AD Amdt-39-10403
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Fairchild | Various | Airworthiness Directives; Fairchild Aircraft Inc. Models SA226- AT, SA226-TC, SA227-AC, and SA227-AT Airplanes |
Unsafe Condition
Fatigue at the bottom of the cargo door could cause failure of the cargo door in flight, leading to decompression injuries and substantial structural damage.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect cargo door lower belt frames at cargo latch receptacles for cracks, repair any cracks, and reinforce by installing doublers.
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 Inc. Models SA226-AT, SA226-TC, SA227-AC, and SA227-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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