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]
Citation XLS+ · Length
Single sourceConfiguration
| Specification | Aero L-59 Super Albatros | Cessna Citation Excel |
|---|---|---|
| Type | Military trainer aircraft COIN[source] | Business jet[source] |
| Manufacturer | Aero Vodochody[source] | Cessna Textron Aviation[source] |
| Status | Out of production, in service[source] | Active In production[source] |
| Primary users | Czech Air Force Egyptian Air Force Tunisian Air Force |
52 ft 6 in (16.0 m)[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; Citation XLS+ · Empty weight
Single sourceMaximum take-off; Citation XLS+ · Max takeoff weight
Single sourceL-59E · 1 × Lotarev DV-2 turbofan thrust
Single source1 × Lotarev DV-2 turbofan , 21.57 kN (4,850 lbf) thrust[source]
Citation XLS+ · 2 × Pratt & Whitney Canada PW545C turbofans thrust each
Single source2 × Pratt & Whitney Canada PW545C turbofans , 4,119 lbf (18.32 kN) thrust each[source]
L-59E · Wing area
Single source18.80 m 2 (202.4 sq ft)[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[source] |
|---|
| Manufactured | 1986–1996[source] | 1996–present[source] |
|---|
| First flight | 30 September 1986[source] | 29 February 1996[source] |
|---|
| Developed from | Aero L-39 Albatros[source] | Cessna Citation V / Cessna Citation X[source] |
|---|
| Variant | Aero L-159 ALCA[source] | — |
|---|
| Fuel capacity | 1,537 L (406 US gal; 338 imp gal) including tip tanks[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 | — |
|---|
| Developed into | — | Cessna Citation Sovereign[source] |
|---|
| Capacity | — | 9 passengers / 7,400 lb (3,357 kg) useful load[source] |
|---|
| National origin | — | United States[source] |
|---|