XA42 will be presented by Tim Tibo on CIAF 2018.

General characteristics

• Crew: 1
• Capacity: 2
• Length: 6.67 m (21 ft 11 in)
• Wingspan: 7.5 m (24 ft 7 in)
• Height: 2.54 m (8 ft 4 in)
• Wing area: 11.25 m² (121.1 sq ft)
• Airfoil: PS-1-16 (wing), PS-1-09 (wing tip), DU86-MOD1 (horizontal tail including elevator and vertical tail including rudder)
• Empty weight: 670 kg (1,477 lb)
• Gross weight: 850 kg (1,874 lb) for acrobatic flight, 999 kg (2,200 lb) for utility flight
• Fuel capacity: 275 l (72.6 US gal) total, 273 l (72.1 US gal) usable, 64 l (16.9 US gal) usable for aerobatics
• Powerplant: 1 × Lycoming AEIO-580-B1A horizontally-opposed six-cylinder four stroke piston engine, 235 kW (315 hp) at 2,700 rpm
• Propellers: 3-bladed MT-Propeller MTV-9-B-C/C203-20d, 2.03 m (6 ft 8 in) diameter ± 5 mm

Performance

• Maximum speed: 417 km/h (259 mph; 225 kn)
• Cruise speed: 343 km/h (213 mph; 185 kn)
• Stall speed: 100 km/h (62 mph; 54 kn)
• Never exceed speed: 417 km/h (259 mph; 225 kn)
• Range: 1,296 km (805 mi; 700 nmi) at 73% power and 4,000 ft with 60 min reserve
• Ferry range: 1,945 km (1,209 mi; 1,050 nmi) at 50% power at 10,000 ft with 60 min reserve
• Service ceiling: 4,572 m (15,000 ft)
• g limits: ± 10
• Roll rate: 450 °/sec
• Maximum glide ratio: 1:7
• Rate of climb: 16.59 m/s (3,266 ft/min) in acrobatic flight, 13.82 m/s (2,720 ft/min) in utility flight
• Wing loading: 75.5 kg/m² (15.5 lb/sq ft) in acrobatic flight, 84.4 kg/m² (17.3 lb/sq ft)
• Power/mass: 2.01 kW/kg (1.22 hp/lb) in acrobatic configuration, 2.24 kW/kg (1.37 hp/lb) in utility configuration
• Fuel flow: 57 L/h (15.1 US gal/h)