EASA Regulations & Airworthiness Directives

Browse 5,125 EASA regulations with AI-powered summaries.

Aircraft:AllAirbus A320286Airbus A321285Airbus A319253Airbus A350222Airbus A330220Airbus A318189Airbus A380182Boeing 737175Airbus A340141Airbus A350-941132Airbus BD-500 (A220 Series)123Airbus Helicopters AS 332119Airbus Helicopters EC 225116Airbus Helicopters SA 330116Boeing 787114Show all...

EASA AD CF-2026-34

Jul 16, 2026

Water/Waste – Waste Service Panel Ball Valve Leakage - Installation

Canadian Airworthiness Directive CF-2026-34 addresses a corrosion issue caused by leakage from the waste service panel ball valve on Airbus Canada Limited Partnership (ACLP) aircraft models BD-500-1A10 and BD-500-1A11. The directive applies to specific serial numbers of these models and mandates corrective action to prevent structural damage. This directive aims to enhance aircraft safety by preventing waste water leakage that can lead to cabin pressure loss or structural failure.

Airworthiness Directive
  • Airbus BD-500 (A220 Series)
  • Airbus Canada BD-500-1A10
  • Airbus Canada BD-500-1A11

EASA AD 2026-0140

Jul 15, 2026

Flight Controls – Flap Actuator – Inspections / Modification

EASA Airworthiness Directive 2026-0140 is an airworthiness directive affecting all serial numbers of Diamond Aircraft Industries GmbH DA 50 C aeroplanes. It addresses issues with the flap actuator that could cause flap extension failure and reduced aileron control. The directive mandates inspections and modifications to the flap actuator to ensure continued safe operation.

Airworthiness Directive
  • Diamond Aircraft Industries DA 50
  • Diamond Aircraft Industries GmbH DA 50 C

EASA PAD 26-085

Jul 15, 2026

Navigation – GLU-2100 Global Navigation Satellite System Clock Oscillator – Operational Limitation

EASA Airworthiness Directive PAD No. 26-085 is a proposed directive addressing an operational limitation for the GLU-2100 Global Navigation Satellite System Clock Oscillator installed on Airbus A350-941 and A350-1041 aeroplanes. It identifies certain affected GLU-2100 units with specific part and serial numbers that may cause erroneous aircraft position information without warning. The directive applies to all manufacturer serial numbers of these aircraft models.

Proposed AD
  • Airbus A3509411041

EASA AD G-2026-0002

Jul 15, 2026

Time Limits / Maintenance Checks – Airworthiness Limitations – Amendment / Implementation

The Civil Aviation Authority Airworthiness Directive G-2026-0002 is an amendment addressing time limits and maintenance checks for BAE Systems Jetstream 4100 series aeroplanes. It updates mandatory airworthiness limitations and structural repair inspections to ensure continued safe operation of these aircraft. This directive applies to all models and serial numbers of the Jetstream 4100 series.

Airworthiness Directive
  • Bae Systems (Operations) Jetstream 4100
  • BAE Systems Jetstream 4100

EASA AD 2026-0139

Jul 14, 2026

Air Conditioning – Air Distribution / Air Recirculation Fans – Inspection(s)

EASA Airworthiness Directive 2026-0139 is an airworthiness directive addressing inspection requirements for air distribution and air recirculation fans installed on SAAB SF340A and 340B aeroplanes. It specifically targets recirculation fans with part numbers EVCTA465, EVCTA465A, and EVCTA465B due to potential electrical arcing issues. The directive mandates inspections and possible replacement of affected parts to ensure continued airworthiness and safety.

Airworthiness Directive
  • Saab Ab 340
  • SAAB SF340A
  • SAAB SF340B

EASA CZIB CZIB-2026-07R2

Jul 14, 2026

Airspace of the Persian Gulf and Gulf of Oman

The EASA Conflict Zone Information Bulletin (CZIB) titled 'Airspace of the Persian Gulf and Gulf of Oman' addresses the high risks to civil aviation in the airspace of Bahrain, Kuwait, Qatar, Oman, and the United Arab Emirates due to ongoing regional military tensions. It applies to all altitudes and flight levels within the specified FIRs and affects air operators subject to Commission Regulation (EU) 965/2012 and third Country Operators authorized by EASA. The bulletin highlights the dangers posed by missile and drone activity, military operations, and the volatile security situation following the US-Iran conflict.

