Avia S-199

ยท Avia Motors
Length
8.94 m
Flat Wing Span
9.92 m
Height
2.59 m
Flat Wing Area
16.5 m²
Max Speed
528 km/h
Number of Engines
1
First Flight
1947-03-01
Number Built
603
Maximum Take-Off Weight
3.736 t (paragliders: kg)
Maximum Range
860 km

Pictures

No pictures yet for this family.

Aircraft Weight Variants

Aircraft Maximum Take-Off Weight (t (paragliders: kg)) Maximum Range (km)
Avia S-199 3.736 860

Similar airplanes

Name Aircraft Engine Length (m) Flat Wing Span (m)
Bell P-39 Airacobra 9.144 10.3632 Compare
Caudron Type B Gnome Omega 9 10 Compare
Boulton Paul P.120 Rolls-Royce Nene 8.8392 10.0584 Compare
Breda A.1 Colombo E.150 9 10.2 Compare
Arado SSD I BMW VI 8.5 10 Compare
Bell XFL Airabonita Allison V-1710 9.07 10.67 Compare
All data (22 fields)
Name
Avia S-199
Manufacturer
Avia Motors
Description
The Avia S-199 is a propeller-driven Messerschmitt Bf 109G-based fighter aircraft built after World War II using the Bf 109G airframe and a Junkers Jumo 211F engine in place of the original and unavailable Daimler-Benz DB 605 engine.
First Flight
1947-03-01
Production End
1949-01-01
Service End
1957-01-01
Designer
Messerschmitt
Type
Fighter aircraft
Length (m)
8.94
Height (m)
2.59
Cockpit Crew
1
Max Speed (km/h)
528
Rate of Climb (m/s)
13.7
Armament
2 × 13 mm MG 131 machine guns; 2 × MG 151/20 cannon; 1 × 250 kg (551 lb) ::or; 4 × 70 kg (155 lb) bombs
National Origin
Czechoslovakia
Number Built
603
Powerplant Description
1 × Junkers Jumo 211F V-12 inverted liquid-cooled piston engine, 1007 kW (1350 hp) each
Primary Users
Czechoslovak Air Force, Israeli Air Force
Wikipedia Article (URL)
en.wikipedia.org/wiki/Avia_S-199
Flat Wing Span (m)
9.92
Flat Wing Area (m²)
16.5
Number of Engines
1