EASA Regulations &amp; Airworthiness Directives

Safety Information Bulletin

Airspace of Iran

The document titled Airspace of Iran is a Conflict Zone Information Bulletin (CZIB) issued by EASA concerning the FIR Tehran (OIIX) airspace at all altitudes and flight levels. It highlights the elevated risks to civil aviation due to ongoing military conflicts and tensions between Iran, the United States, and Israel, including retaliatory attacks and military activities that increase the likelihood of misidentification and threats to aircraft. The bulletin applies to all air operators subject to Commission Regulation (EU) 965/2012 and third country operators authorized by EASA operating in or through this airspace.

All aircraft

EASA CZIB CZIB-2026-05-R2

Safety Information Bulletin

Airspace of Iraq

The document titled Airspace of Iraq is a safety information bulletin issued by EASA concerning the FIR Baghdad (ORBB) airspace at all altitudes and flight levels. It highlights ongoing conflict-related risks due to military activities and the presence of violent non-state actors, affecting the safety of civil aviation operations in Iraqi airspace. The bulletin applies to EASA-regulated air operators and third-country operators authorized by EASA conducting flights to, from, or within the EU.

All aircraft

EASA CZIB CZIB-2026-06-R2

Safety Information Bulletin

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 to, from, or within the EU. 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 (BEY/OLBA).

All aircraft

EASA AD 2026-0134

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.

Airbus A319
Airbus A320
Airbus A321

EASA AD 2026-0133

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.

Airbus A318
Airbus A319
Airbus A320
Airbus A321

EASA AD 2026-0052R1

Airworthiness DirectiveSuperseded

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.

Airbus Helicopters AS 350
Airbus Helicopters EC 130
Airbus Helicopters AS 350 B2
Airbus Helicopters AS 350 B3
Airbus Helicopters EC 130 B4

EASA AD 2026-0132

Rotors Flight Control – Upper Ball Bearing End of the Main Rotor Servo-Controls – Inspection

EASA Airworthiness Directive 2026-0132 is an airworthiness directive addressing the inspection of the upper ball bearing ends of the main rotor servo-controls on Airbus Helicopters AS 350 B3, AS 355 (F, F1, F2, N, NP), and EC 130 (B4, T2) models. The directive mandates a one-time and recurring inspection of the nut tightening torque on affected parts to prevent potential disconnection of the upper ball bearing end from the main rotor servo-controls. This AD applies to specific part numbers equipped with certain nut retainers and aims to ensure continued safe flight control operation.

Airbus Helicopters AS 350
Airbus Helicopters EC 130
Airbus Helicopters AS 355
Airbus Helicopters AS 350 B3
Airbus Helicopters AS 355 F
Airbus Helicopters AS 355 F1
Airbus Helicopters AS 355 F2
Airbus Helicopters AS 355 N
Airbus Helicopters AS 355 NP
Airbus Helicopters EC 130 B4
Airbus Helicopters EC 130 T2

EASA AD 2025-0274R1

Jul 7, 2026

Fire Protection – Fire Panel – Inspection

EASA Airworthiness Directive 2025-0274R1 is a regulatory update addressing fire panel inspections on Airbus A318, A319, A320, and A321 aircraft. It targets specific fire panel part numbers that have been linked to incidents of engine fire switch self-releasing, which could cause uncommanded in-flight engine shutdowns. The directive mandates inspections, replacements, and installation requirements to ensure continued airworthiness and safety.

Airbus A318
Airbus A319
Airbus A320
Airbus A321

EASA AD US-2026-13-03

Jul 7, 2026

Fuselage - Stringers and Stringer Splice Fittings - Inspection

The Federal Aviation Administration's Airworthiness Directive 2026-13-03 addresses certain Boeing 747-8F series airplanes. This directive mandates inspections of fuselage stringers and stringer splice fittings for cracking and the presence of radius fillers at specific fastener locations. It also requires applicable on-condition actions to ensure continued airworthiness.

Boeing 7478F

EASA AD 2025-0158R2

Jul 7, 2026

Landing Gear – Main Landing Gear Door Actuators – Inspections

EASA Airworthiness Directive 2025-0158R2 is an updated regulatory requirement addressing inspections and corrective actions for main landing gear door actuators on Airbus A318, A319, A320, and A321 aircraft models. It targets actuators with specific part number 114122015 and serial numbers listed in Airbus Alert Operators Transmission A32N033-24, aiming to prevent landing gear extension issues caused by actuator assembly errors. The directive mandates repetitive inspections and eventual replacement or modification of affected parts to ensure continued airworthiness.

Airbus A318
Airbus A319
Airbus A320
Airbus A321

EASA AD US-2026-13-05

Air Conditioning - AFM Operating Procedures - Amendment

The Air Conditioning - AFM Operating Procedures - Amendment is an updated regulatory document concerning the Boeing 737 aircraft type. It provides revised operating procedures related to the air conditioning systems as specified in the Aircraft Flight Manual (AFM). This amendment aims to ensure continued safe and efficient operation of the affected Boeing 737 models.

