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]
Length
Single sourceConfiguration
| Specification | Aero L-59 Super Albatros | Indonesian Aerospace N219 |
|---|---|---|
| Type | Military trainer aircraft COIN[source] | Utility aircraft[source] |
| Manufacturer | Aero Vodochody[source] | Indonesian Aerospace[source] |
| Status | Out of production, in service[source] | In production[source] |
| Primary users | Czech Air Force Egyptian Air Force Tunisian Air Force[source] |
16.49 m (54 ft 1 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]
2 × Pratt & Whitney Canada PT6A-42 turboprop engines (850 shp) each
Single source2 × Pratt & Whitney Canada PT6A-42 turboprop engines, 630 kW (850 shp) each[source]
L-59E · 1 × Lotarev DV-2 turbofan thrust
Single source1 × Lotarev DV-2 turbofan , 21.57 kN (4,850 lbf) thrust[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| — |
| Number built | 80[source] | 2 prototypes (December 2024)[source] |
|---|
| Manufactured | 1986–1996[source] | 2017–present[source] |
|---|
| First flight | 30 September 1986[source] | 16 August 2017[source] |
|---|
| Developed from | Aero L-39 Albatros[source] | — |
|---|
| Variant | Aero L-159 ALCA[source] | — |
|---|
| Fuel capacity | 1,537 L (406 US gal; 338 imp gal) including tip tanks[source] | 1,600 kg[source] |
|---|
| Stall speed | 185 km/h (115 mph, 100 kn) (flaps down)[source] | 109 km/h (68 mph, 59 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 | — | Indonesia[source] |
|---|
| Capacity | — | 19 passengers[source] |
|---|
| Propellers | — | 4-bladed Hartzell Propeller aluminum autofeathering or 5-bladed MT-Propeller CFRP autofeathering[source] |
|---|
| g limits | — | -1.2 g to +3.0 g (flaps retracted)[source] |
|---|
| Takeoff distance | — | 435 meters (1,427 feet)[source] |
|---|
| Landing distance | — | 509 meters (1,670 feet)[source] |
|---|
| Alternative designation | — | N219[source] |
|---|