FMA Ae.C.1


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FMA Ae.C.1

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 ENGINE1 x 150hp Armstrong Siddeley Mongoose
  Take-off weight1120 kg2469 lb
  Empty weight700 kg1543 lb
  Wingspan12.00 m39 ft 4 in
  Length7.75 m25 ft 5 in
  Height3.16 m10 ft 4 in
  Wing area19.00 m2204.51 sq ft
  Max. speed171 km/h106 mph
  Cruise speed154 km/h96 mph
  Ceiling4300 m14100 ft
  Range1300 km808 miles

lucas, e-mail, 28.10.2012 02:26

ese era mi argentina !!!!!


KenBrit, 30.04.2012 23:45

The FMA AeC.1 was a light utility aircraft built in Argentina in 1931; it was the first aircraft of domestic design to be produced by FMA. It was a low-wing cantilever monoplane of conventional configuration with fixed tailskid undercarriage. As originally designed, the fully enclosed cabin had three seats, but this was later reduced to two. The passenger seat could be readily removed to make way for a stretcher to facilitate its use as an air ambulance.


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