The Plasmatec has the design and the prototype of an Acrobatic Aircraft for Civil and Military Training: Guará T200. The Guará is ready to be produced in series.
•Basic Type: Primary training and acrobatics. Manufacturer designation: GP-A135-A, Number of seats: 02. Engine LYCOMING AEIO 360 A1B6, 200 HP.
•The aircraft may be used to graduate civil and military pilots and aerobatic flights.
•The aircraft is land type, monoplane, single engine, completely metallic, low wing, rectangular, cantilever, tandem two seater, fixed tricycle landing gear, allowing use of back parachute or seat parachute. Metallic construction fuselage, semi monocock structured. Metallic cantilever empennage. Main dimensions refer to FIG 1-1. The usual internal arrangement is presented in FIG 5-1.
•The aircraft flight qualities herein specified assure maximum safety to its crew. The aircraft is totally controllable at every attitude and does not present uncommon tendencies, either on ground as in flight. The cabin and its interior layout are so arranged that in case of an accident, danger to physical integrity of the crew is minimized.
•Flight qualities are conventional encompassing harmonization and sensitiveness of the controls, without any intermediary device.
Engine - Lycoming AEIO 360 A1B6: 200 HP
Propeller - Hartzell, HC-C3YR-4BF/FC 6890: Three blade
Maximum leveled at flight speed and at maximum power: 136 kt (252 km / h)
Fast Cruise Speed ??(75% maximum power): 120 kt (222 km / h)
Economy Cruise Speed ??(65% maximum power): 110 kt (204 km / h)
Maximum slope ratio: 1400 ft / m (7.10 m / s)
Service Ceiling: 20,000 ft (6100 m)
Take off distance with 50 ft (15m) obst.: 270 m
Landing distance with 50 ft (15m) obst.: 160 m
Range with 30 minutes fuel reserve: 4:00 pm
Stall Speed: 55 kt (101 km / h)
Stall speed with flaps: 45 kt (89 km / h)
Dry weight (standard): 660 kg
Maximum take off weight: 960 kg
Aerobatic Category - Load Factors: + 6.0 g and 3.0 g