UNLIMITED TWO-SEATED AEROBATIC AIRCRAFT

Airframe is a carbon monocoque construction manufactured layup. The wing is a one piece double box main spar for the best safety. Ailerons are hinged on 5 points and equipped with spades to reduce control forces and enhance handling. All control surfaces can be removed within two hours by two people, allowing 2 aircraft per container for shipping. Main gear struts are steel spring type. Tailwheel is linked to the rudder pedals and is lockable.

Powerplant: Lycoming AEIO-580 B1A, 6 cylinder piston engine with 235kW / 315HP. inverted aerobatic oil system. Exhaust system 2 x 3-in-1

Proppellar: MTV-9-B-C/C203-20d 3-blade propeller with 80 inch diameter.


Performance Data:


Height
6.0 ft
Engine Power
315 HP
Length
21.6 ft
Max Speed VNE
225kts
Wing Span
24.6 ft
Stall Speed
53kts
Wing Area
121.25 sq/ft
Virtical Penetration
3,200ft
Empty Weight
583 kg
Pilot weight
130kg
Gross Weight
999 kg
Range
850 Nm
Wing Loading +-10G Fuel capacity / Center Acro
64 Ltrs
Roll Rate
450deg/s
Fuel capacity / Wings
200 Ltrs


MX Aircraft - MX2


The MX2 is an experimental unlimited aerobatic aircraft, built in the USA by MX aircraft, and known to many from the Red Bull Air Race. It is a 2 seat tandem, low wing airframe built entirely from carbon fiber.


Powerplant: Lycoming AEIO-540 Exp, 6 cylinder piston engine 10:1 piston ratio delivering 230kW / 325HP. Inverted aerobatic oil system. Exhaust system 2 x 3-in-1. Smoke system.

Proppellar: Hartzell Claw 3-blade propeller with 80 inch diameter.


Performance Data:


Height
6.0 ft
Engine Power
325 HP
Length
21.5 ft
Max Speed VNE
230kts
Wing Span
24.0 ft
Stall Speed
58kts
Wing Area
102.0 sq/ft
Virtical Penetration
3,200ft
Empty Weight
583 kg
Pilot weight
130kg
Gross Weight
975 kg
Range
850 Nm
Wing Loading +-12G Fuel capacity / Center Acro
64 Ltrs
Roll Rate
450deg/s
Fuel capacity / Wings
200 Ltrs


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