EASA Regulations & Airworthiness Directives

Browse 175 EASA regulations with AI-powered summaries.

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EASA SIB SAIB-2026-17

Oct 9, 2026

Vertical Navigation Approach Disconnect Following Missed Approach

The FAA Aviation Safety Information Bulletin SAIB: 2026-17 titled "Vertical Navigation Approach Disconnect Following Missed Approach" informs operators of Boeing 737-600/-700/-800/-900/-900ER/-7/-8/-9/-8200 series airplanes equipped with Flight Management Computer software versions U14.0 or U14.1 about a potential vertical navigation (VNAV) mode disconnect during subsequent approaches after a missed approach. This bulletin provides information on the anomaly but does not mandate any regulatory action.

Safety Information Bulletin

Boeing 7376007008 (MAX)8008200 (MAX)9 (MAX)900900ER7898200

EASA AD US-2026-18-07

Oct 7, 2026

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

The Federal Aviation Administration's Airworthiness Directive 2026-18-07 addresses certain Boeing Model 737-8, 737-9, and 737-8200 airplanes. This final rule mandates inspections and on-condition actions to detect and repair cracks in the fuselage skin, bear strap, and stub frame at the forward galley door cutout. The directive aims to maintain structural integrity and ensure continued airworthiness of affected aircraft.

Airworthiness Directive

Boeing 7378 (MAX)8200 (MAX)9 (MAX)898200

EASA PAD 26-113

Sep 23, 2026

Engine – High Pressure Turbine Front Seal – Inspection

EASA Airworthiness Directive Proposal 26-113 is a regulatory document addressing the inspection of the High Pressure Turbine (HPT) front seal on CFM INTERNATIONAL S.A. CFM56-5B and CFM56-7B engine models. These engines are commonly installed on Airbus A318, A319, A320, and A321 series aircraft, as well as Boeing 737-600, 737-700, 737-800, 737-900, and 737-900ER series aircraft. The directive proposes a one-time on-wing borescope inspection to detect potential misalignment and cracks in the HPT front seal to prevent uncontained part release and possible engine or aircraft damage.

Proposed AD

CFM International CFM56-5B
CFM International CFM56-7B
Airbus A318
Airbus A319
Airbus A320
Airbus A321
Boeing 737

EASA AD US-2026-15-11

Aug 7, 2026

Fuselage - Fuselage Skin / Bear Strap - Inspection

The Federal Aviation Administration's Airworthiness Directive 2026-15-11 addresses certain Boeing 737-8, 737-9, and 737-8200 airplanes. This directive requires inspections of the fuselage skin and bear strap near the forward galley door cutout due to reported cracks. The directive aims to maintain structural integrity and ensure safety by detecting and repairing cracks before they become critical.

Airworthiness Directive

Boeing 737898200

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 US-2026-13-05

Jul 6, 2026

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 US-2026-13-17

Jul 1, 2026

Navigation - 5G C-Band wireless Broadband Interference with Radio Altimeter System when operating in Canadian airspace - Amendment

Navigation - 5G C-Band wireless Broadband Interference with Radio Altimeter System when operating in Canadian airspace - Amendment is a Federal Aviation Administration (FAA) airworthiness directive addressing interference issues affecting Boeing 737-8, 737-9, and 737-8200 airplanes. This directive responds to increased 5G Lower C-Band interference in Canadian airspace that compromises radio altimeter reliability and impacts critical airplane systems during takeoff and landing. The amendment mandates updates to the airplane flight manual to restrict certain operations relying on radio altimeter data when flying in Canadian airspace.

Airworthiness Directive

Boeing 737898200

EASA AD US-2026-09-12

Jun 16, 2026

Fuselage - Aft Drain Mast Fuselage Skin - Inspections

The Federal Aviation Administration Airworthiness Directive 2026-09-12 is a final rule addressing certain Boeing 737-100, -200, -200C, -300, -400, and -500 series airplanes. It mandates repetitive inspections of the fuselage skin and structure around the aft drain mast to detect cracks or corrosion. This directive aims to maintain structural integrity and prevent rapid decompression due to potential cracks beneath the aft drain mast.

Airworthiness Directive

Boeing 737100200200C300400500

EASA SIB SAIB-2026-01

Mar 23, 2026

Pitot/Static Anti-Ice System

The Special Airworthiness Information Bulletin SAIB: 2026-01 is an FAA advisory concerning The Boeing Company Model 737-200/-300/-400/-500 airplanes. It informs operators about a potential issue where air data probe heaters may remain powered on while the aircraft is on the ground, which could pose a burn risk to maintenance personnel. This bulletin does not mandate corrective action but provides important safety information.

