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THE PS-28 CRUISER IS USED EXTENSIVELY FOR FLIGHT TRAINING IN EUROPE.
The PS-28 Cruiser is Type Certified for VFR Day operations according to EASA LSA regulations and can be fully commercially operated in all EASA countries or in countries wher the PS-28 Cruiser obtained local CAA Type Certification. In April 2012, the PS-28 Cruiser was the very first aircraft to receive certification in the brand new category of Light Sport Aircraft with European General Aviation.
Engine: Rotax 912 ULS2
Power: 73.5 kW, 100 HP at 5800 RPM
Fuel: Mogas RON 95, Avgas 100 LL, EN 228
Propeller: Woodcomp Klassic 170/3/R
Sensenich Fixed 3-blade (*)
Wingspan: 8.6 m (28.22 ft)
Length: 6.62 m (21.72 ft)
Height: 2.315 m (7.60 ft)
Wing surface area: 12.3 m² (132.4 sq ft)
Cockpit width: 1.17 m (3.85 ft)
MTOW: 600 kg (1,320 lbs)
Empty weight: 388 kg (855.4 lbs)
Max. baggage weight in cockpit compartment: 18 kg (40 lbs)
Max. baggage weight in each wing locker: 10 kg (22 lbs)
Cruise speed at 3,000 ft and 75% power: 93 KIAS (172 km/h)
Max. horizontal speed: 119 KIAS (220 km/h)
VNE : 138 KIAS (255 km/h)
Stall speed VS0: 31 KIAS (55 km/h)
Climb rate: 825 ft/min (4.2 m/s)
Take-off distance to 50 ft (15 m):
Concrete: 1,270 ft (387 m)
Grass: 1,499 ft (457 m)
Braking distance:
Concrete: 479 ft (146 m)
Grass: 364 ft (111 m)
Range (30 min. reserve): 516 NM (953 km)
Endurance: 5 hours 25 min
Fuel capacity: 114 l (30 US gal.)
Average fuel consumption: 17.5 l/h (4.6 US gal./1 hour)