SK.ATO.18

THE FLEET OF OUR AIRCRAFT

PS28 CRUISER
OM-SCA , OM-SCN

The PS28 Cruiser aircraft is an all-metal low-flying aircraft used in our country as the main type for flying training. Both aircraft used in our country are equipped identically, except for small details. The aircraft is powered by a Rotax 912 ULS engine with an output of 100 horsepower. The cabin consists of modern instrumentation so-called. glass cockpit with screens from the company DYNON consisting of the flight display EFIS D100 and engine data display EMS 120. In the middle of the instrument panel is GPS GARMIN 695. Both aircraft are equipped with a parachute rescue system from BRS.

Technical specifications

  • Engine: Rotax 912 ULS
  • Power: 73.5 kW, 100 HP at 5800 RPM
  • Fuel: Mogas RON 95, Avgas 100LL, EN 228
  • MTOW: 600 kg (1320 lbs)
  • Empty weight (Classic in standard configuration): 388 kg (855.4 lbs)
  • Speed in 3000ft at 75% power: 93 KIAS (172 km / h)
  • Max. Horizon speed: 119 KIAS (220 km / h)
  • VNE: 138 KIAS (255 km / h)
  • Falling speed VSO: 31 KIAS (55 km / h)
  • Climb: 825 ft / min (4.2 m / s)
  • Take-off distance at 50ft (15m)
    • Concrete: 1270 ft (387 m)
    • Grass: 1499 ft (457 m)
  • Range (with 30 min. Reserve): 516 NM (953 km)
  • Endurance: 5 hours 25 min
  • Tank capacity: 114 l (30 US gal.)
  • Average fuel consumption: 17.5 l / h (4.6 US gal./1 hour)

DIAMOND DA40D Star
OM-SCB

The Diamond DA40D is a composite low-flying aircraft with a four-member cabin layout for a pilot and three passengers. It is powered by a 155 horsepower Centurion 2.0 diesel engine using JET A1 fuel. The cabin is equipped with two GARMIN 1000 image displays. The aircraft is also able to fly according to IFR rules.

Technical specifications

  • Engine: Centurion 2.0S
  • Power: 114kW, 155 HP at 2300 RPM
  • Fuel: JET A1, Diesel
  • MTOW: 1150 kg (2535.32 lbs)
  • Empty weight (Classic in standard configuration): 830 kg (1829.84 lbs)
  • Max. VNO horizon speed: 129 KIAS (239 km / h)
  • VNE: 178 KIAS (330 km / h)
  • Falling speed VSO: 49 KIAS (91 km / h)
  • Climb: 690 ft / min (3.5 m / s)
  • Take-off distance on concrete: 1214 ft (370 m)
  • Range (with 30 min. Reserve): 741 NM (1372 km)
  • Endurance: 5 hours
  • Tank capacity: 106 l (28 US gal.)
  • Average fuel consumption: 20 l / h (5.5 US gal./1 hour)

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