Credit
Michal šenki · Public domain · Resized · Public domain · Source ↗ · Modified
FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Measured figures
L-59E · Length
Single source12.20 m (40 ft 0 in)[source]
Length
Single sourceConfiguration
| Specification | Aero L-59 Super Albatros | Antonov An-178 |
|---|---|---|
| Type | Military trainer aircraft COIN[source] | Military transport aircraft[source] |
| Manufacturer | Aero Vodochody[source] | Antonov[source] |
| Status | Out of production, in service[source] | In development[source] |
| Primary users | Czech Air Force Egyptian Air Force Tunisian Air Force[source] |
32.23 m (105 ft 9 in)[source]
L-59E · at 7,000 m (23,000 ft) (with maximum internal and external fuel)
Single source2,000 km (1,200 mi, 1,100 nmi) at 7,000 m (23,000 ft) (with maximum internal and external fuel)[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 · 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] | 1 as of 2020[source] |
|---|
| Manufactured | 1986–1996[source] | — |
|---|
| First flight | 30 September 1986[source] | 7 May 2015[source] |
|---|
| Developed from | Aero L-39 Albatros[source] | Antonov An-158[source] |
|---|
| Variant | Aero L-159 ALCA[source] | — |
|---|
| Fuel capacity | 1,537 L (406 US gal; 338 imp gal) including tip tanks[source] | 14,650 kg (32,298 lb)[source] |
|---|
| Stall speed | 185 km/h (115 mph, 100 kn) (flaps down)[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 | — | Ukraine[source] |
|---|
| Designer | — | Antonov[source] |
|---|
| Built by | — | Antonov Serial Production Plant[source] |
|---|
| Capacity | — | 90 soldiers, 70 paratroopers, 48 on stretchers +15 seated, 8 medical modules and 12, or 16 tons of cargo, overload variant 18 tons.[source] |
|---|
| Powerplant | — | 2 × Progress D-436 -148FM turbofans[source] |
|---|
| Max landing weight | — | 47,000 kg (103,617 lb)[source] |
|---|
| Thrust each | — | 73.55 kN (16,534 lbf)[source] |
|---|
| Required field length (ISA, SL) | — | 2,500 m (8,200 ft)[source] |
|---|