Aero L-60 Brigadyr

Year of manufacture: 1960
Full restoration: 2015
Chassis: 150911
Engine: Praga Doris M208-M
Registration: LY-EZE
Original registration: HB-EZE

L-60 .pdf

Model History

In the late 1940s, the Czechoslovak Air Force still perated K-65 Čap STOP aircraft a local copy of the 1936 Fieseler Fi 156 Storch, manufactured by Orličan in Chocen. As it became obsolete, 1951 the Czehoslovak Ministry of Defence opened a competition for new liaison and utility aircraft. That contest was won by project named LB-60 and propsed by engineer Ondrej Nenec. The first prototype was tested in 1953. Initially the L-60 was powered by Praga Doris engine, also known as Walter M-208, designed by Jaroslav Kruliš. This engine provided to be unreliable, and majority of the L-60s underwent engine uprades in 1970s, by replacing original powerplant with Polish made Ivchenko AI-14RA radial engine.

Technical Data

  • ICAO code: 60
  • Classification: L1P
  • Category: L/G
  • Predecessor: K65 Čap
  • Prototype: December 1953
  • Type: STOL
  • Years of produced: 1956-1959
  • Aircrafts produced: 273
  • Manufacturer: Aero (CZE)
  • Engine: Praga Doris M208-B, 220hp
  • Engine type: air cooled 6 cylinder flat
  • Also called: Orličan L-60 Brygadyr
  • Persons on board: 4
  • Lenght: 8.54 m
  • Wingspan: 13.96 m
  • Height: 2.72 m
  • Wings area: 24.30 m2
  • Empty weight: 1,460 kg
  • Max takeoff weight: 1,560 kg
  • Maximum speed: 193 km/h (104 kn)
  • Criuse speed: 175 km/h (94 kn)
  • Stoll speed: 52 km/h (28 kn)
  • Range: 720 km at 1000 m
  • Service ceiling: 4,200 m (13,800 ft)