RegNotify

EASA Regulations for Boeing 757

71 airworthiness directives and regulations affecting Boeing 757.

EASA AD US-2026-04-06

Wings - Scimitar Blended Winglets - Inspection

EASA AD US-2026-04-06 is a final airworthiness directive issued by the FAA addressing certain Boeing 757-200 and 757-300 series airplanes equipped with scimitar blended winglets. The directive mandates inspections for cracks in the inspar outer lower wing skin area near access panel 543BB and requires repairs if cracks are found. This AD aims to prevent potential structural integrity issues that could lead to partial wing loss and loss of airplane control.

Feb 27, 2026
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 757

EASA AD US-2026-01-05

Wings - Aviation Partners Boeing (APB) Scimitar Blended Winglets Lower Stringer - Inspection / Maintenance Records Check

EASA Airworthiness Directive US-2026-01-05 is a final rule issued by the FAA addressing certain Boeing 757-200 and 757-300 series airplanes equipped with Aviation Partners Boeing (APB) scimitar blended winglets. The directive mandates inspections and maintenance record checks of the lower stringer areas on the wings to detect cracks and verify approved freeze plug repairs. This AD aims to ensure continued airworthiness by addressing potential structural cracking in critical wing components.

Jan 20, 2026
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 757

EASA AD US-2025-23-03

Engine Strut Structure / Thermal Switch - Inspection

The document titled "Engine Strut Structure / Thermal Switch - Inspection" is a final rule airworthiness directive (AD 2025-23-03) issued by the Federal Aviation Administration (FAA) affecting certain Boeing Company Model 757 airplanes. It addresses issues related to precooler failures and latent failures of overheat detection thermal switches that could cause heat damage to the engine strut structure. The AD mandates inspections, tests, and replacements to ensure continued airworthiness and safety.

Dec 15, 2025
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 757

EASA AD US-2025-20-14

Equipment / Furnishings - IPECO 3A090 and 3A258 Flight Crew Seats - Inspection

The Equipment / Furnishings - IPECO 3A090 and 3A258 Flight Crew Seats - Inspection is a Federal Aviation Administration (FAA) Airworthiness Directive (AD 2025-20-14) that applies to all Boeing 757-200 series airplanes. It addresses uncommanded movement issues in the Captain's and First Officer's seats equipped with Ipeco 3A090 and 3A258 flight crew seats. The AD mandates inspections and maintenance actions to ensure seat safety and airplane controllability.

Dec 1, 2025
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 757

EASA AD US-2025-20-04

Flight Controls - Aileron Trim Actuator - Repetitive Inspections / Modification

Airworthiness Directive 2025-20-04 is a final rule issued by the Federal Aviation Administration addressing The Boeing Company Model 757 airplanes. This directive mandates repetitive inspections of the aileron trim actuator bearing and attachment lug, and introduces a required modification involving changes to the lateral control box support assembly and installation of an aileron trim actuator bracket to terminate these inspections.

Oct 9, 2025
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 757

EASA AD US-2025-19-11

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

The Federal Aviation Administration (FAA) Airworthiness Directive 2025-19-11 addresses all Boeing Company Model 757-200, -200PF, and -200CB series airplanes. This directive requires a records check or inspection of the main landing gear (MLG) outer cylinders due to reports of improper grinding causing possible heat damage. The directive mandates replacement of any affected outer cylinders to ensure continued airworthiness.

Oct 9, 2025
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 757

EASA AD US-2025-11-01

Fuselage - Web at K-hole between Stringers, Outer Chord above the Lower Hinge Intercostal, Inner Chord - Inspection / Records Check

The Federal Register document titled 'Fuselage - Web at K-hole between Stringers, Outer Chord above the Lower Hinge Intercostal, Inner Chord - Inspection / Records Check' is a final rule airworthiness directive (AD 2025-11-01) issued by the FAA. It applies to certain Boeing Company Model 757-200, -200CB, and -300 series airplanes and addresses newly discovered cracking in fuselage frame locations at body station 1640. The directive mandates inspections and records checks to detect cracks and requires corrective actions to maintain structural integrity.

Jun 4, 2025
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 757

EASA SIB SAIB-2025-02

Doors - Main Deck Cargo Door

Special Airworthiness Information Bulletin SAIB: 2025-02 is an FAA informational bulletin addressing an airworthiness concern involving the in-flight opening of the main deck cargo door on Boeing Model 757-200 series airplanes converted to freighter configuration by Precision Conversions, LLC under STC No. ST01529SE. The bulletin highlights an incident on a Boeing 757-236 PCF where the cargo door opened during climb, and provides recommended maintenance and operational procedures to mitigate similar events. It is not a mandatory directive but serves to inform operators of potential risks and preventive measures.

Mar 17, 2025
Safety Information BulletinMaintenanceSafety MgmtBoeing 757

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.

Mar 12, 2025
Airworthiness DirectiveFlight OpsMaintenanceSafety MgmtBoeing 717Boeing 737Boeing 747Boeing 757Boeing 767Boeing 777Boeing MD-11

EASA AD US-2025-02-13

Fuselage - Forward and Aft Hinge Areas of the Main Deck Cargo Door Cutout - Maintenance Record Check / Inspections

The Federal Register document titled "Fuselage - Forward and Aft Hinge Areas of the Main Deck Cargo Door Cutout - Maintenance Record Check / Inspections" is a final rule airworthiness directive (AD 2025-02-13) issued by the FAA. It applies to certain Boeing 757-200, -200CB, and -200PF series airplanes, including those modified by VT Mobile Aerospace Engineering Supplemental Type Certificates (STCs). The AD addresses cracks found at the main deck cargo door cutout forward and aft hinge attachment holes and mandates inspections and corrective actions to ensure structural integrity.