Safety Information Bulletin
All aircraft

EASA AD US-2026-14-11

Jul 13, 2026

Air Conditioning - AFM Operating Procedures - Amendment

The document titled Air Conditioning - AFM Operating Procedures - Amendment is a regulatory amendment concerning the operating procedures related to aircraft air conditioning systems as outlined in the Aircraft Flight Manual (AFM). The amendment aims to update or clarify procedures to ensure proper operation and safety of the air conditioning systems. Specific aircraft types or engine models affected are not explicitly mentioned in the document.

Other
  • Boeing 737

EASA AD 2026-0138

Jul 13, 2026

Landing Gear – Main Landing Gear Axle Beam – Inspection

EASA Airworthiness Directive 2026-0138 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all Dassault Aviation Falcon 6X aeroplanes. It addresses inspection requirements for the main landing gear axle beam, specifically concerning potential interference with certain brake assemblies. The directive mandates inspection and replacement actions to ensure continued airworthiness and safety of the landing gear components.

Airworthiness Directive
  • Dassault Falcon 6X

EASA PAD 26-084

Jul 13, 2026

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

EASA Airworthiness Directive PAD No. 26-084 is a proposed amendment concerning the time limits and maintenance checks for Rolls-Royce Deutschland Ltd & Co KG RB211 Trent 900 engines, specifically models RB211 Trent 970-84, 972-84, and 972E-84, commonly installed on Airbus A380 aircraft. This directive updates the Airworthiness Limitations Section (ALS) within the Rolls-Royce Time Limits Manual Revision 70 to ensure continued airworthiness of these engines. It mandates compliance with new and more restrictive maintenance tasks and life limits to address potential unsafe conditions.

Proposed AD
  • Rolls-Royce Deutschland Ltd & Co Kg RB211 TRENT 900
  • Airbus A380

EASA AD 2026-0137

Jul 10, 2026

Doors – Door Locking Mechanism – Modification

EASA Airworthiness Directive 2026-0137 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Pipistrel Vertical Solutions d.o.o. Virus SW 121 and SW 128 aeroplanes. It addresses a safety issue related to the door locking mechanism on these aircraft models. The directive mandates modifications to the door locking mechanism to prevent potential in-flight door detachment.

Airworthiness Directive
  • Pipistrel Vertical Solutions D.O.O. Virus SW
  • Pipistrel Virus SW 121
  • Pipistrel Virus SW 128

EASA AD 2026-0136

Jul 10, 2026

Flights Controls – Trimmable Horizontal Stabilizer Actuator Ballscrew Lower Splines – Inspection / Replacement

EASA Airworthiness Directive 2026-0136 is an airworthiness directive addressing corrosion issues in the trimmable horizontal stabilizer actuator (THSA) ballscrew lower splines on Airbus A318, A319, A320, and A321 aircraft. It applies to specific THSA part numbers that may suffer corrosion leading to potential loss of control of the airplane. The directive mandates inspections and possible replacement of affected parts to ensure continued airworthiness.

Airworthiness Directive
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2026-0135

Jul 9, 2026

Fuselage – Rear Fuselage – Inspections

EASA Airworthiness Directive 2026-0135 is an airworthiness directive affecting Airbus A330 aircraft modified under EASA Supplemental Type Certificate 10063798 for passenger to freighter conversion. It mandates inspections and modifications related to the rear fuselage to address potential structural integrity issues caused by differences in fastener sizes between the STC design and Airbus Service Bulletin requirements.

Airworthiness Directive
  • Airbus A330

EASA SIB BEA-2026-03

Jul 9, 2026

Operation in Icing Conditions

BEA 2026-03 is a Special Airworthiness Bulletin providing guidance on the operation of the ice protection system for Embraer EMB-500 aircraft. It addresses the importance of correctly using the wing and horizontal stabilizer de-ice system during icing conditions to maintain safe stall warning thresholds and approach speeds. The bulletin offers non-mandatory recommendations to operators, training centers, and owners to ensure proper system use and ice contamination verification.

