AD 2024-24-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | Defense and Space S | Airworthiness Directives; Airbus Defense and Space S.A. (Formerly Known as Construcciones Aeronauticas, S.A.) Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Airbus Defense and Space S.A. (Formerly Known as Construcciones Aeronauticas, S.A.) Airplanes |
Unsafe Condition
cracking, which could lead to reduced structural integrity of the lugs on the horizontal stabilizer-to-fuselage rear attachment fittings
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
repetitive inspections, as specified in EASA AD 2024-0049, and contacting the manufacturer for corrective actions
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 50 flight hours
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Airbus Defense and Space S.A. (formerly known as Construcciones Aeronauticas, S.A.) Model CN-235, CN-235-200, CN-235-300, and C-295 airplanes
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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