AD 2000-10-22
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Lake | LA-4 | Airworthiness Directives; REVO, Incorporated Models Lake LA-4, Lake LA-4A, Lake LA-4P, Lake LA-4-200, and Lake Model 250 Airplanes |
Unsafe Condition
Fatigue cracks in the wing spars, specifically at the second-most inboard wing attachment bolt hole, could result in wing separation and loss of control.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the left and right wing upper and lower spar doublers for cracks; replace any cracked parts; incorporate a modification kit.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 12 months of the effective date of the AD.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
REVO, Incorporated Models Lake LA-4, Lake LA-4A, Lake LA-4P, Lake LA-4-200, and Lake Model 250 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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