AD 2018-21-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Socata | TB 9 and Model TB 10 | Airworthiness Directives; SOCATA Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; SOCATA Airplanes |
Unsafe Condition
fatigue cracking of the wing front attachments on the wing and fuselage sides
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
inspect the front attachments and install modification kits, replace the wing attachment on the wing side after repetitive inspections
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
SOCATA Model TB 9, Model TB 10, and Model TB 200 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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