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Aero L-60 Brigadýr








Aero L-60 Brigadýr


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L-60 Brigadýr

L60 Brigadyr PICT0014.JPG
L60 as air ambulance at the Polish Aviation Museum
Role
Utility aircraft
Manufacturer

Aero
First flight
24 December 1953
Primary user
Czechoslovakian aviation
Produced
273

The Aero L-60 Brigadýr (Czech: Brigadier) was a small, high-wing 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 flat-six 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 by Aero, 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.




Contents





  • 1 Variants


  • 2 Operators

    • 2.1 Civil operators[1]


    • 2.2 Military operators



  • 3 Specifications (L-60)


  • 4 See also


  • 5 References


  • 6 External links




Variants[edit]



  • XL-60 : Prototype.


  • L-60 : Single-engined light utility transport, observation aircraft.


  • L-60A : 50 production aircraft for the Czech Air Force. Also known as the K-60. Armed with MG-15 7.92 mm machine gun in a rear cab. First flew on June 24, 1955.


  • L-60B : Agricultural crop spraying aircraft (300 l chemicals tank).


  • L-60D : Glider tug aircraft.


  • L-60E :Air ambulance aircraft.


  • L-60F : Glider tug aircraft.


  • L-60S : Aircraft fitted with the PZL-built 260-hp Ivchenko AI-14R radial piston engine.


  • L-60SF : Fitted with the M-462RF radial piston engine.


  • L-160 : Improved version with all-metal tail.


Operators[edit]



Civil operators[1][edit]



 Argentina


 Austria


 Bulgaria


 Cuba


 Czechoslovakia

  • Slov-Air

 East Germany


 Hungary

  • MÉM Flight Service used 2 L-60 (registered: HA-BRA, HA-BRB) from 1959 for short period.[citation needed]

 New Zealand


 People's Republic of China


 Poland


  • Polish Air Ambulance Service used 3 L-60F in 1957–1974

 Romania


 Soviet Union


 United Arab Emirates


 Yugoslavia


Military operators[edit]



 Czechoslovakia
  • Czechoslovakian Air Force

 East Germany
  • East German Air Force


Specifications (L-60)[edit]




Aero L-60S aerotows historical gliders


Data from Jane's All The World's Aircraft 1961–62[2]


General characteristics



  • Crew: One, pilot


  • Capacity: Three passengers


  • Length: 8.54 m (28 ft 0 in)


  • Wingspan: 13.96 m (45 ft 9½ in)


  • Height: 2.72 m (8 ft 11 in)


  • Wing area: 24.30 m² (261.6 ft²)


  • Airfoil: NACA 4412


  • Aspect ratio: 8.07:1


  • Empty weight: 968 kg (2,134 lb)


  • Loaded weight: 1,460 kg (3,219 lb)


  • Max. takeoff weight: 1,560 kg (3,439 lb)


  • Powerplant: 1 × Praga Doris M 208-B air-cooled flat-six, 142 kW (190 hp)

Performance



  • Maximum speed: 193 km/h (104 knots, 120 mph)


  • Cruise speed: 175 km/h (95 knots, 109 mph) at sea level


  • Stall speed: 52 km/h (28 knots, 32 mph)


  • Range: 720 km (389 nm, 447 miles)


  • Service ceiling: 4,200 m (13,780 ft)


  • Climb to 1,000 m (3,300 ft): 4.3 min


See also[edit]




Aircraft of comparable role, configuration and era


  • Dornier Do 27

  • Yakovlev Yak-12



References[edit]


Notes


  1. ^ Krzyżan, Marian, Samoloty w muzeach polskich, Warsaw: Wydawnictwa Komunikacji i Łączności, 1983, .mw-parser-output cite.citationfont-style:inherit.mw-parser-output qquotes:"""""""'""'".mw-parser-output code.cs1-codecolor:inherit;background:inherit;border:inherit;padding:inherit.mw-parser-output .cs1-lock-free abackground:url("//upload.wikimedia.org/wikipedia/commons/thumb/6/65/Lock-green.svg/9px-Lock-green.svg.png")no-repeat;background-position:right .1em center.mw-parser-output .cs1-lock-limited a,.mw-parser-output .cs1-lock-registration abackground:url("//upload.wikimedia.org/wikipedia/commons/thumb/d/d6/Lock-gray-alt-2.svg/9px-Lock-gray-alt-2.svg.png")no-repeat;background-position:right .1em center.mw-parser-output .cs1-lock-subscription abackground:url("//upload.wikimedia.org/wikipedia/commons/thumb/a/aa/Lock-red-alt-2.svg/9px-Lock-red-alt-2.svg.png")no-repeat;background-position:right .1em center.mw-parser-output .cs1-subscription,.mw-parser-output .cs1-registrationcolor:#555.mw-parser-output .cs1-subscription span,.mw-parser-output .cs1-registration spanborder-bottom:1px dotted;cursor:help.mw-parser-output .cs1-hidden-errordisplay:none;font-size:100%.mw-parser-output .cs1-visible-errorfont-size:100%.mw-parser-output .cs1-subscription,.mw-parser-output .cs1-registration,.mw-parser-output .cs1-formatfont-size:95%.mw-parser-output .cs1-kern-left,.mw-parser-output .cs1-kern-wl-leftpadding-left:0.2em.mw-parser-output .cs1-kern-right,.mw-parser-output .cs1-kern-wl-rightpadding-right:0.2em
    ISBN 978-83-206-0432-0



  2. ^ Taylor 1961, p. 35.



Bibliography

  • Taylor, John W. R. Jane's All The World's Aircraft 1961–62. London: Sampson Low, Marston & Company, 1961.


External links[edit]




  • Specs & Photo at Flugzeuginfo.net








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