AD 2025-02400
Published 2025-02-11 · 1 model · 3 US-registered tails affected · Federal Register
Airworthiness Directives; Embraer S.A. (Type Certificate Previously Held by Yaborã Indústria Aeronáutica S.A.; Embraer S.A.) Airplanes Federal Register ↗
Abstract
The FAA is adopting a new airworthiness directive (AD) for all Embraer S.A. Model EMB-120, -120ER, -120FC, -120QC, and -120RT airplanes. This AD was prompted by a structural assessment, which found that the fuselage longitudinal skin splice and panel between certain frames are susceptible to cracking. This AD requires performing repetitive inspections of the fuselage center I longitudinal skin splice and applicable corrective actions, as specified in an Ag[ecirc]ncia Nacional de Avia[ccedil][atilde]o Civil (ANAC) AD, which is incorporated by reference (IBR). The FAA is issuing this AD to address the unsafe condition on these products.
Applicability · by US fleet size
- EMBRAER EMB-120 TCDS A31SO 3 tails
Federal Register text
Verbatim; the Federal Register publication is the legally binding document. Cite: 90 FR 9283. View on Federal Register ↗
[Federal Register Volume 90, Number 27 (Tuesday, February 11, 2025)] [Rules and Regulations] [Pages 9283-9286] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR Doc No: 2025-02400]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2024-2140; Project Identifier MCAI-2024-00242-T; Amendment 39-22942; AD 2025-02-09] RIN 2120-AA64
Airworthiness Directives; Embraer S.A. (Type Certificate Previously Held by Yabor[atilde] Ind[uacute]stria Aeron[aacute]utica S.A.; Embraer S.A.) 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 all Embraer S.A. Model EMB-120, -120ER, -120FC, -120QC, and -120RT airplanes. This AD was prompted by a structural assessment, which found that the fuselage longitudinal skin splice and panel between certain frames are susceptible to cracking. This AD requires performing repetitive inspections of the fuselage center I longitudinal skin splice and applicable corrective actions, as specified in an Ag[ecirc]ncia Nacional de Avia[ccedil][atilde]o Civil (ANAC) AD, which is incorporated by reference (IBR). The FAA is issuing this AD to address the unsafe condition on these products.
[[Page 9284]]
DATES: This AD is effective March 18, 2025. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of March 18, 2025.