FMA AeC.1
title: "FMA AeC.1" type: doc version: 1 created: 2026-02-28 author: "Wikipedia contributors" status: active scope: public tags: ["1930s-argentine-civil-utility-aircraft", "fma-aircraft", "low-wing-aircraft", "single-engined-piston-aircraft", "aircraft-with-fixed-conventional-landing-gear", "aircraft-first-flown-in-1931", "single-engined-tractor-aircraft"] topic_path: "arts/film" source: "https://en.wikipedia.org/wiki/FMA_AeC.1" license: "CC BY-SA 4.0" wikipedia_page_id: 0 wikipedia_revision_id: 0
::data[format=table title="Infobox aircraft"]
| Field | Value |
|---|---|
| name | AeC.1 |
| image | FMA Ae. C.1 Prototipo.jpg |
| aircraft_type | Utility aircraft |
| manufacturer | FMA |
| first_flight | 28 October 1931 |
| :: |
| name = AeC.1 | logo = | logo_size = | image = FMA Ae. C.1 Prototipo.jpg | 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 = | construction_number = | civil_registration = | military_serial = | radio_code = | requirement = | aircraft_carried = | flights = | total_hours = | total_distance = | construction_date = | introduction = | retired = | first_flight = 28 October 1931 | initiated = | in_service = | last_flight = | expected = | developed_from = | variants = | developed_into = | preservation = | fate = | predecessors = | successors = | concluded = 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 Fabrica Militar de Aviones (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.
Specifications
|prime units? = met |crew=One pilot |capacity=2 passengers |length m=7.75 |length ft=25 |length in=5 |span m=12.00 |span ft=39 |span in=4 |height m=3.16 |height ft=10 |height in=4 |wing area sqm=16.9 |wing area sqft=182 |empty weight kg=700 |empty weight lb=1,540 |gross weight kg=1,120 |gross weight lb=2,470 |eng1 number=1 |eng1 name=Armstrong Siddeley Mongoose |eng1 kw=112 |eng1 hp=150 |max speed kmh=180 |max speed mph=110 |range km=1,300 |range miles=810 |ceiling m=4,300 |ceiling ft=14,100 |climb rate ms=3.3 |climb rate ftmin=660
|see also= |related= |similar aircraft= |lists=
References
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