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Avia B-158

The Avia B.158 was a prototype Czechoslovak twin-engined light bomber aircraft of the 1930s. Only a single example was built and it was abandoned, following the German occupation of Czechoslovakia in March 1939.

Avia B.158
Role light bomber
National origin Czechoslovakia
Manufacturer Avia
First flight 1938
Number built 1

Development and design

In 1935, the Czech aircraft company Avia produced the B-58 design for a small twin-engined bomber with a fixed undercarriage, powered by two 313 kW (420 hp) Avia Rk.17 radial engines. This design was abandoned in 1936 and replaced by a more powerful and advanced derivative, the Avia B.158, which was designed to meet a requirement from the Czechoslovak Ministry of National Defense (MNO) for a high performance medium bomber, capable of operation during both day and night, and competing against Aero Vodochody's A.300.[1][2]

In 1937, Avia started to build a single prototype of the B-158, a three-seat low-winged monoplane with inverted gull-wings, a retractable tailwheel undercarriage and 634 kW (850 hp) Avia (Hispano-Suiza) 12Ydrs engines, making its maiden flight in mid-1938.[2] It was fitted with a twin-tail to give a better field of fire for the dorsal gun position.[3]

While the competing Aero A.300 gave superior performance, neither had entered into production by the time Germany completed its conquest of Czechoslovakia. After testing by the Luftwaffe at their test centre at Rechlin, the prototype B-158 was scrapped in 1940.[1][3]

Specifications (B.158)

Data from Plane Facts:One-off Czech [2]

General characteristics

  • Crew: three
  • Length: 12.00 m (39 ft 4 in)
  • Wingspan: 16.00 m (52 ft 6 in)
  • Height: 5.20 m (17 ft 1 in) [3]
  • Wing area: 43.00 m2 (462.8 sq ft)
  • Empty weight: 4,300 kg (9,480 lb)
  • Gross weight: 6,600 kg (14,551 lb)
  • Max takeoff weight: 7,260 kg (16,006 lb)
  • Powerplant: 2 × Avia (Hispano-Suiza) 12Ydrs liquid-cooled V12 engine, 630 kW (850 hp) each

Performance

  • Maximum speed: 435 km/h (270 mph, 235 kn)
  • Cruise speed: 365 km/h (227 mph, 197 kn)
  • Range: 1,100 km (680 mi, 590 nmi)
  • Service ceiling: 8,500 m (27,900 ft)
  • Rate of climb: 7.00 m/s (1,378 ft/min)

Armament

  • Guns: 3×7.92 mm vz.30 (Česká zbrojovka Strakonice) machine guns in nose, dorsal and ventral positions
  • Bombs: 1,000 kg (2,200 lb)

See also

Related development

References

Notes
  1. ^ a b "Avia B-158 December 21, 2009, at the Wayback Machine". Samaloty Wojskowe Świata 1935-1945. (In Polish). Retrieved 14 December 2009.
  2. ^ a b c Air International January 1981, p.48.
  3. ^ a b c "Avia B-158". УГОЛОК НЕБА. (In Russian) Retrieved 14 December 2009.
Bibliography

External links

  • AVIA B-158 (In Czech)

avia, avia, prototype, czechoslovak, twin, engined, light, bomber, aircraft, 1930s, only, single, example, built, abandoned, following, german, occupation, czechoslovakia, march, 1939, avia, 158role, light, bombernational, origin, czechoslovakiamanufacturer, a. The Avia B 158 was a prototype Czechoslovak twin engined light bomber aircraft of the 1930s Only a single example was built and it was abandoned following the German occupation of Czechoslovakia in March 1939 Avia B 158Role light bomberNational origin CzechoslovakiaManufacturer AviaFirst flight 1938Number built 1 Contents 1 Development and design 2 Specifications B 158 3 See also 4 References 5 External linksDevelopment and design EditIn 1935 the Czech aircraft company Avia produced the B 58 design for a small twin engined bomber with a fixed undercarriage powered by two 313 kW 420 hp Avia Rk 17 radial engines This design was abandoned in 1936 and replaced by a more powerful and advanced derivative the Avia B 158 which was designed to meet a requirement from the Czechoslovak Ministry of National Defense MNO for a high performance medium bomber capable of operation during both day and night and competing against Aero Vodochody s A 300 1 2 In 1937 Avia started to build a single prototype of the B 158 a three seat low winged monoplane with inverted gull wings a retractable tailwheel undercarriage and 634 kW 850 hp Avia Hispano Suiza 12Ydrs engines making its maiden flight in mid 1938 2 It was fitted with a twin tail to give a better field of fire for the dorsal gun position 3 While the competing Aero A 300 gave superior performance neither had entered into production by the time Germany completed its conquest of Czechoslovakia After testing by the Luftwaffe at their test centre at Rechlin the prototype B 158 was scrapped in 1940 1 3 Specifications B 158 EditData from Plane Facts One off Czech 2 General characteristicsCrew three Length 12 00 m 39 ft 4 in Wingspan 16 00 m 52 ft 6 in Height 5 20 m 17 ft 1 in 3 Wing area 43 00 m2 462 8 sq ft Empty weight 4 300 kg 9 480 lb Gross weight 6 600 kg 14 551 lb Max takeoff weight 7 260 kg 16 006 lb Powerplant 2 Avia Hispano Suiza 12Ydrs liquid cooled V12 engine 630 kW 850 hp eachPerformance Maximum speed 435 km h 270 mph 235 kn Cruise speed 365 km h 227 mph 197 kn Range 1 100 km 680 mi 590 nmi Service ceiling 8 500 m 27 900 ft Rate of climb 7 00 m s 1 378 ft min Armament Guns 3 7 92 mm vz 30 Ceska zbrojovka Strakonice machine guns in nose dorsal and ventral positions Bombs 1 000 kg 2 200 lb See also Edit Aviation portalRelated development Aero A 300References EditNotes a b Avia B 158 Archived December 21 2009 at the Wayback Machine Samaloty Wojskowe Swiata 1935 1945 In Polish Retrieved 14 December 2009 a b c Air International January 1981 p 48 a b c Avia B 158 UGOLOK NEBA In Russian Retrieved 14 December 2009 Bibliography Plane Facts One off Czech Air International January 1981 Vol 20 No 1 p 48 External links Edit Wikimedia Commons has media related to Avia B 158 AVIA B 158 In Czech Retrieved from https en wikipedia org w index php title Avia B 158 amp oldid 993809837, wikipedia, wiki, book, books, library,

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