Performance claims, figures and charts contained in this web site were taken from the original STC holder's sales literature and were based on actual performance testing of their specific aircraft. The test aircraft used was a U206G equipped with Flint wing tip tanks and was operated a gross weight of 3,800 pounds. In no way do these figures constitute any claims or warranties as to each specific aircraft's performance modified with this conversion. Aircraft performance will vary depending on various parameters such as; model, age, condition, rigging, weight, damage history, existing modifications, engine condition, etc.

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