Airworthiness directives › 2024-26-07
AD 2024-26-07 Airworthiness Directives; Embraer S.A. (Type Certificate Previously Held by Yaborã Indústria Aeronáutica S.A.; Embraer S.A.; Empresa Brasileira de Aeronáutica S.A. (EMBRAER)) Airplanes
Models named: EMB-135ER, -135KE, -135KL, -135LR, EMB-145, -145EP, -145ER, -145LR, -145MP, -145MR. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
This AD applies to all Embraer S.A. (Type Certificate previously held by Yaborã Indústria Aeronáutica S.A.; Embraer S.A.; Empresa Brasileira de Aeronáutica S.A. (EMBRAER)) airplanes specified in paragraphs (c)(1) and (2) of this AD, certificated in any category. (1) Model EMB-135ER, -135KE, -135KL, and -135LR airplanes. (2) Model EMB-145, -145EP, -145ER, -145LR, -145MP, -145MR, and -145XR airplanes.
Compliance
Comply with this AD within the compliance times specified, unless already done.
Required actions
Except as specified in paragraph (h) of this AD: Comply with all required actions and compliance times specified in, and in accordance with, Agência Nacional de Aviação Civil (ANAC) AD 2024-04-03R01, effective May 31, 2024 (ANAC AD 2024-04-03R01).
Unsafe condition
This AD was prompted by a structural assessment that indicated certain central fuselage longitudinal splices are subjected to fatigue damage on multiple sites due to loose fasteners, which may reduce the structural residual strength below the required levels. The FAA is issuing this AD to address undetected fatigue damage on certain central fuselage longitudinal splices. The unsafe condition, if not addressed, could result in reduced structural integrity of the airplane.
Affected ADs
None.
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The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1