AD 2025-02-09
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.) Airplanes |
Unsafe Condition
The fuselage center I longitudinal skin splice and panel between frames 22 and 23 are susceptible to cracking.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform repetitive inspections of the fuselage center I longitudinal skin splice and applicable corrective actions, as specified in ANAC AD 2024-04-02R01.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 50,000 total flight cycles, or within 800 flight cycles after the effective date of this AD, whichever occurs later.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
All Embraer S.A. Model EMB-120, -120ER, -120FC, -120QC, and -120RT 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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