Aero L-59 Super Albatros

· Aero Vodochody · 1 × Lotarev DV-2

Airplanes

Length

12.2 m

Flat Wing Span

9.54 m

Height

4.77 m

Flat Wing Area

18.8 m²

Max Speed

865 km/h

Max Ceiling

11800 m

Number of Engines

Aircraft Engine

First Flight

1986-09-30

Number Built

Maximum Take-Off Weight

7 t (paragliders: kg)

Total Fuel Capacity

1537

Maximum Range

2000 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Aero L-59 Super Albatros	7	1537	2000

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)
PZL-Mielec Lim-6		11.36	9.628	Compare
Soko G-4 Super Galeb	Armstrong Siddeley Viper	12.25	9.88	Compare
Lockheed XFV		11.23	9.4	Compare
Hawker P.1052		11.8872	9.4488	Compare
Aero L-159 ALCA		12.72	9.54	Compare
McDonnell Douglas T-45 Goshawk		11.8872	9.144	Compare

All data (24 fields)

Name: Aero L-59 Super Albatros
Manufacturer: Aero Vodochody
Description: The Aero L-59 Super Albatros (also known as the L-39MS Albatros) is a military jet trainer produced by the Czechoslovak aerospace manufacturer Aero Vodochody.
First Flight: 1986-09-30
Production End: 1996-01-01
Designer: Aero Vodochody
Type: Military trainer aircraft, COIN
Length (m): 12.2
Height (m): 4.77
Cockpit Crew: 2
Max Speed (km/h): 865
Min Speed (km/h): 185
Max Ceiling (m): 11800
Rate of Climb (m/s): 27.9908
Armament: one GSh-23L cannon in under-fuselage pod; four underwing hardpoints
Number Built: 80
Powerplant Description: 1 × Lotarev DV-2 turbofan, 21.57 kN thrust each
Primary Users: Czech Air Force, Egyptian Air Force , Tunisian Air Force
Status: Out of production, in service
Wikipedia Article (URL): en.wikipedia.org/wiki/Aero_L-59_Super_Albatros
Flat Wing Span (m): 9.54
Flat Wing Area (m²): 18.8
Aircraft Engine: Lotarev DV-2
Number of Engines: 1