AD 2025-26-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | SOCATA | Various | Airworthiness Directives; DAHER AEROSPACE (Type Certificate Previously Held by SOCATA) Airplanes |
| aircraft | Socata | Various | Airworthiness Directives; DAHER AEROSPACE (Type Certificate Previously Held by SOCATA) Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; DAHER AEROSPACE (Type Certificate Previously Held by SOCATA) Airplanes |
Unsafe Condition
cracks on the vertical stabilizer attachment fitting which, if not addressed, could result in reduced structural integrity of the vertical stabilizer.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
repetitively inspecting the vertical stabilizer attachment fittings and bolts for cracks or corrosion, and, if necessary, repairing or replacing the damaged part and then applying a corrosion protection reinforcement.
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
DAHER AEROSPACE (Type Certificate Previously Held by SOCATA) Model TBM 700 airplanes, serial-numbered.
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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