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]
Tarragon · Length
Single sourceConfiguration
| Specification | Aero L-59 Super Albatros | Pelegrin Tarragon |
|---|---|---|
| Type | Military trainer aircraft COIN[source] | Ultralight aircraft[source] |
| Manufacturer | Aero Vodochody[source] | Pelegrin Limited[source] |
| Status | Out of production, in service[source] | In production (2018)[source] |
| Primary users | Czech Air Force Egyptian Air Force Tunisian Air Force[source] |
7.53 m (24 ft 8 in)[source]
Tarragon · 1 × Rotax 912ULS four cylinder, liquid and air-cooled, four stroke aircraft engine
Single source1 × Rotax 912ULS four cylinder, liquid and air-cooled, four stroke aircraft engine , 75 kW (101 hp)[source]
L-59E · 1 × Lotarev DV-2 turbofan thrust
Single source1 × Lotarev DV-2 turbofan , 21.57 kN (4,850 lbf) thrust[source]
L-59E · Wing area
Single source18.80 m 2 (202.4 sq ft)[source]
L-59E · Service ceiling
Single source11,800 m (38,700 ft)[source]
L-59E · 5,510 ft/min
Single source28.0 m/s (5,510 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| — |
| Number built | 80[source] | — |
|---|
| Manufactured | 1986–1996[source] | — |
|---|
| First flight | 30 September 1986[source] | — |
|---|
| Developed from | Aero L-39 Albatros[source] | Millennium Master[source] |
|---|
| Variant | Aero L-159 ALCA[source] | — |
|---|
| Fuel capacity | 1,537 L (406 US gal; 338 imp gal) including tip tanks[source] | 96 litres (21 imp gal; 25 US gal)[source] |
|---|
| Stall speed | 185 km/h (115 mph, 100 kn) (flaps down)[source] | 65 km/h (40 mph, 35 kn)[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 | — | Latvia[source] |
|---|
| Capacity | — | one passenger[source] |
|---|
| Propellers | — | 3-bladed constant speed propeller[source] |
|---|
| Never exceed speed | — | 370 km/h (230 mph, 200 kn)[source] |
|---|