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]
Cessna S550 Citation S/II · Length
Configuration
| Specification | Aero L-59 Super Albatros | Cessna Citation II |
|---|---|---|
| Type | Military trainer aircraft COIN[source] | Corporate jet[source] |
| Manufacturer | Aero Vodochody[source] | Cessna[source] |
| Status | Out of production, in service[source] | — |
| Primary users | Czech Air Force Egyptian Air Force Tunisian Air Force[source] | — |
| Number built | 80 |
47 ft 8 + 1 ⁄ 2 in (14.542 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; Cessna S550 Citation S/II · Empty weight
Single sourceMaximum take-off; Cessna S550 Citation S/II · Max takeoff weight
Single sourceL-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]
Cessna S550 Citation S/II · with max fuel
Single source1,998 nmi (2,299 mi, 3,700 km) (with max fuel)[source]
L-59E · 1 × Lotarev DV-2 turbofan thrust
Single source1 × Lotarev DV-2 turbofan , 21.57 kN (4,850 lbf) thrust[source]
Cessna S550 Citation S/II · 2 × Pratt & Whitney Canada JT15D -4B turbofans thrust each
Single source2 × Pratt & Whitney Canada JT15D -4B turbofans , 2,500 lbf (11 kN) thrust each[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
1184: 688 II and II/SP, 160 S/II, 336 Bravo[source] |
| Manufactured | 1986–1996[source] | 1978–2006[source] |
|---|
| First flight | 30 September 1986[source] | January 31, 1977[source] |
|---|
| Developed from | Aero L-39 Albatros[source] | Cessna Citation I[source] |
|---|
| Variant | Aero L-159 ALCA[source] | — |
|---|
| Fuel capacity | 1,537 L (406 US gal; 338 imp gal) including tip tanks[source] | 862 US gal (718 imp gal; 3,260 L) usable fuel[source] |
|---|
| Stall speed | 185 km/h (115 mph, 100 kn) (flaps down)[source] | 82 kn (94 mph, 152 km/h) ( CAS )[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 | — | United States[source] |
|---|
| Developed into | — | Cessna Citation V[source] |
|---|
| Capacity | — | Six to eight passengers[source] |
|---|
| Airfoil | — | NACA 23000[source] |
|---|