AD 2010-26-54
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Cessna | LC41-550FG | Airworthiness Directives; Cessna Aircraft Company (Cessna) (Type Certificate A00003SE Previously Held by Columbia Aircraft Manufacturing (Previously The Lancair Company)) Models LC41-550FG and LC42-550FG Airplanes |
Unsafe Condition
Disbonding of the wing skin from the upper forward wing spar, as occurred in a Cessna Model LC41-550FG airplane during a production acceptance flight test, leading to a significant structural failure.
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Required Actions
Obtain written approval from the Manager, Wichita Aircraft Certification Office (ACO), to operate the airplane. The written approval must clearly state that operation is approved per Emergency AD 2010-26-54.
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Compliance Time
Before further flight
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Affected Aircraft
Cessna Aircraft Company (Type Certificate A00003SE previously held by Columbia Aircraft Manufacturing (previously The Lancair Company)) Models LC41-550FG and LC42-550FG airplanes, specifically serial numbers 41028, 41705, 411114, 411160, 411161, 411162, 411163, 411164, 411165, 411167, 411170, 411171 for LC41-550FG, and 42517 for LC42-550FG.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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