Aero C-3A

Siebel Si 204

PaysGermany
TypeTransport léger/formateur
Premier vol25 mai 1940
Construit1216

Lla Siebel Si 204 était un petit avion bimoteur de transport et d’entraînement développé pendant la Seconde Guerre mondiale. Il était basé sur le Fh 104 Hallore. Conçu à l’origine en réponse à une commande de développement du ministère de l’Aviation pour un petit avion de transport civil en 1938, il a finalement été produit pour la Luftwaffe.

Source: Wikipedia

Aero C-3A Walk Around
PhotographePavel Senk
LocalisationInconnu
Photos41
Attendez, à la recherche de Siebel Si 204 pour vous...

Smer Siebel Si 204 A (1/72 Maquette, 0929) - Amazon

Voir aussi :

Seconde Guerre mondiale : l’histoire visuelle définitive de la Blitzkrieg à la bombe atomique (DK Definitive Visual Histories) - Amazon Carte par carte de la Seconde Guerre mondiale (carte par carte de l’histoire du Danemark) - Amazon


General Characteristics

The Aero C-3A was the Czechoslovak post-war production variant of the German Siebel Si 204D, a small, twin-engined transport and instrument trainer aircraft. Production took place at the Aero and ČKD-Praga plants during the German occupation and continued after the liberation of Czechoslovakia. The C-3A variant was specifically used by the Czechoslovak Air Force for training pilots on multi-engine aircraft, earning the nickname « Sibly. »

Property Typical Value (Aero C-3A)
Rôle Multi-Engine Trainer / Light Transport
Fabricant Aero Vodochody (Czechoslovakia)
In Service (Post-War) 1945–c. 1960s
No. Built (C-3 Series) 541 (by Aero, plus 492 by BMM/ČKD)
Crew 2 (Pilot and Co-pilot/Trainee)
Capacity (Passengers) Up to 8 passengers (Civilian C-103 variant)
Length 11.95 m (39 ft 2 in)
Envergure 21.28 m (69 ft 10 in)
Max Takeoff Weight 5,600 kg (12,346 lb)

Design and Powerplant

  • Engines: Two Argus As 411TA-1 12-cylinder, inverted V-12 air-cooled piston engines (Often referred to as M-411 in Czechoslovakia).
  • Power Output (each): Approximately 426 kW (571 hp) to 433 kW (580 hp).
  • Structure: All-metal low-wing cantilever monoplane. It featured a distinctive twin vertical stabilizer tail unit (similar to its predecessor, the Si 204).
  • Landing Gear: Fully retractable main landing gear, folding into the engine nacelles, plus a fixed tail wheel.
  • Cockpit: The C-3A trainer variant had dual controls and a « stepped » cockpit canopy similar to the original Si 204, providing good visibility for both pilot and instructor.

Performance and Service

  • Maximum Speed: Up to 359 km/h (223 mph, 194 knots).
  • Max Cruise Speed: 319 km/h (198 mph, 172 knots).
  • Service Ceiling: 7,500 m (24,606 ft).
  • Range: Approximately 1,600 km (994 mi, 864 nmi).
  • Variantes:
    • C-3A: Trainer version with dual controls (the subject of this request).
    • C-3B: Bombardier training version, equipped with a bomb sight and a defensive machine gun turret.
    • C-103: Civilian passenger transport variant.
  • Other Uses: C-3 aircraft were also used for non-military purposes, including fighting forest pests and crushing ice on the Danube River.

Vues : 1368

Ecrire un commentaire

<a href="" title=""> <abbr title=""> <acronym title=""> <b> <blockquote cite=""> <cite> <code> <del datetime=""> <em> <i> <q cite=""> <s> <strike> <strong> 

requis

Ce site utilise Akismet pour réduire les indésirables. En savoir plus sur comment les données de vos commentaires sont utilisées.