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)