AD 2014-09-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Socata | TBM 700 | Airworthiness Directives; SOCATA Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; SOCATA Airplanes |
Unsafe Condition
Cracks on the outboard hinge fittings of the horizontal stabilizer, caused by incorrect installation during production, inducing stress.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Install shims on the outboard hinge fittings of the horizontal stabilizer to eliminate stress. Discontinue repetitive inspections of the fittings for cracks if the modification is installed.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight
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Affected Aircraft
SOCATA Model TBM 700 airplanes.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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