Specifications (Lasta 95N and 95V-54)
Data from VTI - Military Technical Institute Belgrade
General characteristics
- Crew: Two, student and instructor
- Length: 7.965 m (26 feet 1 in)
- Wingspan: 9.702 m (31 ft 10 in)
- Height: 2.84 m (9 ft 4 in)
- Wing area: 12.9 m² (138.85 ft²)
- Empty weight: 888 kg (1958 lb)
- Max. takeoff weight: 1210 kg (2668 lb)
- Powerplant: 1 × Lycoming AEIO-540-L1.B5D or Lycoming AEIO-580-B1A six-cylinder horizontally opposed air cooled, 300 hp Lycoming AEIO-540 (315 hp Lycoming AEIO-580)
- Propellers: two blade, variable pitch, constant speed HARTZELL HC-C2YR-4CF/FC 8475-6 propeller
Performance
- Never exceed speed: 425 km/h (229 knots, 264 mph)
- Maximum speed: 345 km/h (186 knots, 214 mph)
- Cruise speed: 320 km/h (173 knots, 200 mph)
- Stall speed: 95 km/h (51 knots, 59 mph)
- Range: 1160 km (721 miles)
- Service ceiling: 6000 m (20000 ft)
- Rate of climb: 8.5 m/s (1,673 ft/min)
- Limit load factor: +6/-3 g
Armament
- Hardpoints: 2 (one under each wing) holding either 100 kg bombs, 7.62 mm or 12.7 mm caliber gun pods or 57mm rocket pods (7 rockets each)
Read more about this topic: Utva Lasta