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EASA Regulations & Airworthiness Directives

Browse 175 EASA regulations with AI-powered summaries.

Aircraft:All Airbus A320286 Airbus A321285 Airbus A319253 Airbus A350222 Airbus A330220 Airbus A318189 Airbus A380182 Boeing 737175 Airbus A340141 Airbus A350-941132 Airbus BD-500 (A220 Series)123 Airbus Helicopters AS 332119 Airbus Helicopters EC 225116 Airbus Helicopters SA 330116 Boeing 787114 Show all...

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EASA AD US-2025-02-02

Fuselage - Frame Inner Chord and Web at Station (STA) 727 - Inspections

The Federal Aviation Administration's Airworthiness Directive 2025-02-02 is a final rule addressing all Boeing 737-100, -200, -200C, -300, -400, and -500 series airplanes. It mandates inspections of the fuselage frame inner chord and web at station 727 to detect cracks and requires applicable on-condition repair actions. This directive aims to ensure structural integrity by preventing cracks from compromising principal structural elements.

Airworthiness Directive

Boeing 737

EASA AD US-2025-02-07

Navigation - Aeroplane Flight Manual - Revision / Software Installation

Airworthiness Directive 2025-02-07 is a final rule issued by the Federal Aviation Administration addressing certain Boeing airplanes including Model MD-11, MD-11F, 717-200, 737-600 through 737-9 series, 747-400 series, 757, 767, and 777. The directive focuses on updating the Aeroplane Flight Manual and installing updated multimode receiver (MMR) operational software to address issues with Coordinated Universal Time calculation errors and simultaneous MMR resets. This affects airplanes equipped with Collins GLU-2100 MMR part number 822-2532-100 with software versions earlier than COL4C-0087-0003.

Airworthiness Directive

Boeing 717
Boeing 737
Boeing 747
Boeing 757
Boeing 767
Boeing 777
Boeing MD-11

EASA AD US-2024-23-03

Flight Controls - Cruise Thrust Split Monitor (MONFD) of the Autothrottle (A/T) System - Inspection / Replacement

Flight Controls - Cruise Thrust Split Monitor (MONFD) of the Autothrottle (A/T) System - Inspection / Replacement is a regulatory document addressing the inspection and replacement procedures for the Cruise Thrust Split Monitor component within the Autothrottle system. The document aims to ensure the proper functioning of the autothrottle system to maintain safe flight operations. Specific affected aircraft types, engine models, or part numbers are not clearly identified in the provided text.

Airworthiness Directive

Boeing 737

EASA AD US-2024-23-11

Flight Controls - Spoiler Control Wire Bundles - Inspection

Flight Controls - Spoiler Control Wire Bundles - Inspection is a regulatory document addressing the inspection requirements for spoiler control wire bundles in aircraft flight control systems. The document aims to ensure the integrity and proper functioning of these wire bundles to maintain flight safety. Specific aircraft types or engine models affected are not explicitly mentioned in the provided content.

Airworthiness Directive

Boeing 737

EASA AD US-2024-18-08

Equipment / Furnishings - Galley Wire Bundle Spiral Wrap Sleeving - Identification / Replacement

The document titled Equipment / Furnishings - Galley Wire Bundle Spiral Wrap Sleeving - Identification / Replacement is a regulatory communication addressing the identification and replacement procedures for spiral wrap sleeving used in galley wire bundles. It focuses on ensuring the proper condition and compliance of these components to maintain safety and functionality in aircraft galleys. The document does not specify particular aircraft types or engine models affected.

Boeing 737

EASA AD US-2024-19-06

Ice/Rain Protection System - Standby Power System Control Unit - Installation / Power Tests

The Federal Register document titled "Ice/Rain Protection System - Standby Power System Control Unit - Installation / Power Tests" is a final rule airworthiness directive (AD 2024-19-06) issued by the FAA. It applies to certain Boeing 737-8 and 737-9 airplanes and addresses a design issue in the standby power system control unit (SPCU) that poses a risk of single point failure. The directive mandates installation of four diodes, wiring bundle changes in the P5 panel, and subsequent installation and power tests to mitigate the unsafe condition.

