FMA Ae.C.1
1931
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FMA Ae.C.1

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Specification 
 CREW1
 PASSENGERS2
 ENGINE1 x 150hp Armstrong Siddeley Mongoose
 WEIGHTS
    Take-off weight1120 kg2469 lb
    Empty weight700 kg1543 lb
 DIMENSIONS
    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
 PERFORMANCE
    Max. speed171 km/h106 mph
    Cruise speed154 km/h96 mph
    Ceiling4300 m14100 ft
    Range1300 km808 miles

Comments
lucas, 28.10.2012

ese era mi argentina !!!!!

KenBrit, 30.04.2012

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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