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Lancair IVP Lancair Turbine IVP STANDARD DATA: IV Seats 4. Gross wt. 3,200. Empty wt. 1,750. Fuel capacity 82. Engine 350-hp Continental TSIO-550. PERFORMANCE: Top mph 361. Cruise mph 341. Initial climb rate 2,600. Ceiling 35,000. Range 1,450. Takeoff distance 1,200. Landing distance 1,900. STANDARD DATA: IV-P Seats 4. Gross wt. 3,550. Empty wt. 2,000. […]

1959’€“81

1999’€“Present

1991’€“Present

1964’€“70

1965’€“81

1954’€“81

1999’€“2006

1960’€“69

STANDARD DATA: Gross wt. 1,000. Empty wt. 605. Fuel capacity 16. Wingspan 16’8″. Length 16′. PERFORMANCE: Top mph 200. Cruise mph 150. Stall mph 52. Climb rate 2,500+. Takeoff run 300. Landing roll 800. Range 300. The Jungster I was developed as an 8/10-scale version of the famous Jungmeister aerobatic airplane. The intention was to […]