About: Aero L-60 Brigadýr   Sponge Permalink

An Entity of Type : dbkwik:resource/AGhloO_nVTaFp7GvOmHv5Q==, within Data Space : 134.155.108.49:8890 associated with source dataset(s)

The Aero L-60 Brigadýr () was a small, propeller-driven Czechoslovakian STOL utility aircraft developed for both civil and military use. A prototype, designated XL-60, with Argus As 10C engine, first flew on December 24, 1953, but it was not successful. The plane was thoroughly redesigned and the second improved prototype, with M-208B engine, flew on June 8, 1954. The aircraft's configuration bears a strong resemblance to the Fieseler Fi 156 "Storch" licence-produced in Czechoslovakia during and after World War II (as K-65 Čáp), and which this aircraft was intended to replace. By the end of production in 1960, 273 had been built, including an improved version, the L-160 with an all-metal tail.

AttributesValues
rdf:type
rdfs:label
  • Aero L-60 Brigadýr
rdfs:comment
  • The Aero L-60 Brigadýr () was a small, propeller-driven Czechoslovakian STOL utility aircraft developed for both civil and military use. A prototype, designated XL-60, with Argus As 10C engine, first flew on December 24, 1953, but it was not successful. The plane was thoroughly redesigned and the second improved prototype, with M-208B engine, flew on June 8, 1954. The aircraft's configuration bears a strong resemblance to the Fieseler Fi 156 "Storch" licence-produced in Czechoslovakia during and after World War II (as K-65 Čáp), and which this aircraft was intended to replace. By the end of production in 1960, 273 had been built, including an improved version, the L-160 with an all-metal tail.
sameAs
dcterms:subject
dbkwik:military/pr...iPageUsesTemplate
max takeoff weight alt
  • 3439.0
loaded weight main
  • 1460.0
airfoil
  • NACA 4412
number of props
  • 1(xsd:integer)
length alt
  • 853.44
span main
  • 13.96 m
Produced
  • 273(xsd:integer)
cruise speed main
  • 175.0
more performance
  • 258.0
cruise speed alt
  • 95(xsd:integer)
height alt
  • 271.78000000000003
primary user
  • Czechoslovakian aviation
Type
  • Utility aircraft
type of prop
  • air-cooled flat-six
range alt
  • 389(xsd:integer)
length main
  • 8.54 m
power alt
  • 190.0
area main
  • 24.3
power main
  • 142.0
stall speed alt
  • 28(xsd:integer)
height main
  • 2.72 m
span alt
  • 45(xsd:integer)
range main
  • 720.0
Manufacturer
max speed main
  • 193.0
engine (prop)
  • Praga Doris M 208-B
Capacity
  • Three passengers
ceiling main
  • 4,200 m
empty weight main
  • 968.0
aspect ratio
  • 8(xsd:double)
stall speed main
  • 52.0
loaded weight alt
  • 3219.0
area alt
  • 261.6
First Flight
  • 1953-12-24(xsd:date)
max speed alt
  • 104(xsd:integer)
jet or prop?
  • prop
empty weight alt
  • 2134.0
plane or copter?
  • plane
ceiling alt
  • 13780.0
max takeoff weight main
  • 1560.0
cruise speed more
  • at sea level
Crew
  • One, pilot
ref
  • Jane's All The World's Aircraft 1961–62
abstract
  • The Aero L-60 Brigadýr () was a small, propeller-driven Czechoslovakian STOL utility aircraft developed for both civil and military use. A prototype, designated XL-60, with Argus As 10C engine, first flew on December 24, 1953, but it was not successful. The plane was thoroughly redesigned and the second improved prototype, with M-208B engine, flew on June 8, 1954. The aircraft's configuration bears a strong resemblance to the Fieseler Fi 156 "Storch" licence-produced in Czechoslovakia during and after World War II (as K-65 Čáp), and which this aircraft was intended to replace. By the end of production in 1960, 273 had been built, including an improved version, the L-160 with an all-metal tail. Aircraft retrofitted with a PZL-built Ivchenko AI-14R radial engine are known as the L-60S.
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