Latin American Military - Argentina - Gendarmería Nacional Argentina - RACA/Hughes 500

Revised: February 1, 1999
Copyright © 1997-1999 by Juan Carlos Barroux R.

<Will be completed!>

RACA/Hughes 500

RACA/Hughes 500 multirole helicopter

Designation: RACA/Hughes 500
Manufacturer: RACA, Argentina under license from Hughes, 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
GN-908    A07053     ---           --      --         --

RACA/Hughes 500C multirole helicopter

Designation: RACA/Hughes 500C
Manufacturer: RACA, Argentina under license from Hughes, 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
GN-909    A07665     ---           --      --         --
GN-910    A08165     ---           --      --         --
GN-911    ---        ---           --      --         --

RACA/Hughes 500D multirole helicopter

Designation: RACA/Hughes 500D
Manufacturer: RACA, Argentina under license from Hughes, 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
GN-918    ---        ---           --      --         --

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