Siebel Si 204

Siebel Si 204
Land	Duitsland
Type	Licht transport/trainer
Eerste vlucht	25 mei 1940
Gebouwd	1216

De Siebel Si 204 was een klein tweemotorig transport- en trainingsvliegtuig ontwikkeld in de Tweede Wereldoorlog. Het was gebaseerd op de Fh 104 Hallore. Oorspronkelijk ontworpen als reactie op een ontwikkelingsorder van het Ministerie van Luchtvaart voor een klein civiel transportvliegtuig in 1938, werd het uiteindelijk geproduceerd voor de Luftwaffe.

Bron: Wikipedia

Aero C-3A Walk Around
Fotograaf	Pavel Senk
Lokalisatie	Onbewust
Foto 's	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

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