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The ADI Stallion is a US civil utility aircraft that first flew in July 1994. It is marketed in kit form for homebuilding. It is a single-engined high-winged monoplane with wings based on htose of the Lancair IV and a retractable tricycle landing gear. It has a steel-tube fuselage centre section with the remainder of the airframe of composite construction and is designed to be powered by engines of 230–350 hp (172–261 kW).

Made by Aircraft Designs.

Height Main
289.56
Designer
Martin Hollmann
Stall Speed Main
71 mph
Length Alt
7.62 m
Max Takeoff Weight Main
3800.0
Jet Or Prop
prop
Range Main
2
700 miles
Height Alt
2.90 m
Aspect Ratio
9
Max Speed Main
306 mph
Capacity
5
Cruise Speed Main
295 mph
Max Takeoff Weight Alt
1784.0
Ceiling Main
32000.0
Type Of Prop
air-cooled turbocharged flat-six engine
Crew
one pilot
Span Main
1066.8
Cruise Speed Alt
256
Area Main
140.1
Span Alt
10.67 m
Plane Or Copter?
plane
Power Alt
224.0
Engine(prop)
Continental IO-550
Manufacturer
Aircraft Designs
First Flight
July 1994
Origin
United States
National Origin
United States
Climb Rate Main
2600.0
Power Main
350 hp
Number Of Props
1
Stall Speed Alt
62
Climb Rate Alt
13.2 m-s
Length Main
762.0
Area Alt
13.00 m²
Range Alt
2346
Max Speed Alt
266
Related
*Lancair IV
Empty Weight Main
2200.0
Ceiling Alt
9
750 m
Empty Weight Alt
998.0
Category
Homebuilt aircraft
Propeller aircraft
Single-engine aircraft
United States civil utility aircraft 1990-1999

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