Safety Information Bulletin
  • Embraer EMB-500 (Phenom 100)
  • Embraer EMB-500

EASA CZIB CZIB-2026-04-R1

Jul 8, 2026

Airspace of Iran

The document titled 'Airspace of Iran' is a safety information bulletin issued by EASA concerning the FIR Tehran (OIIX) airspace at all altitudes and flight levels. It highlights the high risks to civil aviation due to ongoing military conflicts and tensions involving Iran, including recent military strikes and retaliatory actions. The bulletin applies to air operators subject to Commission Regulation (EU) 965/2012 and third country operators authorized by EASA operating to, from, or within the EU.

Safety Information Bulletin
All aircraft

EASA CZIB CZIB-2026-05-R1

Jul 8, 2026

Airspace of Iraq

The document titled Airspace of Iraq is a Conflict Zone Information Bulletin (CZIB) issued by EASA concerning the FIR Baghdad (ORBB) airspace at all altitudes and flight levels. It highlights ongoing high risks to civil aviation due to military conflicts involving Iran, the United States, and Israel, as well as the presence of Iranian-backed militant groups and violent non-state actors in Iraqi airspace. The bulletin applies to all air operators subject to Commission Regulation (EU) 965/2012 and third country operators authorized by EASA operating in the affected airspace.

Safety Information Bulletin
All aircraft

EASA CZIB CZIB-2026-06-R1

Jul 8, 2026

Airspace of Lebanon

The EASA Conflict Zone Information Bulletin (CZIB) titled 'Airspace of Lebanon' addresses the high-risk conditions in the FIR Beirut (OLBB) airspace at all altitudes and flight levels due to ongoing military tensions in the region. It applies to air operators subject to Commission Regulation (EU) 965/2012 and third Country Operators authorized by EASA conducting operations in this airspace. The bulletin highlights that operations are only considered sufficiently mitigated when approaches start from the sea and departures end over the sea to Beirut International Airport.

Safety Information Bulletin
All aircraft

EASA AD 2026-0134

Jul 8, 2026

Flight Controls – Elevator Aileron Computer – Replacement

EASA Airworthiness Directive 2026-0134 is an airworthiness directive addressing the replacement of the Elevator Aileron Computer (ELAC) on Airbus A319, A320, and A321 aeroplanes. It applies to specific ELAC part numbers associated with these aircraft models and aims to ensure continued safe flight control operation. The directive updates previous requirements related to ELAC replacement and installation.

Airworthiness Directive
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2026-0133

Jul 8, 2026

Fuselage – Centre Fuselage Forward Pressure Bulkhead – Inspection

EASA Airworthiness Directive 2026-0133 is an airworthiness directive addressing inspection requirements for the centre fuselage forward pressure bulkhead on Airbus A318, A319, A320, and A321 aeroplanes. It applies to various models and serial numbers except those with specific Airbus modifications embodied in production or service. The directive mandates repetitive rototest inspections of the forward pressure bulkhead hole C1 and provides an optional terminating modification.

Airworthiness Directive
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2026-0052R1

Jul 8, 2026

Instruments – Fuse Cover Attachment of Circuit Breaker Panel – Modification

EASA Airworthiness Directive 2026-0052R1 is a regulatory update addressing a safety issue in Airbus Helicopters AS 350 B2, AS 350 B3, and EC 130 B4 models. The directive mandates modification of the fuse cover attachment on the circuit breaker panel to prevent interference with the pilot pedal, which could impair yaw control. This AD applies to specific affected parts identified by part numbers and requires compliance with updated service bulletin instructions.

Airworthiness DirectiveSuperseded
  • Airbus Helicopters AS 350
  • Airbus Helicopters EC 130
  • Airbus Helicopters AS 350 B2
  • Airbus Helicopters AS 350 B3
  • Airbus Helicopters EC 130 B4