AD Amdt-39-10318
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Fairchild | Various | Airworthiness Directives; Fairchild Aircraft Incorporated Models SA226-TC, SA226-T, SA226-T(B), and SA226-AT Airplanes |
Unsafe Condition
Fatigue cracking of the wing trailing edge ribs due to high local stress concentration.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the center flap hinge and wing trailing edge ribs at the flap actuator attach brackets for cracks. If no cracks are found, install a doubler on the rib or replace a cracked rib with a new rib assembly reinforced with a doubler.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Fairchild Aircraft Incorporated Models SA226-TC, SA226-T, SA226-T(B), and SA226-AT 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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