Skip to content
Vincony — fast, managed web hosting for your next site
The Pilots Desk
Attack aircraftlight attack aircraft

Aero L-159 ALCA

Aero L-159 ALCA

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.

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.