XA41
The unlimited single-seated aerobatic aircraft
You have the choice how to use the most modern all-rounder of the world:
- compete and exercise up to unlimited competition aerobatics
- enjoy to fly in style with speed and range
- discover the feeling of easy slow-speed handling and accurate high-speed maneuverability
Equipment can range from „spartan-competition“ to „luxury-leather“ with highend avionics, just ask us !
XA41
The unlimited single-seated aerobatic aircraft
You have the choice how to use the most modern all-rounder of the world:
- compete and exercise up to unlimited competition aerobatics
- enjoy to fly in style with speed and range
- discover the feeling of easy slow-speed handling and accurate high-speed maneuverability
Equipment can range from „spartan-competition“ to „luxury-leather“ with highend avionics, just ask us !
Airframe
- Airframe carbon monocoque construction manufactured layup method
- surface protected by high quality acrylic paint
- the wing is a one piece double box main spar for the best safety
- ailerons are hinged on 5 points
- equipped with spades to reduce control forces and enhance handling
- all control surfaces can be removed within two hours by two people
- main gear struts are steel spring type
- tailwheel is linked to the rudder pedals and is lockable
Systems
- 12 V electric system
- 20 amp alternator
- smoke tank with filling system
- two wing tanks (each 105 l / 27.7 US.gal)
- aerobatic tank with 67 l / 17,7 US.gal
Cockpit
- high-end stick and rudder controls for performance on max-level
- aileron and elevator controls are actuated via carbon tubing
- engine is controlled via push-pull cables
- canopy has an emergency jettison system
- rudder pedals are adjustable
- seat is equipped with a 5-point aerobatic harness system
Powerplant / Propeller
- Lycoming AEIO-580 B1A, 6 cylinder piston engine with 235kW / 315HP
- inverted aerobatic oil system
- MTV-9-B-C/C203-20d 3-blade propeller with 80 inch diameter
- 2x 3-in-1 exhaust system
Technical specs
Engine |
| Lycoming AEIO-580-B1A |
| 6 cylinder piston engine with 235 kW / 315 HP |
Propeller |
| MT Propeller MTV-9-B-C / C203-20d |
| 3-blade, hydraulic constant speed |
Dimensions | ||
| Empty mass approx. | 1370 lbs | 623 kg |
| Maximum empty mass | 1477 lbs | 670 kg |
MTOM and MLM | ||
| Utility | 2200 lbs | 999 kg |
| max. baggage load | 22 lbs | 10 kg |
| Acro II | 2200 lbs | 999 kg |
| Acro III unlimited (+/- 10g) | 1847 lbs | 850 kg |
| Total fuel capacity | 72.65 US.gal | 275 Liter |
| Usable fuel | 72.15 US.gal | 273 Liter |
| Usable for Aerobatics (Acro III) | 15 US.gal | 57 Liter |
| Smoke Oil | 7 US.gal | 27 Liter |
Speeds | |
| VNE, Never exceed speed | 225 KIAS |
| VNO, max. cruising speed | 185 KIAS |
| Maximum operating altitude | 15.000 ft |
Performance | |
| Rollrate | 450° / sec |
| Rate of climb with 1874 lbs / 850 kg at Vy | 3.212 ft / min |
In 4.000 ft,ISA, @ 45% power setting | ||
| Lean for best economy | 167 KTAS | |
| Fuel flow | 10 US.gal / h | 37 Liter / h |
| Distance including 60 min reserve | 1050 NM |
Media Gallery
Images
