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]
A310 MRTT · Length
Single sourceConfiguration
| Specification | Aero L-59 Super Albatros | Airbus A310 MRTT |
|---|---|---|
| Type | Military trainer aircraft COIN[source] | Multi-role tanker / transport[source] |
| Manufacturer | Aero Vodochody[source] | Airbus Military SAS , Airbus Deutschland, Lufthansa Technik[source] |
| Status | Out of production, in service[source] | Active service[source] |
| Primary users | Czech Air Force Egyptian Air Force Tunisian Air Force[source] |
47.4 m (155 ft 6 in)[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; A310 MRTT · Empty weight
Single sourceMaximum take-off; A310 MRTT · 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]
L-59E · 1 × Lotarev DV-2 turbofan thrust
Single source1 × Lotarev DV-2 turbofan , 21.57 kN (4,850 lbf) thrust[source]
A310 MRTT · 2 × General Electric CF6-80C2 or Pratt & Whitney PW4152 turbofan jet engines thrust each
Single source2 × General Electric CF6-80C2 or Pratt & Whitney PW4152 turbofan jet engines , 262 kN (59,000 lbf) thrust each[source]
L-59E · Wing area
Single source18.80 m 2 (202.4 sq ft)[source]
L-59E · Service ceiling
Single source11,800 m (38,700 ft)[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.
German Air Force Royal Canadian Air Force[source] |
| Number built | 80[source] | 6, (from existing A310-300C airframes)[source] |
|---|
| Manufactured | 1986–1996[source] | — |
|---|
| First flight | 30 September 1986[source] | December 2003[source] |
|---|
| Developed from | Aero L-39 Albatros[source] | Airbus A310-300C[source] |
|---|
| Variant | Aero L-159 ALCA[source] | Airbus CC-150 Polaris[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 | — |
|---|
| Designer | — | Airbus Military SAS[source] |
|---|
| Introduction date | — | October 2004[source] |
|---|
| Successors | — | Airbus A330 MRTT[source] |
|---|
| Capacity | — | 214 passengers / 40,000 kg (88,000 lb) deliverable fuel / 36,000 kg (79,000 lb) cargo[source] |
|---|