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- FMA_AeC.1 abstract "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.".
- FMA_AeC.1 manufacturer Fábrica_Argentina_de_Aviones.
- FMA_AeC.1 numberBuilt "1".
- FMA_AeC.1 type Utility_aircraft.
- FMA_AeC.1 wikiPageID "16455294".
- FMA_AeC.1 wikiPageLength "4176".
- FMA_AeC.1 wikiPageOutDegree "8".
- FMA_AeC.1 wikiPageRevisionID "668360081".
- FMA_AeC.1 wikiPageWikiLink Aircraft.
- FMA_AeC.1 wikiPageWikiLink Argentina.
- FMA_AeC.1 wikiPageWikiLink Armstrong_Siddeley_Mongoose.
- FMA_AeC.1 wikiPageWikiLink Category:Argentine_civil_utility_aircraft_1930–1939.
- FMA_AeC.1 wikiPageWikiLink Category:FMA_aircraft.
- FMA_AeC.1 wikiPageWikiLink Fábrica_Argentina_de_Aviones.
- FMA_AeC.1 wikiPageWikiLink Utility_aircraft.
- FMA_AeC.1 wikiPageWikiLinkText "AeC.1".
- FMA_AeC.1 wikiPageWikiLinkText "FMA AeC.1".
- FMA_AeC.1 capacity "2".
- FMA_AeC.1 ceilingFt "14100".
- FMA_AeC.1 ceilingM "4300".
- FMA_AeC.1 climbRateFtmin "660".
- FMA_AeC.1 climbRateMs "3.3".
- FMA_AeC.1 crew "One pilot".
- FMA_AeC.1 emptyWeightKg "700".
- FMA_AeC.1 emptyWeightLb "1540".
- FMA_AeC.1 eng1Hp "150".
- FMA_AeC.1 eng1Kw "112".
- FMA_AeC.1 eng1Number "1".
- FMA_AeC.1 eng1Type Armstrong_Siddeley_Mongoose.
- FMA_AeC.1 firstFlight "1931-10-28".
- FMA_AeC.1 grossWeightKg "1120".
- FMA_AeC.1 grossWeightLb "2470".
- FMA_AeC.1 heightFt "10".
- FMA_AeC.1 heightIn "4".
- FMA_AeC.1 heightM "3.16".
- FMA_AeC.1 lengthFt "25".
- FMA_AeC.1 lengthIn "5".
- FMA_AeC.1 lengthM "7.75".
- FMA_AeC.1 manufacturer Fábrica_Argentina_de_Aviones.
- FMA_AeC.1 maxSpeedKmh "180".
- FMA_AeC.1 maxSpeedMph "110".
- FMA_AeC.1 metOrEng%3F_ "met".
- FMA_AeC.1 numberBuilt "1".
- FMA_AeC.1 rangeKm "1300".
- FMA_AeC.1 rangeMiles "810".
- FMA_AeC.1 spanFt "39".
- FMA_AeC.1 spanIn "4".
- FMA_AeC.1 spanM "12".
- FMA_AeC.1 type "Utility aircraft".
- FMA_AeC.1 wikiPageUsesTemplate Template:Aerospecs.
- FMA_AeC.1 wikiPageUsesTemplate Template:Aircontent.
- FMA_AeC.1 wikiPageUsesTemplate Template:Avyear.
- FMA_AeC.1 wikiPageUsesTemplate Template:Cite_book.
- FMA_AeC.1 wikiPageUsesTemplate Template:Commons_category-inline.
- FMA_AeC.1 wikiPageUsesTemplate Template:FMA_aircraft.
- FMA_AeC.1 wikiPageUsesTemplate Template:Infobox_Aircraft_Type.
- FMA_AeC.1 wingAreaSqft "182".
- FMA_AeC.1 wingAreaSqm "16.9".
- FMA_AeC.1 subject Category:Argentine_civil_utility_aircraft_1930–1939.
- FMA_AeC.1 subject Category:FMA_aircraft.
- FMA_AeC.1 hypernym Aircraft.
- FMA_AeC.1 type Aircraft.
- FMA_AeC.1 type MeanOfTransportation.
- FMA_AeC.1 type Redirect.
- FMA_AeC.1 type Product.
- FMA_AeC.1 type DesignedArtifact.
- FMA_AeC.1 type Thing.
- FMA_AeC.1 type Q11436.
- FMA_AeC.1 comment "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.".
- FMA_AeC.1 label "FMA AeC.1".
- FMA_AeC.1 sameAs Q5426614.
- FMA_AeC.1 sameAs m.03y6cl1.
- FMA_AeC.1 sameAs FMA_Ae._C.1.
- FMA_AeC.1 sameAs FMA_AeC.1.
- FMA_AeC.1 sameAs Q5426614.
- FMA_AeC.1 wasDerivedFrom FMA_AeC.1?oldid=668360081.
- FMA_AeC.1 isPrimaryTopicOf FMA_AeC.1.