Credit
Michal šenki · Public domain · Resized · Public domain · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
L-59E · Length
Single source12.20 m (40 ft 0 in)[source]
Virus 912 SW 100 · Length
Single sourceConfiguration
| Specification | Aero L-59 Super Albatros | Pipistrel Virus |
|---|---|---|
| Type | Military trainer aircraft COIN[source] | General aviation aircraft[source] |
| Manufacturer | Aero Vodochody[source] | Pipistrel[source] |
| Status | Out of production, in service[source] | In production[source] |
| Primary users | Czech Air Force Egyptian Air Force Tunisian Air Force[source] |
6.5 m (21 ft 4 in)[source]
Empty; L-59E · includes gun
Single sourceMaximum take-off; L-59E · Max takeoff weight
Single source4,030 kg (8,885 lb) (includes gun)[source]
7,000 kg (15,432 lb)[source]
Empty; Virus 912 SW 100 · Empty weight
Single sourceMaximum take-off; Virus 912 SW 100 · Max takeoff weight
Single sourceMaximum; L-59E · at 5,000 m (16,000 ft)
Single source865 km/h (537 mph, 467 kn) at 5,000 m (16,000 ft)[source]
Virus 912 SW 100 · 1 × Rotax 912 ULS
Single source1 × Rotax 912 ULS , 75 kW (100 hp)[source]
L-59E · 1 × Lotarev DV-2 turbofan thrust
Single source1 × Lotarev DV-2 turbofan , 21.57 kN (4,850 lbf) thrust[source]
Virus 912 SW 100 · Endurance
Single source5.3 hours[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| — |
| Number built | 80[source] | 1000 (Sinus and Virus family total, March 2019)[source] |
|---|
| Manufactured | 1986–1996[source] | 1999-present[source] |
|---|
| First flight | 30 September 1986[source] | August 10, 1999 ( 1999-08-10 )[source] |
|---|
| Developed from | Aero L-39 Albatros[source] | Pipistrel Sinus[source] |
|---|
| Variant | Aero L-159 ALCA[source] | Pipistrel Velis Electro[source] |
|---|
| Fuel capacity | 1,537 L (406 US gal; 338 imp gal) including tip tanks[source] | 100 litres (22 imp gal; 26 US gal)[source] |
|---|
| Stall speed | 185 km/h (115 mph, 100 kn) (flaps down)[source] | 79 km/h (49 mph, 43 kn) without flaps[source] |
|---|
| Guns | one GSh-23L cannon in under-fuselage pod[source] | — |
|---|
| Hardpoints | four underwing hardpoints with a capacity of inner hardpoints 500 kg (1,100 lb)capacity, outer hardpoints 250 kg (550 lb)[source] | — |
|---|
| Country of origin | Czechoslovakia[source]Inventory Origin column; table 1, row 26, cell 2; revision 1374778711; retrieved 2026-10-01 | — |
|---|
| National origin | — | Slovenia[source] |
|---|
| Capacity | — | one passenger[source] |
|---|
| Aspect ratio | — | 11.3[source] |
|---|
| Never exceed speed | — | 302 km/h (188 mph, 163 kn)[source] |
|---|
| g limits | — | +4/-2[source] |
|---|
| Maximum glide ratio | — | 17:1[source] |
|---|