EASA Regulations for Boeing 757-200CB

12 airworthiness directives and regulations affecting Boeing 757-200CB.

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New ADs and bulletins for Boeing 757-200CB, summarized like the ones below, every Monday.

EASA SIB SAIB-2026-09

Apr 23, 2026

Hydraulic Power - Hydraulic Power Transfer Unit System

The FAA Special Airworthiness Information Bulletin SAIB: 2026-09 addresses errors found in Boeing Alert Requirements Bulletin 757-29A0071 RB, Original Issue, dated November 16, 2023, which affects The Boeing Company Model 757-200, -200PF, -200CB, and -300 series airplanes. This bulletin informs operators about issues related to the hydraulic power transfer unit (PTU) control valve and provides recommended actions to mitigate potential safety concerns. The document serves as an interim advisory prior to the anticipated supersedure of Airworthiness Directive 2024-25-09.

Safety Information Bulletin
  • Boeing 757200200PF200CB300

EASA AD US-2024-07-05

May 2, 2024

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.

Airworthiness Directive
  • Boeing 757200200CB300

EASA AD US-2024-05-09

Apr 10, 2024

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.

Airworthiness Directive
  • Boeing 757200200CB300

EASA AD US-2022-15-09

Aug 5, 2022

Fuselage - Fuselage Frame Web - Inspection

The Federal Aviation Administration's Airworthiness Directive 2022-15-09 supersedes AD 2019-23-06 and applies to certain Boeing 757-200, -200CB, and -300 series airplanes. It mandates inspections of the fuselage frame web fastener holes at body station 1640, including visual and high frequency eddy current (HFEC) inspections, to detect cracks and previous repairs. The directive addresses structural integrity concerns related to cracks that could compromise airplane safety.

Airworthiness Directive
  • Boeing 757200200CB300

EASA AD US-2022-07-07

Apr 22, 2022

Equipment / Furnishings - Passenger Service Units, Life Vest Panels and Video Panel Lanyard Assemblies - Installation

The Federal Aviation Administration (FAA) Airworthiness Directive 2022-07-07 addresses certain Boeing 757-200, -200CB, and -300 series airplanes. This directive mandates the installation of lanyard assemblies on passenger service units (PSUs), life vest panels, and video panels to prevent these components from detaching during survivable accidents. The directive aims to enhance cabin safety by reducing the risk of injury and facilitating evacuation.

Airworthiness Directive
  • Boeing 757200200CB300

EASA AD US-2021-22-23

Dec 14, 2021

Wings - Lower Aft Wing Skin Bolt Holes - Repetitive Inspections / Repair

Federal Aviation Administration Airworthiness Directive 2021-22-23 is a final rule addressing all Boeing 757-200, -200PF, -200CB, and -300 series airplanes. It requires repetitive high frequency eddy current inspections for cracks in the lower aft wing skin bolt holes at flap track attachment points, prompted by crack findings on a similar Boeing 737-300 design. The directive mandates repairs if cracks are detected to maintain structural integrity.

Airworthiness Directive
  • Boeing 757200200PF200CB300

EASA AD US-2020-21-17

Dec 15, 2020

Superseded by FAA AD 2022-08-12

Airworthiness Directive 2020-21-17 is a final rule issued by the Federal Aviation Administration (FAA) that supersedes AD 2018-16-05 and applies to certain Boeing 757-200, -200PF, -200CB, and -300 series airplanes. It addresses repetitive inspections for skin cracking, shim migration, diagonal brace cracking, and fastener looseness at the upper link drag fittings and adds new inspection requirements for additional fastener hole locations. The directive aims to maintain structural integrity of the engine strut by preventing unsafe conditions caused by cracks and bolt rotation.

Airworthiness Directive
  • Boeing 757200200PF200CB300

EASA AD US-2020-20-10

Oct 8, 2020

Fuselage - Fuselage Frame - Inspections / Repair

Airworthiness Directive 2020-20-10 is a final rule issued by the Federal Aviation Administration (FAA) addressing certain Boeing 757-200, -200CB, and -300 series airplanes. This directive requires inspections and repairs of the fuselage frame at station 1640 to detect and correct fatigue cracking that could compromise structural integrity. It expands upon previous inspection requirements to enhance safety.

Airworthiness Directive
  • Boeing 757200200CB300

EASA AD US-2020-05-25

Apr 3, 2020

Fuselage - Fuselage Frames - Inspection

Federal Register Volume 85, Number 61 (March 30, 2020) is a final rule airworthiness directive issued by the FAA addressing all Boeing 757-200, -200PF, -200CB, and -300 series airplanes. It mandates inspections of the aft cargo compartment fuselage frames, specifically at station 1460 frame web and inner chord between stringers, due to discovered cracking during maintenance. The directive requires repetitive surface high frequency eddy current inspections and applicable on-condition corrective actions to ensure structural integrity.

Airworthiness Directive
  • Boeing 757200200PF200CB300

EASA AD US-2019-23-06

Dec 16, 2019

Superseded by FAA AD 2022-15-09

FAA Airworthiness Directive 2019-23-06 is a final rule addressing certain Boeing 757-200, -200CB, and -300 series airplanes. It mandates inspections for cracks initiating in the fuselage frame web at body station 1640, including visual and high frequency eddy current inspections, with applicable corrective actions. This directive aims to maintain structural integrity and safety of the affected aircraft.

Airworthiness Directive
  • Boeing 757200200CB300

EASA AD US-2017-26-07

Jan 4, 2018

Fuselage - Frame Web at STA 1681 - Inspection

Federal Aviation Administration Airworthiness Directive 2017-26-07 is a final rule addressing certain Boeing 757-200, -200CB, and -300 series airplanes. It mandates inspections of the fuselage frame web at station 1681 for fatigue cracking, including checks for existing repairs and repetitive inspections, to ensure structural integrity. This directive responds to reports of fatigue cracks that could compromise airplane safety.

Airworthiness Directive
  • Boeing 757200200CB300