ADI Stallion

Airplanes

Length

7.62 m

Flat Wing Span

10.67 m

Height

2.9 m

Flat Wing Area

13 m²

Flat Wing Aspect Ratio

8.8

Max Seating

Cruise Speed

474 km/h

Max Speed

493 km/h

Max Ceiling

9750 m

Number of Engines

First Flight

1994-07-01

Number Built

Maximum Take-Off Weight

1.784 t (paragliders: kg)

Maximum Range

4345 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
ADI Stallion	1.784	4345

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)
Bernard 15	Hispano-Suiza piston aero-engines	7.5	11.4	Compare
Armstrong Whitworth Scimitar	Armstrong Siddeley Panther	7.62	10.0584	Compare
Adventure Air Adventurer		7.62	10.668	Compare
Bellanca Skyrocket II	Continental IO-520	8.2296	10.3632	Compare
Beneš-Mráz Be-150 Beta-Junior	Walter Junior	7.55	10.66	Compare
Berliner-Joyce P-16		8.59	10.36	Compare

All data (23 fields)

Name: ADI Stallion
Manufacturer: Aircraft Designs Inc
Description: The ADI Stallion is a US civil utility aircraft that first flew in July 1994.
First Flight: 1994-07-01
Designer: Martin Hollmann
Type: Light utility aircraft
Length (m): 7.62
Height (m): 2.9
Max Seating: 5
Max Speed (km/h): 493
Cruise Speed (km/h): 474
Min Speed (km/h): 115
Max Ceiling (m): 9750
Rate of Climb (m/s): 13.2
Capacity Description: 5 passengers
National Origin: United States of America
Number Built: 7
Powerplant Description: 1 × Continental TSIO-550-B air-cooled turbocharged flat-six engine, 224 kW (300 hp) each
Wikipedia Article (URL): en.wikipedia.org/wiki/ADI_Stallion
Flat Wing Span (m): 10.67
Flat Wing Area (m²): 13
Flat Wing Aspect Ratio: 8.8
Number of Engines: 1