FMA AeC.3
title: "FMA AeC.3" type: doc version: 1 created: 2026-02-28 author: "Wikipedia contributors" status: active scope: public tags: ["1930s-argentine-civil-utility-aircraft", "fma-aircraft", "aircraft-with-fixed-conventional-landing-gear", "single-engined-piston-aircraft", "low-wing-aircraft", "single-engined-tractor-aircraft"] topic_path: "arts/film" source: "https://en.wikipedia.org/wiki/FMA_AeC.3" license: "CC BY-SA 4.0" wikipedia_page_id: 0 wikipedia_revision_id: 0
::data[format=table title="Infobox aircraft"]
| Field | Value |
|---|---|
| name | AeC.3 and AeC.4 |
| aircraft_type | Utility aircraft |
| manufacturer | FMA |
| number_built | 16 |
| first_flight | 27 March 1934 |
| :: |
| name = AeC.3 and AeC.4 | logo = | logo_size = | image = | alt = | caption = | long_caption = | other_names = | aircraft_type = Utility aircraft | aim = | outcome = | related = | national_origin = | manufacturer = FMA | design_group = | designer = | builder = | issuer = | status = | owners = | primary_user = | more_users = | service = | major_applications = | proposals = | prototypes = | number_built = 16 | construction_number = | civil_registration = | military_serial = | radio_code = | requirement = | aircraft_carried = | flights = | total_hours = | total_distance = | construction_date = | introduction = | retired = | first_flight = 27 March 1934 | initiated = | in_service = | last_flight = | expected = | developed_from = | variants = | developed_into = | preservation = | fate = | predecessors = | successors = | concluded = The FMA AeC.3 was a light utility aircraft built in Argentina in 1934. The AeC.3 was a further development in the series of designs that had originated with the AeC.1 three years previously. Deliveries to Argentina's aeroclubs were made in late 1934.
Development
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 Warner Scarab engine.
On 21 January 1936, a refined version flew as the AeC.3G, with an uprated 145 HP Armstrong Siddeley Genet Major engine. The main innovation introduced on this aircraft was the use of flaps, the first Argentine aircraft to be so equipped. This aircraft first flew as an open-cockpit type, but later had a roof fitted to create an enclosed cabin.
A further development, the last in this family of aircraft, was the AeC.4 that flew on 17 October. This was essentially an AeC.3G with improved aerodynamics, and only a single example was built.
Operational history
In 1935, Carola Lorenzini set a South American altitude record of 5,500 m (18,040 ft) in an AeC.3, and another aircraft of this type was flown by Santiago Germanó to win the aerobatics prize at the Resistencia air meet the same year. A final feat for the AeC.3 for 1935 was its use by Pedro B. Mórtola in a long-distance round-trip flight between Buenos Aires and Rio Gallegos, covering 5,200 km in 37 hours 20 minutes.
Variants
- AeC.3 – version powered by a 125 HP Warner Scarab engine
- AeC.3G – AeC.3 powered by a 145 HP Armstrong Siddeley Genet Major engine, and fitted with flaps
- AeC.4 – AeC.3G with improved aerodynamics
Specifications (AeC.3)
|prime units? = met |crew=One pilot |capacity=1 passenger |length m=8.20 |length ft=26 |length in=11 |span m=12.30 |span ft=40 |span in=4 |height m=2.50 |height ft=8 |height in=2 |wing area sqm=19.0 |wing area sqft=205 |empty weight kg=670 |empty weight lb=1,480 |gross weight kg=964 |gross weight lb=2,125 |eng1 number=1 |eng1 name=Armstrong Siddeley Genet Major |eng1 kw=97 |eng1 hp=130 |max speed kmh=170 |max speed mph=105 |range km=700 |range miles=430 |ceiling m=4,500 |ceiling ft=14,700 |climb rate ms=4.2 |climb rate ftmin=840
|see also= |related= |similar aircraft= |lists=
References
References
- Stahl, Guillermo A.. (2012-03-01). "An Evaluation of the Argentinean Basic Trainer Aircraft Domestic Development Project". [[Air Force Institute of Technology]].
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