Safety Information Bulletin

Boeing 737200300400500

EASA AD US-2026-04-05

Feb 25, 2026

Electrical Power - AFM Operating Procedures - Amendment

EASA AD US-2026-04-05 is a final airworthiness directive issued by the FAA addressing electrical power and airplane flight manual (AFM) operating procedures for all Boeing 737-8, 737-9, and 737-8200 models. It responds to in-flight incidents of uncontrollable excessive cabin and flight deck temperatures caused by a tripped circuit breaker in the standby power control unit (SPCU). This directive mandates revisions to the AFM to include specific non-normal checklists for flightcrew to manage this condition.

Airworthiness Directive

Boeing 737

EASA AD US-2025-25-04

Dec 15, 2025

Equipment / Furnishings - Escape Slide Assembly - Inspection

The Equipment / Furnishings - Escape Slide Assembly - Inspection is a Federal Aviation Administration (FAA) Airworthiness Directive (AD 2025-25-04) that applies to The Boeing Company Model 737-600, -700, -700C, -800, -900, -900ER, 737-8, 737-9, and 737-8200 airplanes. This directive addresses the inspection and replacement of certain escape slide assemblies to prevent uncommanded inflation inside the slide compartment, which could cause injury or impede emergency evacuation.

Airworthiness Directive

Boeing 737

EASA AD US-2025-24-02

Nov 28, 2025

Landing Gear - Main Landing Gear Brake Hydraulic Hoses - Inspection

The Federal Aviation Administration's Airworthiness Directive 2025-24-02 addresses certain Boeing 737-700, -800, -900, and -900ER series airplanes. This directive mandates inspections and tests of the main landing gear brake hydraulic hoses and wheel speed transducer wiring to correct installation errors that could affect braking performance. The directive aims to prevent runway excursions caused by loss of braking due to crossed hydraulic hoses and interchanged transducer wires.

Airworthiness Directive

Boeing 737

EASA AD US-2025-19-12

Oct 29, 2025

Landing Gear - Main Landing Gear Outer Cylinders - Records Check / Inspection

The document titled "Landing Gear - Main Landing Gear Outer Cylinders - Records Check / Inspection" is a final rule airworthiness directive (AD 2025-19-12) issued by the Federal Aviation Administration (FAA) affecting all Boeing 737-600, -700, -700C, -800, -900, and -900ER series airplanes. This AD addresses potential heat damage caused by improper grinding of the inner diameter of the main landing gear outer cylinders. It mandates inspections or records checks and replacement of affected parts to ensure continued airworthiness.

Airworthiness Directive

Boeing 737

EASA SIB SAIB-2025-08

Sep 18, 2025

Indicating/Recording System - Erroneous Illumination of Cabin Altitude Warning Lights in High Altitude Landing Mode

The Special Airworthiness Information Bulletin SAIB: 2025-08 is an FAA advisory addressing erroneous illumination of cabin altitude warning lights in high altitude landing mode on Boeing 737-700 and 737-800 series airplanes with specific serial numbers. This bulletin provides information and recommended corrective actions but does not mandate compliance. It highlights issues related to wiring errors in previous Boeing Alert Service Bulletins affecting the cabin altitude warning system.

Safety Information Bulletin

Boeing 737

EASA AD US-2025-15-01

Jul 23, 2025

Fuselage - Frame Web - Repetitive Inspections

Fuselage - Frame Web - Repetitive Inspections is a Federal Aviation Administration (FAA) final rule airworthiness directive (AD 2025-15-01) that applies to all Boeing 737-600, -700, -700C, -800, -900, and -900ER series airplanes. This AD mandates repetitive inspections for cracks in specific fuselage frame webs at stations 312, 328, and 344 between designated stringers, and requires repair of any cracks found. The directive addresses a reported frame web crack that could compromise structural integrity.

Airworthiness Directive

Boeing 737

EASA AD US-2025-07-03

May 7, 2025

Fuselage - Frame Fittings and Failsafe Strap Outboard Chords - Repetitive Inspections

Fuselage - Frame Fittings and Failsafe Strap Outboard Chords - Repetitive Inspections is a Federal Aviation Administration (FAA) Airworthiness Directive (AD 2025-07-03) that applies to all Boeing 737-600, -700, -700C, -800, -900, and -900ER series airplanes. This AD mandates repetitive detailed and ultrasonic inspections for cracking on the left- and right-hand sides of certain frame fittings and failsafe straps at station 663.75, with required repairs if cracking is found. The directive aims to maintain the structural integrity of these Boeing 737 models by addressing potential failures in principal structural elements.

Airworthiness Directive

Boeing 737

EASA AD US-2025-04-03

Mar 27, 2025

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.

Other

Boeing 737

EASA AD US-2025-04-01

Mar 27, 2025

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.

Airworthiness Directive

Boeing 737

EASA AD US-2025-04-02

Mar 25, 2025

[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.

Airworthiness Directive

Boeing 737

EASA AD US-2025-05-16

Mar 25, 2025

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.

Airworthiness Directive

Boeing 737