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 | Learjet 45 |
|---|---|---|
| Type | Military trainer aircraft COIN[source] | Business jet[source] |
| Manufacturer | Aero Vodochody[source] | Bombardier Aerospace[source] |
| Status | Out of production, in service[source] | Active[source] |
| Primary users | Czech Air Force Egyptian Air Force Tunisian Air Force[source] |
58 ft 0 in (17.68 m)[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] | 642[source] |
|---|
| Manufactured | 1986–1996[source] | 1995–2012[source] |
|---|
| First flight | 30 September 1986[source] | 7 October 1995[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] | — |
|---|
| 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 | — | Canada/United States[source] |
|---|
| Introduction date | — | Mid-1998[source] |
|---|
| Developed into | — | Learjet 40 Learjet 70/75[source] |
|---|
| Capacity | — | 9 passengers[source] |
|---|