The Aero L-39 Albatros was the successor to the earlier L-29 and, just like its predecessor, it became the standard trainer for the Warsaw Pact. The Albatros is a cantilever low-wing monoplane with dual tandem seats which is also capable of performing close support missions in both trainer and dedicated light attack versions, it was remarkable thanks to its simplistic modular design which made it easily repairable and servicable to the point that it can operate independently of ground facilities. Production of the basic L-39 continued into the 1990s after it was adopted by a large number of nations including Czechoslovakia, the USSR, most Warsaw Pact nations, and Soviet client states such as Afghanistan, Algeria, Cuba, Ethiopia, Iraq, Libya, Nigeria, Syria and Vietnam upon which production switched to the more advanced L-59 Super Albatros with a significant influx of Western avionics and equipment.
The first flight of the Albatros was undertaken by the second prototype on 4 November 1968. It entered service intially with the Czech air force in 1972 as the L-39C and was adopted by most Warsaw Pact nations shortly thereafter. Other variants included the L-39V target tug, the L-39Z0 weapons trainer (with combat capability) and the L-39ZA ground attack and reconnaissance version which featured reinforced landing gear and an underfuselage gun pod. The first attempt to install Western avionics and engines resulted in the L-139 which only reached the prototype stage. Nevertheless, this led to a significant upgrade known as the the L-39MS which was ultimately redesignated as the L-59 Super Albatros for export. The L-59 can be recognized by its elongated nose, lengthened fuselage and features a modern cockpit, more powerful engines, plus other structural improvements. Finally, the L-159 ALCA is a modern dedicated multi-role aircraft which is described in a separate entry.
Preceded by:
NoneSucceeded by:
NoneDesign | L-39ZA |
Name | Albatros |
Type | Close Support |
Year | 1974 |
Crew | 2 |
Dimensions | |
Length | 12.13 m |
Height | 4.770 m |
Wing Span | 9.46 m |
Wing Area | n/a |
Weight | |
Empty | 3,565 kg |
Maximum | 4,635 kg |
Wing Loading | 246.5 kg/m² |
Performance | |
Speed | 630 km/h |
Ceiling | 7,500 m |
Range | 1,100 km |
Powerplant | |
Engine | 1 x Al-25TL Ivchyenko 1,720 kgf |
Thrust/Weight | 0.44 |
Armament | |
Guns | 1 x 23-mm |
Payload | 1,100 kg |
Hardpoints | 4 |
Production | |
Built | n/a |
Total | 2,800 |