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The FMA AeC.3 was a light utility aircraft built in Argentina in 1934; a further development in the series of designs that had originated with the AeC.1 three years previously. Like its immediate predecessor the AeC.2 the AeC.3 was an open-cockpit variant of the family and was distinguished mainly in its use of an Armstrong Siddeley Genet Major engine. Deliveries to Argentina's aeroclubs were made late in the year.

The FMA AeC.3 was a light utility aircraft built in Argentina in 1934; a further development in the series of designs that had originated with the AeC.1

Made by Fabrica Argentina de Aviones.

Empty Weight Lb
1480
Wing Area Sqm
19
Eng 1 Type
Armstrong Siddeley Genet Major
Max Speed Mph
105
Ceiling Ft
14700
Eng 1 Kw
97
Span In
4
Gross Weight Lb
2125
Capacity
1
Crew
One pilot
Climb Rate Ftmin
840
Empty Weight Kg
670
Gross Weight Kg
964
Height In
2
Range Km
700
Climb Rate Ms
4
Manufacturer
Fabrica Argentina de Aviones
Range Miles
430
First Flight
27
Max Speed Kmh
170
Height Ft
8
Span Ft
40
Wing Area Sqft
205
Met Or Eng
met
Span M
12
Length Ft
26
Height M
3
Ceiling M
4500
Eng 1 Hp
130
Eng 1 Number
1
Length In
11
Length M
8
Category
Argentine civil utility aircraft 1930-1939
FMA aircraft

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