Aero L-159 ALCA
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The Aero L-159 ALCA is a subsonic light combat aircraft and advanced trainer developed in the single-seat L-159A and two-seat L-159B versions, respectively, produced in the Czech Republic by Aero Vodochody. It was derived from the Aero L-59 Super Albatros trainer, which was in turn developed from the Aero L-39 Albatros series. Development of the L-159 started in 1993 as an initiative to replace various Soviet-era fighter aircraft with a modern Czech-built equivalent; it was decided against pursuing a clean-sheet design to avoid excessive costs. Development was supported by the Czech government, which ordered 72 L-159A single-seat aircraft for roughly 50 billion CZK to equip the Czech Air Force. In 1998, the Boeing Company became a strategic partner in both the project and Aero Vodochody itself. On 4 August 1997, the L-159 performed its maiden flight; on 10 April 2000, the first production aircraft was delivered to the Czech Air Force. Further development of the type proceeded, particularly of the twin-seat L-159 models. In 2003, the Czech fleet of 72 L-159A aircraft was reduced to 24 due to budget constraints. Following several years of storage, the Czech government has re-sold most of the redundant aircraft to both military and civilian operators, namely the Iraqi Air Force and Draken International. The L-159 has seen active combat use by the Iraqi Air Force against Islamic State of Iraq and the Levant (ISIS) insurgents in the country. In Draken's service, the L-159 (colloquially known as "Honey Badger") has been employed as an aggressor aircraft for pilot training. Since 2007, six L-159A aircraft have been rebuilt into T1 trainer derivatives. During 2017, Aero Vodochody formally restarted production of the type, and unveiled a newly built L-159T1 for the Iraqi Air Force; furthermore, the Czech Air Force was in the process of acquiring L-159T2 two-seaters.
Summary from Wikipedia, photo via Wikimedia Commons, licensed under CC BY-SA.
- Manufacturer
- AERO Vodochody Aerospace
- Category
- Attack aircraft
- First flight
- 1997-08-04
Specifications
- Cruise speed
- 505 kt
- Max speed
- 520 kt
- Range
- 850 nm
- Service ceiling
- 43,200 ft
- Rate of climb
- 12,000 ft/min
- Max takeoff weight
- 17,637 lb
- Empty weight
- 9,590 lb
- Fuel capacity
- 130 US gal
- Powerplant
- Honeywell/ITEC F124-GA-100
- Engines
- 1
- Seats
- 1
- Length
- 41.8 ft
- Wingspan
- 31.7 ft
- Height
- 16 ft
- Number built
- 72
Specifications are approximate and may vary by variant. Compiled from Wikipedia (CC BY-SA).
Reference and training only. Specifications vary by variant — consult the manufacturer and the official documents.