Lancair Super ES

Time constraints kept us from sampling the ES-P up at the altitudes where Lancair designed it to shine. [The last 310-hp Lancair ES we tested ran 190 KTAS at 8000 feet msl. Assuming approximately the same drag profile for the ES-P, a rough estimate of its potential at 17,500 feet is 212 KTAS, and 235 KTAS at FL250.—Ed.]. Empty Weight (ES)1900 lbs (Super ES) 2000 lbs Gross Weight 3200 lbs Standard Fuel Capacity 95 gal Useful Load (ES) 1300 lbs (Super ES) 1200 lbs Baggage Capacity 175 lbs Trailering Width 100 in Cabin Area. fi rst fl ight in your new Lancair ES. Continental IO-550-N 310 hp @ 2700 rpm, 6 cylinder, fuel injected 3-blade constant speed propeller.

Lancair Super ES. Derived from the award-winning, world record setting Lancair IV, the ES and Super ES are the result of nearly 10 years of research, innovation and pilot input. These visionary, four-place aircraft have it all; high climb rate, long endurance, slow landing speed, premium comfort, all packaged in a very elegant, streamlined.. The Lancair ES is a family of 4-seat American amateur-built aircraft that were designed by Lance Neibauer and produced by his company, Lancair of Redmond, Oregon. Derived from the award-winning, world record setting Lancair IV, the ES and Super ES were the result of nearly 10 years of research, innovation and pilot input. These aircraft