Siebel Si 204

Siebel Si 204
Paese	Germania
digitare	Trasporto leggero/addestratore
Primo volo	25 maggio 1940
Costruito	1216

Le Siebel Si 204 era un piccolo aereo bimotore da trasporto e addestramento sviluppato durante la seconda guerra mondiale. Era basato sull'Fh 104 Hallore. Originariamente progettato in risposta a un ordine di sviluppo del Ministero dell'Aviazione per un piccolo aereo da trasporto civile nel 1938, fu infine prodotto per la Luftwaffe.

fonte: Wikipedia

Aero C-3A Walk Around
Fotografo	Pavel Senk
Localizzazione	Inconsapevole
Foto	41

Aero C-3A 1

Aero C-3A 2

Aero C-3A 3

Aero C-3A 4

Aero C-3A 5

Aero C-3A 6

Aero C-3A 7

Aero C-3A 8

Aero C-3A 9

Click on a photo and use the mouse scroll to view all photos

Aspetta, cercando Siebel Si 204 per te...

Vedi anche:

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)
Ruolo	Multi-Engine Trainer / Light Transport
Produttore	Aero Vodochody (Czechoslovakia)
In Service (Post-War)	1945–c. 1960s
No. Built (C-3 Series)	541 (by Aero, plus 492 by BMM/ČKD)
Equipaggio	2 (Pilot and Co-pilot/Trainee)
Capacity (Passengers)	Up to 8 passengers (Civilian C-103 variant)
Lunghezza	11.95 m (39 ft 2 in)
Apertura alare	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).
Varianti:
- 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.