Aircraft Technologies Atlantis
# Aircraft Technologies Atlantis

The Aircraft Technologies Atlantis is an American aerobatic homebuilt aircraft, built by Aircraft Technologies of Lilburn, Georgia. The aircraft is supplied as a kit or in the form of plans for amateur construction.

## Design and development

The Atlantis is a two-seat side-by side low wing aircraft with conventional landing gear. The fuselage is constructed of welded steel tubing. Fuel tanks are located in the wings, with a central header tank. The aircraft uses two control sticks for each pilot and a pull-up flap handle between the seats. The seats recline to a 35 degree angle.

## Operational history

In November 2014 three examples were registered in the United States with the Federal Aviation Administration.

## Specifications (Atlantis)

Data from Sport Aviation

General characteristics

* Crew: 1
* Capacity: 1 passenger
* Empty weight: 1,100 lb (499 kg)
* Gross weight: 1,900 lb (862 kg)
* Fuel capacity: 60 U.S. gallons (230 L; 50 imp gal)
* Powerplant: 1 × Lycoming IO-360 horizontally opposed piston aircraft engine, 200 hp (150 kW)
* Propellers: 2-bladed MT constant speed

Performance

* Cruise speed: 155 kn (178 mph, 287 km/h)
* Stall speed: 43 kn (50 mph, 80 km/h)
* g limits: +/-20g wing, +/-15g fuselage and tail
* Roll rate: 200 degrees per second
* Wing loading: 95 lb/sq ft (460 $kg/m^2)$