Feb 12, 2025
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 757

EASA SIB SAIB-2025-01

Hydraulic Power System - Fatigue Failure of Hydraulic Flexible Hoses

The Special Airworthiness Information Bulletin (SAIB) 2025-01 issued by the FAA addresses fatigue failure of hydraulic flexible hoses in the wheel wells of the main and nose landing gear on Boeing 757 series airplanes. The bulletin provides information on the issue and recommends maintenance actions to prevent loss of the left hydraulic system. This SAIB is informational and does not mandate regulatory action under 14 CFR part 39.

Jan 17, 2025
Safety Information BulletinMaintenanceSafety MgmtBoeing 757

EASA AD US-2024-25-09

Hydraulic Power - Power Transfer Unit Control Valve - Installation

The document titled "Hydraulic Power - Power Transfer Unit Control Valve - Installation" is a regulatory guideline focusing on the installation procedures and requirements for the power transfer unit control valve within aircraft hydraulic power systems. The document does not specify particular aircraft types, engine models, or part numbers affected. It provides detailed instructions to ensure proper installation and functionality of this critical hydraulic component.

Jan 13, 2025
OtherMaintenanceSafety MgmtBoeing 757

EASA AD US-2024-24-01

Fuselage - Upper Frame at the Frame Splices between Stringers - Inspections

The document titled 'Fuselage - Upper Frame at the Frame Splices between Stringers - Inspections' is a regulatory directive focusing on inspection requirements for the upper fuselage frame splices located between stringers. It addresses structural integrity concerns relevant to aircraft fuselage maintenance. Specific aircraft types, engine models, or part numbers are not explicitly mentioned in the document.

Dec 10, 2024
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 757

EASA AD US-2024-12-09

[Correction] Wings - Wing Skin / Shim - Inspection

The Correction to Airworthiness Directive 2024-12-09 issued by the Federal Aviation Administration (FAA) addresses all Boeing Company Model 757 airplanes. This correction fixes an incorrect AD number referenced in the original final rule related to inspections of the wing upper skin and drag fittings to detect cracks, loose fasteners, and shim migration. The directive ensures continued airworthiness by mandating inspections and on-condition repairs to maintain structural integrity of the engine strut attachment.

Aug 8, 2024
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 757

EASA AD US-2024-12-07

Fuselage - Lavatory Service Panel, Access Pan, and Attaching Structure - Inspection

The Federal Register document titled 'Fuselage - Lavatory Service Panel, Access Pan, and Attaching Structure - Inspection' is a final rule airworthiness directive (AD 2024-12-07) issued by the FAA affecting Boeing 757-200 airplanes modified by specific supplemental type certificates. It addresses reports of cracking in and around the lavatory service panel structure. The AD mandates repetitive inspections, reinforcement of the attaching structure, and repair or replacement of affected parts to ensure continued airworthiness.

Jun 28, 2024
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 757Boeing 757-200

EASA AD US-2024-10-05

Equipment / Furnishings - Decompression Panels and Pressure Equalization Valves in the Forward and Aft Lower Lobe Cargo Compartments - Inspections / Replacement / Installation

The Federal Aviation Administration's Airworthiness Directive 2024-10-05 addresses certain Boeing Company Model 757 airplanes. It mandates inspections and corrective actions for decompression panels and pressure equalization valves in the forward and aft lower lobe cargo compartments to prevent damage that could compromise cargo fire protection and airplane structural integrity.

Jun 18, 2024
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 757

EASA AD US-2024-10-07

Fuselage - Fuselage Skin Door Cutout - Inspection / Maintenance Records Check

Fuselage - Fuselage Skin Door Cutout - Inspection / Maintenance Records Check is a final rule airworthiness directive issued by the FAA affecting all Boeing Company Model 757 airplanes. It addresses potential cracks in hidden areas beneath scuff plates in the fuselage skin and bear strap of certain doors, including passenger entry, crew entry, cargo doors, and main deck cargo doors on cargo-modified aircraft.

Jun 18, 2024
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 757

EASA AD US-2024-07-05

Fuselage - Station 1640 Frame Web Between S-14 and S-15 - Inspection / Maintenance Records Check

The Federal Aviation Administration's Airworthiness Directive 2024-07-05 is a final rule addressing certain Boeing 757-200, 757-200CB, and 757-300 airplanes. It mandates inspections or maintenance records checks for liner holes in the fuselage at station 1640 frame web between stringers S-14 and S-15 due to detected cracks. The directive aims to ensure structural integrity by requiring corrective actions when necessary.

May 2, 2024
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 757Boeing 757-200Boeing 757-200CBBoeing 757-300

EASA AD US-2024-05-09

Fuselage - Station 1640 - Maintenance Records Check / Frame Web - Inspection

Federal Aviation Administration Airworthiness Directive 2024-05-09 is a final rule addressing certain Boeing 757-200, -200CB, and -300 series airplanes. It mandates inspections and maintenance record checks due to a reported crack at fuselage station 1640 frame web near the lower hinge intercostal tee clip center hole of the upper fastener row. The directive aims to ensure structural integrity by detecting and repairing potential cracks.

Apr 10, 2024
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 757Boeing 757-200Boeing 757-200CBBoeing 757-300

EASA AD 2023-0203

Engine — Critical Parts — Recalculation / Replacement

EASA Airworthiness Directive 2023-0203 is issued for Rolls-Royce Deutschland RB211-535E4 series engines installed on Boeing 757 aircraft among others. The directive addresses recalculation and replacement requirements for critical engine parts to ensure continued airworthiness. It mandates operators to reassess the life consumed by affected parts and replace them if necessary to prevent potential failures.

Nov 20, 2023
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg RB211-535Boeing 757