Siebel Si 204 - Photos & Videos

Σιεμπέλ Σι 204
Χώρα	Γερμανία
Πληκτρολογήστε	Ελαφρές μεταφορές/εκπαιδευτές
Πρώτη πτήση	25 Μαΐου 1940
Χτισμένο	1216

Teh Σιεμπέλ Σι 204 ήταν ένα μικρό δικινητήριο μεταγωγικό και εκπαιδευτικό αεροσκάφος που αναπτύχθηκε στον Β' Παγκόσμιο Πόλεμο. Βασίστηκε στο Fh 104 Hallore. Αρχικά σχεδιάστηκε ως απάντηση σε μια εντολή ανάπτυξης του Υπουργείου Αεροπορίας για ένα μικρό αεροσκάφος πολιτικών μεταφορών το 1938, τελικά παρήχθη για τη Luftwaffe.

Πηγή: Wikipedia

Aero C-3A Walk Around
Φωτογράφος	Pavel Senk
Εντοπισμού	Αγνοώ
Φωτογραφίες	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)
Ρόλο	Multi-Engine Trainer / Light Transport
Κατασκευαστής	Aero Vodochody (Czechoslovakia)
In Service (Post-War)	1945–c. 1960s
No. Built (C-3 Series)	541 (by Aero, plus 492 by BMM/ČKD)
Πλήρωμα	2 (Pilot and Co-pilot/Trainee)
Capacity (Passengers)	Up to 8 passengers (Civilian C-103 variant)
Μήκος	11.95 m (39 ft 2 in)
Εκπέτασμα	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).
Παραλλαγές:
- 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.