AD Amdt-39-10524
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Lake | LA-4 | Airworthiness Directives; REVO, Incorporated Models Colonial C-2, Lake LA-4, Lake LA-4A, Lake LA-4P, and Lake LA-4-200 Airplanes |
Unsafe Condition
Fatigue cracks to the horizontal and vertical stabilizer attachment fitting could result in loss of control of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Measure clearances between attachment fitting and horizontal stabilizer rear beam (minimum 5/32 inch) and stabilizer skin (minimum 1/16 inch). Remove affected horizontal tail half if clearances are insufficient, inspect attachment fitting for fretting, cracking, or corrosion. Replace attachment fitting if defects found and trim stabilizer skin to ensure clearance.
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
REVO, Incorporated Models Colonial C-2, Lake LA-4, Lake LA-4A, Lake LA-4P, and Lake LA-4-200 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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