Other

Boeing 737

EASA AD 2026-0130

Airworthiness DirectiveSuperseded

Electrical Systems Installation – Battery Retaining Rods – Identification / Replacement

EASA Airworthiness Directive 2026-0130 is an airworthiness directive addressing battery retaining rods on Airbus A318, A319, A320, and A321 aeroplanes. It mandates inspections and potential replacement or reidentification of affected battery retaining rods with Part Number D9241023700000 to prevent battery displacement and associated electrical system failures.

Airbus A318
Airbus A319
Airbus A320
Airbus A321

EASA AD 2026-0131

Engine Fuel & Control – Electronic Engine Control Unit – Software Update; Engine Fuel & Control – Preference Injector – Non-extinguishing Test / Replacement

EASA Airworthiness Directive 2026-0131 addresses safety concerns for SAFRAN Helicopter Engines ARRIUS 2B2 engines, commonly installed on Airbus Helicopters Deutschland EC135 and EC635 models. The directive mandates software updates to the Electronic Engine Control Unit and introduces non-extinguishing tests and replacement requirements for the preference injector component. These measures aim to prevent engine flameouts caused by fuel coking and injector clogging.

Safran ARRIUS 2
Airbus Helicopters EC135
Airbus Helicopters EC635

EASA PAD 26-083

Time Limits / Maintenance Checks – Airworthiness Limitations Section – Amendment

EASA Airworthiness Directive PAD No. 26-083 is a proposed amendment addressing time limits and maintenance checks in the Airworthiness Limitations Section for CFM INTERNATIONAL CFM56-7B engines installed on Boeing 737-600, 737-700, 737-800, 737-900, and 737-900ER aircraft. The directive updates mandatory life limits and inspection tasks to ensure continued airworthiness of these engines. It applies to all serial numbers of multiple CFM56-7B engine variants.

Proposed AD

CFM International CFM56-7B
Boeing 737-600
Boeing 737-700
Boeing 737-800
Boeing 737-900
Boeing 737-900ER

EASA AD 2025-0094R1

Airworthiness DirectiveSuperseded

Electrical Power – Overhead Panel Wires Interference – Inspection / Modification

EASA Airworthiness Directive 2025-0094R1 is issued for Leonardo S.p.A. AB139 and AW139 helicopters, addressing interference issues between electrical cables and connectors in the overhead panel. The directive mandates inspections and modifications to prevent potential cable damage that could lead to fire and loss of helicopter control. It applies to all serial numbers from 31201 onward, focusing on Long Nose helicopter configurations.

Leonardo S.P.A. Helicopters AB139
Leonardo S.P.A. Helicopters AW139
Leonardo AB139
Leonardo AW139

EASA AD 2025-0171R2

Engine – High Pressure Turbine Rotor Stage 1 Blade – Inspection

EASA Airworthiness Directive 2025-0171R2 is an updated regulatory requirement addressing inspections of high pressure turbine (HPT) rotor stage 1 blades on CFM International LEAP-1A engines installed on certain Airbus A319, A320, and A321 aircraft. The directive mandates repetitive borescope inspections of specific affected turbine blades to detect cracks and prevent potential in-flight engine failures. It applies to multiple LEAP-1A engine variants and specifies affected part numbers for inspection and corrective actions.

CFM International LEAP-1A
CFM International LEAP-1C
Airbus A319
Airbus A320
Airbus A321

EASA AD CF-2026-26

Fuselage – Corrosion on Waste Box, Waste Access Doubler and Waste Service Door of Aft Waste Service Port

The Canadian Airworthiness Directive CF-2026-26 addresses corrosion issues on the waste box, waste access doubler, and waste service door of the aft waste service port on Airbus Canada Limited Partnership (ACLP) aircraft models BD-500-1A10 and BD-500-1A11. This directive mandates inspections, repairs, and application of protective coatings to prevent structural damage caused by corrosion. It applies to aircraft with specific serial numbers ranging from 50001 to 50047 for BD-500-1A10 and 55001 to 55063 for BD-500-1A11.

Airbus BD-500 (A220 Series)
Airbus Canada Limited Partnership BD-500-1A10
Airbus Canada Limited Partnership BD-500-1A11

EASA AD 2026-0129

Main Rotor Drive – Main Gearbox Flexible Mounting Plate – Maintenance Task

EASA Airworthiness Directive 2026-0129 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus Helicopters AS 332 C, C1, L, and L1 models. It mandates maintenance on the main gearbox flexible mounting plate, specifically part numbers 332A38010600 and 332A38010620, to ensure proper torque on attachment bolts. This directive addresses a maintenance task correction related to helicopters performing external load transport with loads of 2.5 tons or less.

Airbus Helicopters SA 330
Airbus Helicopters AS 332
Airbus Helicopters EC 225
Airbus Helicopters AS 332 C
Airbus Helicopters AS 332 C1
Airbus Helicopters AS 332 L
Airbus Helicopters AS 332 L1

EASA AD 2026-0123

Time Limits / Maintenance Checks – Airworthiness Limitations Section – Amendment

EASA Airworthiness Directive 2026-0123 is an amendment concerning time limits and maintenance checks in the Airworthiness Limitations Section for GE Aviation Czech H75, H80, and H85 engine models. This directive applies to these engines installed on aircraft such as the Aircraft Industries L410-UVP-E20, L410-NG, Do 28 series, Thrush S-2R series, and Viking Air DHC-3 Otter. It mandates compliance with updated maintenance tasks and life limits to ensure continued airworthiness.