Airworthiness Directive

Boeing 737

EASA AD US-2024-18-07

Equipment / Furnishings - Support Brackets of the Air Conditioning Outlet Extrusions between Body Station 360 and BS 907 - Inspections / Modification

The document titled 'Equipment / Furnishings - Support Brackets of the Air Conditioning Outlet Extrusions between Body Station 360 and BS 907 - Inspections / Modification' is a regulatory directive addressing the inspection and modification requirements for support brackets of air conditioning outlet extrusions on certain aircraft. It focuses on ensuring the structural integrity and proper functioning of these components to maintain air conditioning system reliability. The document does not specify particular aircraft types or engine models affected.

Airworthiness Directive

Boeing 737

EASA AD US-2024-16-10

Indicating / Recording System - Aeroplane Flight Manual / Display Unit Software Errors - Installation of New Software

The document titled 'Indicating / Recording System - Aeroplane Flight Manual / Display Unit Software Errors - Installation of New Software' is a regulatory communication addressing issues related to software errors in aeroplane flight manual display units. It focuses on the installation of new software to mitigate these errors. The document does not specify particular aircraft types, engine models, or part numbers affected.

Safety Information Bulletin

Boeing 737

EASA SIB SAFO24006

Potential for Jammed or Restricted Rudder on Boeing Model 737 Series Airplanes Equipped with Optional Collins Aerospace SVO-730 Rudder Rollout Guidance Actuators (RRGA).

The Safety Alert for Operators SAFO 24006 notifies operators of Boeing 737 series airplanes, including the 737-600/-700/-800/-900/-900ER (737NG) and 737-8/-8200/-9 (737 MAX) models, equipped with optional Collins Aerospace SVO-730 Rudder Rollout Guidance Actuators (RRGA) about the potential for jammed or restricted rudder movement. This condition may occur due to moisture freezing inside the actuator, which can limit rudder control during flight or landing rollout. The alert provides important safety information and recommended procedures to address this issue.

Safety Information Bulletin

Boeing 737

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.

Airworthiness Directive

Boeing 737898200700800900ER

EASA AD US-2024-06-01

Fuselage - Skin and Bear Strap at the Forward Galley Door Cutout - Inspection

Federal Aviation Administration Airworthiness Directive 2024-06-01 is a final rule addressing certain Boeing 737-600, -700, -700C, -800, -900, and -900ER airplanes. It mandates inspections of the fuselage skin and bear strap at the forward galley door cutout forward upper corner due to reported cracks caused by high operating stresses. The directive aims to ensure structural integrity and prevent potential rapid decompression.

Airworthiness Directive

Boeing 737600700700C800900900ER

EASA AD US-2024-06-03

Electrical Power - P6 Panel / Standby Power Control Unit - Installation

Airworthiness Directive 2024-06-03 is a final rule issued by the Federal Aviation Administration (FAA) addressing certain Boeing 737-8 and 737-9 airplanes. It mandates the installation of two bonding jumpers from the P6 panel structure to the primary structure to prevent failure of the standby power control unit (SPCU). This directive aims to maintain critical flightcrew instrumentation and displays by ensuring redundant grounding paths.

Airworthiness Directive

Boeing 73789

EASA AD 2024-0067-E

Engine — Life Limited Parts — Replacement

EASA Airworthiness Directive 2024-0067-E is an emergency directive addressing life limited parts replacement for CFM International CFM56 series engines, including models CFM56-2, -3, -5, -5B, -5C, and -7B. These engines are commonly installed on Airbus A318, A319, A320, A321, A340, and Boeing 737 series aircraft from the 300 to 900ER variants. The directive targets specific compressor discharge pressure seals, high-pressure compressor stage 3 disks, and high-pressure turbine rear shafts identified as affected parts due to potential damage from improper maintenance.

