AD 2024-26-07
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Embraer | S | 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 |
Unsafe Condition
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.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform repetitive inspections of certain upper central fuselage longitudinal splices as specified in ANAC AD 2024-04-03R01. Report inspection results. Repair any discrepancies, including cracking, if found.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the timeframes specified in ANAC AD 2024-04-03R01.
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Affected Aircraft
Embraer S.A. Model EMB-135ER, -135KE, -135KL, -135LR, EMB-145, -145EP, -145ER, -145LR, -145MP, -145MR, and -145XR airplanes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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