025-04-02

[Correction] Powerplant - Fan Cowl Support Beam Hinge Fittings - Replacement / Radial Restraint Assembly - Modification / External Doubler at Starter Vent - Installation

Correction to Airworthiness Directive 2025-04-02 issued by the Federal Aviation Administration (FAA) addresses The Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes. The directive involves replacement of fasteners on fan cowl support beam hinge fittings, modification of the radial restraint assembly, and installation of an external doubler at the starter vent or optionally installing a serviceable fan cowl. It also requires revising maintenance programs to incorporate new airworthiness limitations related to fan blade out conditions and engine nacelle maintenance errors.

Mar 25, 2025
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 737

EASA AD 2025-0064

Engine Exhaust — Ejector Duct — Inspection

EASA Airworthiness Directive 2025-0064 is an airworthiness directive addressing inspection requirements for the engine exhaust ejector ducts on Leonardo S.p.A. AW189 helicopters. It applies to ejector ducts with part numbers 8G7810P00131 (left-hand side) and 8G7810P00231 (right-hand side) installed on all serial numbers of AW189 helicopters. The directive mandates repetitive inspections to detect cracking and potential damage that could affect flight safety.

Mar 25, 2025
Airworthiness DirectiveMaintenanceSafety MgmtLeonardo S.P.A. Helicopters AW189

EASA AD US-2025-05-16

Fuselage - Skin under the Drag Link Assembly - Inspection

The document titled 'Fuselage - Skin under the Drag Link Assembly - Inspection' is a regulatory directive focusing on the inspection requirements for the fuselage skin located beneath the drag link assembly. The document aims to ensure the structural integrity of this specific aircraft component, although no specific aircraft types, engine models, or part numbers are mentioned.

Mar 25, 2025
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 737

EASA SIB CASA-2025-02

Collective Pitch Transducers Part Number 412-074-101-103/-107 causing Engine Parameter Oscillations and Full Authority Digital Engine Control (FADEC) Faults

The Transport Canada Civil Aviation Safety Alert (CASA) titled "Collective Pitch Transducers Part Number 412-074-101-103/-107 causing Engine Parameter Oscillations and Full Authority Digital Engine Control (FADEC) Faults" addresses issues affecting Bell Textron Canada Limited (BTCL) Model 407 helicopters. The alert informs owners, operators, and maintainers about engine parameter oscillations and FADEC faults linked to specific collective pitch transducers (CPT) part numbers 412-074-101-103 and 412-074-101-107 installed on these helicopters.

Mar 24, 2025
Safety Information BulletinMaintenanceSafety MgmtBell 407

EASA AD CF-2025-18

Fuselage — Harness Low Clearance Condition in the AFT Fuselage Below Floor

Canadian Airworthiness Directive CF-2025-18 addresses a low clearance condition involving the hydraulic motor pump harness in the aft fuselage below the floor on Airbus Canada Limited Partnership (ACLP) Model BD-500-1A10 and BD-500-1A11 aircraft. This directive mandates modifications to the harness installation to prevent potential chafing and ignition risks. The affected aircraft include serial numbers 50001 through 50065 and 50067 through 50069 for the BD-500-1A10, and serial numbers 55001 through 55230, 55232, 55233, 55235, 55236, 55238, 55240, and 55242 through 55246 for the BD-500-1A11.

Mar 24, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus BD-500 (A220 Series)

EASA AD US-2025-06-02

Wings - Upper Wing Skin Common to Certain Fasteners - Repetitive Inspections

The document titled 'Wings - Upper Wing Skin Common to Certain Fasteners - Repetitive Inspections' is an airworthiness directive addressing the need for ongoing inspections of the upper wing skin area related to specific fasteners. It applies to aircraft models equipped with these wing components, ensuring structural integrity through repetitive checks.

Mar 24, 2025
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 777

EASA AD ISR-I-78-2025-03-01

Changes to the 1124 & 1124A Westwind models AFMs

Airworthiness Directive ISR I-78-2025-03-01 is issued by the Civil Aviation Authority of Israel and applies to all 1124 and 1124A Westwind aircraft models. This directive mandates changes to the Aircraft Flight Manuals (AFMs) of these models to address the thrust reverser system's status and function during flight. The directive ensures that thrust reverser deployment is prohibited before landing to enhance flight safety.

Mar 20, 2025
Airworthiness DirectiveFlight OpsSafety MgmtIsrael Aerospace Industries 1124