AD 2005-06-13
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Fairchild | Various | Airworthiness Directives; Fairchild Aircraft, Inc. SA226 and SA227 Series Airplanes |
Unsafe Condition
Fatigue cracking of the wing spar center web cutout area between Wing Station (WS) 8 and WS 17.5, which could result in structural failure of the wing spar and loss of control of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Repetitively inspect the wing spar center web cutout on both wings for cracks between WS 8 and WS 17.5. Immediately repair any area found cracked. The repair will eliminate the need for further repetitive inspections on that particular wing spar.
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
Fairchild Aircraft, Inc. SA226 and SA227 series airplanes, including additional Model SA227-CC/DC airplanes with serial numbers from CC/DC879 through CC/DC896.
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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