AD 2002-19-14
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Lockheed | C-130A | Airworthiness Directives; Lockheed C-130A Airplanes, Type Certificated in the Restricted Category |
Unsafe Condition
Fatigue cracking at fastener holes in the left- and right-side lower skin panels and stringers of the center wing between wing stations 41.0 and 71.0, which could result in structural failure of the wings and consequent loss of control of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the left- and right-side lower skin panels and stringers of the center wing between wing stations 41.0 and 71.0 for cracks at fastener holes. Replace any cracked part with a new part or repair and inspect at new intervals.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Not specified in the provided text.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
All Lockheed C-130A airplanes type certificated in the restricted category.
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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