fbpx
Wikipedia

FMA AeC.1

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.

AeC.1
Role Utility aircraft
Manufacturer FMA
First flight 28 October 1931


Specifications edit

General characteristics

  • Crew: One pilot
  • Capacity: 2 passengers
  • Length: 7.75 m (25 ft 5 in)
  • Wingspan: 12.00 m (39 ft 4 in)
  • Height: 3.16 m (10 ft 4 in)
  • Wing area: 16.9 m2 (182 sq ft)
  • Empty weight: 700 kg (1,540 lb)
  • Gross weight: 1,120 kg (2,470 lb)
  • Powerplant: 1 × Armstrong Siddeley Mongoose , 112 kW (150 hp)

Performance

  • Maximum speed: 180 km/h (110 mph, 96 kn)
  • Range: 1,300 km (810 mi, 700 nmi)
  • Service ceiling: 4,300 m (14,100 ft)
  • Rate of climb: 3.3 m/s (660 ft/min)

References edit

  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 393.
  • World Aircraft Information Files. London: Bright Star Publishing. pp. File 894 Sheet 27.

External links edit

  Media related to Ae.C.1 at Wikimedia Commons

light, utility, aircraft, built, argentina, 1931, first, aircraft, domestic, design, produced, fabrica, militar, aviones, wing, cantilever, monoplane, conventional, configuration, with, fixed, tailskid, undercarriage, originally, designed, fully, enclosed, cab. 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 AeC 1 Role Utility aircraft Manufacturer FMA First flight 28 October 1931Specifications editGeneral characteristics Crew One pilot Capacity 2 passengers Length 7 75 m 25 ft 5 in Wingspan 12 00 m 39 ft 4 in Height 3 16 m 10 ft 4 in Wing area 16 9 m2 182 sq ft Empty weight 700 kg 1 540 lb Gross weight 1 120 kg 2 470 lb Powerplant 1 Armstrong Siddeley Mongoose 112 kW 150 hp Performance Maximum speed 180 km h 110 mph 96 kn Range 1 300 km 810 mi 700 nmi Service ceiling 4 300 m 14 100 ft Rate of climb 3 3 m s 660 ft min References editTaylor Michael J H 1989 Jane s Encyclopedia of Aviation London Studio Editions p 393 World Aircraft Information Files London Bright Star Publishing pp File 894 Sheet 27 External links edit nbsp Media related to Ae C 1 at Wikimedia Commons Retrieved from https en wikipedia org w index php title FMA AeC 1 amp oldid 1022456330, wikipedia, wiki, book, books, library,

article

, read, download, free, free download, mp3, video, mp4, 3gp, jpg, jpeg, gif, png, picture, music, song, movie, book, game, games.