EASA Regulations for Boeing 757-200PF

6 airworthiness directives and regulations affecting Boeing 757-200PF.

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New ADs and bulletins for Boeing 757-200PF, 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-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Superseded by FAA AD 2022-08-12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-2020-05-25

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