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 | PAC P-750 XSTOL |
|---|---|---|
| Type | Military trainer aircraft COIN[source] | Utility aircraft[source] |
| Manufacturer | Aero Vodochody[source] | Pacific Aerospace[source] |
| Status | Out of production, in service[source] | Active, in production[source] |
| Primary users | Czech Air Force Egyptian Air Force Tunisian Air Force[source] |
11.11 m (36 ft 5 in)[source]
1 × Pratt & Whitney Canada PT6 A-34 turboprop
Single source1 × Pratt & Whitney Canada PT6 A-34 turboprop , 560 kW (750 hp)[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] | 120[source] |
|---|
| Manufactured | 1986–1996[source] | 2001–present[source] |
|---|
| First flight | 30 September 1986[source] | 2001[source] |
|---|
| Developed from | Aero L-39 Albatros[source] | PAC Cresco[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] | 107 km/h (66 mph, 58 kn) Idle Power, 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 | — | New Zealand[source] |
|---|
| Capacity | — | Pilot + nine passengers or 17 parachutists[source] |
|---|
| Aspect ratio | — | 6.59[source] |
|---|
| Take-Off Ground Roll | — | 220 m (720 ft) (ISA, SL)[source] |
|---|
| Landing Ground Roll (excl. approach from 15 m AGL) | — | 166 m (545 ft) (SL)[source] |
|---|