Revised: February 1, 1999
Copyright © 1997-1999 by Juan Carlos Barroux R.
The first 4 arrived in 1981 completed by a second batch of 4 in 1983. They all are in use with the Escuela de Aviación del Ejército (Campo de Mayo, Buenos Aires) as basic helicopter trainers.
Designation: Fairchild Hiller UH-12E.4 Manufacturer: Fairchild Hiller, U.S.A. Crew: Seats: Engine: x Engine Type: Turboshaft Engine Thrust: kW ( shp) Rotors: bladed main rotor and bladed trail rotor Main Rotor Diameter: m Main Rotor Disk Area: square meters Fuselage Length: m Height: m Empty Weight: kg Max. Weight MTOW: kg Max. Weight with Sling: kg Max. Speed at Sea Level: Max. Cruising Speed: km/h Normal Cruising Speed: km/h Ceiling: Range on Internal Fuel: km Range with Max. Fuel: km Range with Max. Payload: km Combat Radius: km () Radar: EW: Avionics: Weapons: Notes: S/N C/N Unit Built Bought Disposition Notes AE-356 5133 EscAvEj -- -- -- AE-357 5138 EscAvEJ -- -- -- AE-358 5139 EscAvEJ -- -- -- AE-359 5140 EscAvEJ -- -- -- AE-360 -- EscAvEJ -- -- -- AE-361 -- EscAvEJ -- -- -- AE-362 -- EscAvEJ -- -- -- AE-363 -- EscAvEJ -- -- --
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Copyright © 1997-1999 by Juan Carlos Barroux R.
Juan Carlos Barroux R. - lamilitary@geocities.com