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]
F.27 · Length
Single sourceConfiguration
| Specification | Aero L-59 Super Albatros | Fokker F27 Friendship |
|---|---|---|
| Type | Military trainer aircraft COIN[source] | Regional airliner[source] |
| Manufacturer | Aero Vodochody[source] | Fokker[source] |
| Status | Out of production, in service[source] | In limited service[source] |
| Primary users | Czech Air Force Egyptian Air Force Tunisian Air Force[source] |
25.06 m (82 ft 3 in)[source]
F.27 · 2 × Rolls-Royce Dart Mk.532-7 two-stage centrifugal compressor turboprop each
Single source2 × Rolls-Royce Dart Mk.532-7 two-stage centrifugal compressor turboprop, 1,678 kW (2,250 hp) each[source]
L-59E · 1 × Lotarev DV-2 turbofan thrust
Single source1 × Lotarev DV-2 turbofan , 21.57 kN (4,850 lbf) thrust[source]
L-59E · Service ceiling
Single source11,800 m (38,700 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] | 586[source] |
|---|
| Manufactured | 1986–1996[source] | 1955–1987[source] |
|---|
| First flight | 30 September 1986[source] | 24 November 1955[source] |
|---|
| Developed from | Aero L-39 Albatros[source] | — |
|---|
| Variant | Aero L-159 ALCA[source] | Fairchild F-27/FH-227[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 | — | Netherlands[source] |
|---|
| Introduction date | — | 19 November 1958[source] |
|---|
| Developed into | — | Fokker 50[source] |
|---|
| Capacity | — | 44-52 passengers[source] |
|---|