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]
Falcon 2000LXS · Length
Single sourceConfiguration
| Specification | Aero L-59 Super Albatros | Dassault Falcon 2000 |
|---|---|---|
| Type | Military trainer aircraft COIN[source] | Business jet[source] |
| Manufacturer | Aero Vodochody[source] | Dassault Aviation Dassault Reliance Aerospace Limited (DRAL)[source] |
| Status | Out of production, in service[source] | Active in production[source] |
| Primary users | Czech Air Force Egyptian Air Force Tunisian Air Force[source] |
20.23 m (66 ft 4 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]
Falcon 2000LXS · 6 passengers, 2 crew, Mach .80
Single source7,408 km (4,603 mi, 4,000 nmi) (6 passengers, 2 crew, Mach .80)[source]
L-59E · 1 × Lotarev DV-2 turbofan thrust
Single source1 × Lotarev DV-2 turbofan , 21.57 kN (4,850 lbf) thrust[source]
Falcon 2000LXS · 2 × Pratt & Whitney Canada PW308C turbofan engines thrust each
Single source2 × Pratt & Whitney Canada PW308C turbofan engines, 31.14 kN (7,000 lbf) thrust each[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] | 675 (Oct 2022)[source] |
|---|
| Manufactured | 1986–1996[source] | 1995–present[source] |
|---|
| First flight | 30 September 1986[source] | 4 March 1993[source] |
|---|
| Developed from | Aero L-39 Albatros[source] | Dassault Falcon 900[source] |
|---|
| Variant | Aero L-159 ALCA[source] | — |
|---|
| Fuel capacity | 1,537 L (406 US gal; 338 imp gal) including tip tanks[source] | 16,660 lb (7,557 kg)[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 | — | France[source] |
|---|
| Capacity | — | 10 passengers[source] |
|---|
| Take-off distance | — | 1,425 m (4,675 ft)[source] |
|---|
| Landing distance | — | 689 m (2,260 ft) ((FAR 91, 6 pax, SL, NBAA IFR reserves)[source] |
|---|