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AD 2025-10060

Published 2025-06-03 · 1 model · 1 US-registered tails affected · Federal Register

Airworthiness Directives; The Boeing Company Airplanes Federal Register ↗

Abstract

The FAA is adopting a new airworthiness directive (AD) for certain The Boeing Company Model 757-200, -200CB, and -300 series airplanes. This AD was prompted by a report of cracking found in new locations at a certain body station (STA) during frame segment replacement repairs, including in the web at the K-hole between certain stringers, in the outer chord above the lower hinge intercostal, and in the inner chord and web between certain stringers. This AD requires an inspection or records check for the presence of approved or local repairs, repetitive eddy current inspections for cracking, and applicable on-condition actions. The FAA is issuing this AD to address the unsafe condition on these products.

Applicability · by US fleet size

  • PARKS 3 1 tails

Federal Register text

Verbatim; the Federal Register publication is the legally binding document. Cite: 90 FR 23429. View on Federal Register ↗

[Federal Register Volume 90, Number 105 (Tuesday, June 3, 2025)] [Rules and Regulations] [Pages 23429-23432] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR Doc No: 2025-10060]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2025-0012; Project Identifier AD-2024-00219-T; Amendment 39-23047; AD 2025-11-01] RIN 2120-AA64

Airworthiness Directives; The Boeing Company Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

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SUMMARY: The FAA is adopting a new airworthiness directive (AD) for certain The Boeing Company Model 757-200, -200CB, and -300 series airplanes. This AD was prompted by a report of cracking found in new locations at a certain body station (STA) during frame segment replacement repairs, including in the web at the K-hole between certain stringers, in the outer chord above the

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lower hinge intercostal, and in the inner chord and web between certain stringers. This AD requires an inspection or records check for the presence of approved or local repairs, repetitive eddy current inspections for cracking, and applicable on-condition actions. The FAA is issuing this AD to address the unsafe condition on these products.

DATES: This AD is effective July 8, 2025. The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD as of July 8, 2025.