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FMA AeC.2

The FMA AeC.2 was a light utility aircraft built in Argentina in the early 1930s, and also produced as a military trainer and observation aircraft under the designations AeME.1, AeMO.1, AeMOe.1 and AeMOe.2.

AeC.2 and derivatives
Role Utility aircraft
Manufacturer FMA
First flight 18 April 1932
Number built 71

Development

The design was derived from the AeC.1, but instead of an enclosed cabin, featured two open cockpits in tandem. Only two of the civil AeC.2s were built, but these were followed by seven AeME.1 trainers. Six of the AeME.1s, plus one of the AeC.2s, participated in a long-distance publicity tour of Brazil as part of the "Sol de Mayo" squadron.

 
AeMOe.1

In 1934, a version with a revised empennage, the AeMO.1, was developed as an observation machine; 41 examples of which were delivered from July onwards. Some of these were armed with a trainable .303 Vickers machine gun in the observer's cockpit, and some with twin synchronised machine guns in the forward fuselage.

Six AeMOe.1s followed, for crew training in the Observation role, which were generally similar in design but featuring a NACA cowling for the engine, and then the definitive AeMOe.2 version appeared in 1937 with a further refined empennage, 61 examples of which were built.

 
AeMS.1 prototype

Also based on the AeMOe.1, the sole AeMS.1 was an air ambulance version with an enclosed cabin that could carry four stretchers and an attendant.


Variants

  • AeC.2 (Civil) - civil version (2 built)
  • AeME.1 (Militar de Entrenamiento) - military trainer (7 built)
  • AeMO.1 (Militar de Observación) - military observation aircraft (41 built)
  • AeMOe.1 (Militar de Observación y Entrenamiento) - military observation and trainer aircraft (6 built)
  • AeMOe.2 - military observation and trainer aircraft (14 built)
  • AeMS.1 - (Militar Sanitario) - military air ambulance (1 built)


Specifications (AeME.1)

General characteristics

  • Crew: Two, pilot and instructor
  • Length: 7.90 m (25 ft 11 in)
  • Wingspan: 12.00 m (39 ft 4 in)
  • Height: 2.70 m (8 ft 10 in)
  • Wing area: 16.9 m2 (182 sq ft)
  • Empty weight: 650 kg (1,430 lb)
  • Gross weight: 1,130 kg (2,490 lb)
  • Powerplant: 1 × Wright R-760 , 180 kW (240 hp)

Performance

  • Maximum speed: 220 km/h (140 mph, 120 kn)
  • Range: 1,500 km (930 mi, 810 nmi)
  • Service ceiling: 5,000 m (16,400 ft)
  • Rate of climb: 4.2 m/s (820 ft/min)

See also

Related lists

References

  • 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

  Media related to FMA Ae. C.2 at Wikimedia Commons

this, article, includes, list, references, related, reading, external, links, sources, remain, unclear, because, lacks, inline, citations, please, help, improve, this, article, introducing, more, precise, citations, 2017, learn, when, remove, this, template, m. This article includes a list of references related reading or external links but its sources remain unclear because it lacks inline citations Please help to improve this article by introducing more precise citations May 2017 Learn how and when to remove this template message The FMA AeC 2 was a light utility aircraft built in Argentina in the early 1930s and also produced as a military trainer and observation aircraft under the designations AeME 1 AeMO 1 AeMOe 1 and AeMOe 2 AeC 2 and derivativesRole Utility aircraftManufacturer FMAFirst flight 18 April 1932Number built 71 Contents 1 Development 2 Variants 3 Specifications AeME 1 4 See also 5 References 6 External linksDevelopment EditThe design was derived from the AeC 1 but instead of an enclosed cabin featured two open cockpits in tandem Only two of the civil AeC 2s were built but these were followed by seven AeME 1 trainers Six of the AeME 1s plus one of the AeC 2s participated in a long distance publicity tour of Brazil as part of the Sol de Mayo squadron AeMOe 1 In 1934 a version with a revised empennage the AeMO 1 was developed as an observation machine 41 examples of which were delivered from July onwards Some of these were armed with a trainable 303 Vickers machine gun in the observer s cockpit and some with twin synchronised machine guns in the forward fuselage Six AeMOe 1s followed for crew training in the Observation role which were generally similar in design but featuring a NACA cowling for the engine and then the definitive AeMOe 2 version appeared in 1937 with a further refined empennage 61 examples of which were built AeMS 1 prototype Also based on the AeMOe 1 the sole AeMS 1 was an air ambulance version with an enclosed cabin that could carry four stretchers and an attendant Variants EditAeC 2 Civil civil version 2 built AeME 1 Militar de Entrenamiento military trainer 7 built AeMO 1 Militar de Observacion military observation aircraft 41 built AeMOe 1 Militar de Observacion y Entrenamiento military observation and trainer aircraft 6 built AeMOe 2 military observation and trainer aircraft 14 built AeMS 1 Militar Sanitario military air ambulance 1 built Specifications AeME 1 EditGeneral characteristics Crew Two pilot and instructor Length 7 90 m 25 ft 11 in Wingspan 12 00 m 39 ft 4 in Height 2 70 m 8 ft 10 in Wing area 16 9 m2 182 sq ft Empty weight 650 kg 1 430 lb Gross weight 1 130 kg 2 490 lb Powerplant 1 Wright R 760 180 kW 240 hp Performance Maximum speed 220 km h 140 mph 120 kn Range 1 500 km 930 mi 810 nmi Service ceiling 5 000 m 16 400 ft Rate of climb 4 2 m s 820 ft min See also EditRelated lists List of Interwar military aircraftReferences 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 Media related to FMA Ae C 2 at Wikimedia Commons Retrieved from https en wikipedia org w index php title FMA AeC 2 amp oldid 1018208698, wikipedia, wiki, book, books, library,

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