The Aero L159 ALCA is developed by the Czech Republic as a Light multi-role fighter and lead in fighter trainer. The first L159 (two seater) flew August 4th 1997, and the first single seater on August 18th 1998.
In a fast track the first L159 was delivered in April 2000.
Developing Nation: | Czech Republic |
Task: | Light multi-role fighter and lead in fighter trainer |
First Flight: | – two seater: August 4th 1997 – single seater: August 18th 1998 – first production airframe: October 20th 1999 |
First Delivery: | April 2000 |
Crew: | – 1 – 2 in tandem (L 159T) |
Wing Span: | 9,54 m |
Wing Area: | 18,8 m² |
Length: | 12,72 m |
Height: | 4,77 m |
Engine (s): | Honeywell/ITEC F124-GA-100 non afterburning turbofan with 28,2 kN thrust (1x) |
Weight: | 4320 kg |
Max.Take off weight: | 8000 kg |
Fuel: | – internal fuel L 159A: 1596 kg – internal fuel L 159B: 1273 kg |
Max. Speed: | 936 km/h |
Max. Range: | 2530 km including external fuel |
Ceiling: | ~14000 m |
Weapons: | 7 external hard points, up to 2340 kg weaponry like AIM9 sidewinders, AAM’s, AGM-65 Maverick ASM’s, Gun pods, rockets and bombs |
Extra: | Czech Republic is the only operator up to now (feb. 2004) of the L 159 (72 x) |
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