Airworthiness Directive

CFM International CFM56-2
CFM International CFM56-3
CFM International CFM56-5
CFM International CFM56-5B
CFM International CFM56-5C
CFM International CFM56-7B
Airbus A318
Airbus A319
Airbus A320
Airbus A321
Airbus A340
Boeing 737

EASA AD US-2024-03-04

Flight Controls - Aft Rudder Quadrant - Inspection

Airworthiness Directive 2024-03-04 is a final rule issued by the Federal Aviation Administration (FAA) addressing certain Boeing 737-8, 737-8200, and 737-9 airplanes. It mandates a one-time inspection of the aft rudder quadrant due to a reported missing washer and nut and a migrated bolt, which could compromise rudder control. The directive aims to ensure continued safe flight by correcting this unsafe condition.

Airworthiness Directive

Boeing 737882009

EASA AD US-2024-01-06

Fuselage - Skin Repairs at Stringer S—17 - Repetitive Inspections

Federal Aviation Administration Airworthiness Directive 2024-01-06 is a final rule addressing certain Boeing 737-600, 737-700, and 737-800 series airplanes. It mandates repetitive inspections of fuselage skin repairs at Stringer S-17 to detect cracks and requires corrective actions if necessary. This directive aims to ensure continued airworthiness by preventing fatigue cracking that could compromise structural integrity.

Airworthiness Directive

Boeing 737600700800

EASA SIB SAFO24001

Boeing 737-900ER Mid-Cabin Door Plug Inspection

The Safety Alert for Operators SAFO 24001 titled Boeing 737-900ER Mid-Cabin Door Plug Inspection informs operators about inspection recommendations for the Boeing 737-900ER fuselage plug assembly. It highlights the similarity between the 737-900ER and the 737-9 MAX mid-cabin door plug designs and addresses safety concerns following an incident involving a 737-9 MAX. The document applies to all operators under 14 CFR Parts 91, 91K, 121, 125, 129, and 135 operating the Boeing 737-900ER aircraft.

Safety Information Bulletin

Boeing 737

EASA AD US-2024-02-51

[Final Rule] Doors - Mid-Cabin Door Plug - Inspection

The Final Rule titled 'Doors - Mid-Cabin Door Plug - Inspection' approves a Method of Compliance (MOC) to FAA Emergency Airworthiness Directive 2024-02-51 for Boeing Model 737-9 airplanes equipped with a mid-cabin door plug. This rule provides specific inspection instructions and corrective actions to ensure the mid-cabin door plug meets type design requirements. It applies exclusively to the Boeing 737-9 aircraft listed in the referenced AD.

Boeing 7379

EASA AD US-2023-13-05

Fuselage - Skin Lap Splices - Inspection / Repair

The Federal Aviation Administration's Airworthiness Directive 2023-13-05 addresses fuselage skin lap splice cracking on all Boeing 737-600, -700, -700C, -800, -900, and -900ER series airplanes. This directive requires inspections and repairs of specific skin lap splice areas at stations S-4, S-14, and S-24 to detect and mitigate cracking, buckling, wrinkling, or bulging. The AD aims to maintain the structural integrity of these aircraft by preventing fatigue-related damage in critical fuselage areas.

Airworthiness Directive

Boeing 737600700700C800900900ER

EASA AD US-2023-13-12

Oxygen - Chemical Oxygen Generators - Replacements

The Federal Aviation Administration's Airworthiness Directive 2023-13-12 addresses premature aging of certain passenger chemical oxygen generators installed on various Boeing aircraft models including the 737 series (100 through 900ER), 757 series, and 767 series airplanes. This final rule mandates repetitive replacement of affected chemical oxygen generators and restricts installation of certain parts to ensure safety during emergencies. The directive aims to prevent failure of oxygen generators to activate, which could jeopardize occupant safety.

Airworthiness Directive

Boeing 737
Boeing 757
Boeing 767

EASA AD US-2023-15-05

Airplane Flight Manual / Minimum Equipment List - Amendment

The Airplane Flight Manual / Minimum Equipment List - Amendment is a final rule airworthiness directive issued by the FAA affecting all Boeing Company Model 737 airplanes equipped with CFM International LEAP-1B series turbofan engines. It addresses an unsafe condition related to engine anti-ice use in dry air that can cause overheating and failure of the engine inlet inner barrel. The directive mandates revisions to the airplane flight manual and minimum equipment list to mitigate this risk.

Airworthiness Directive

Boeing 737