Circa 1932
Inter-Wars
Avia 10A
Circa 1929, the single-seat AVIA 10 A designed by Jarlaud at the Béchereau works.
Azionaria Vercellese Industrie Aeronautiche / Avia
Vercellese Industrie Aeronautiche
Azionaria Vercellese Industrie Aeronautiche / Avia
In 1929, Charles Fauvel participated in the creation of AVIA with Massenet, Auger and a few friends; this was a committee founded to promote the development of soaring. He then left the air force to join AVIA as sport director.
Azionaria Vercellese Industrie Aeronautiche; first flew F.L.3 two-seat cabin monoplane in 1939, and 400 built between 1939 and 1942.
Vercellese Industrie Aeronautiche was formed at Vercelli about 1940 to produce F.L.3 light tourer.
In 1946-1947 was renamed AVIA (Azionaria Vercellese Industrie Aeronautiche), continuing to develop F.L.3. Production resumed after the war, until the end of 1947, when company was absorbed by Francis Lombardi. Types known as Lombardi (AVIA) included L.M.5 Aviastar, first produced 1945.
Avia Rk.17

As well as producing aircraft and building Hispano-Suiza and Lorraine aero-engines under licence, Avia also designed and built their own radial engines. The Rk.17 was a 9-cylinder supercharged model, rated at 360 hp / 270 kW. It was a nine-cylinder version of their Rk.12.
It was a conventional air-cooled radial: nitrided steel barrels with integral fins were screwed into heat treated Y alloy heads. The pistons were also of heat treated Y alloy. The crankcase was cast from heat treated silumin alloy, with some minor parts using magnesium alloy. The single throw two piece crankshaft was linked to the pistons with an I-section Y alloy master rod, with a single piece big end, which carried the other eight piston rods.
Applications
Avia Ba.122
Letov Š-50
Specifications
Type: 9-cylinder air-cooled radial
Bore: 130 mm (5.12 in)
Stroke: 140 mm (5.51 in)
Displacement: 16.72 L (1,020 cu in)
Length: 1,065 mm (41.93 in)
Diameter: 1,184 mm (46.61 in)
Dry weight: 260 kg (573 lb) with ancillaries, without propeller hub
Valvetrain: one inlet and one exhaust valve per cylinder, operated by push-rods via rocker gear. Eight cam push-rod disc drive.
Supercharger: impeller drive ratio 10.7:1
Fuel system: single barrel Stromberg NAR80G carburettor
Ignition system: Scintilla magnetos, automatic advance
Fuel type: petrol, 85 Octane
Oil system: dry sump, with one pressure and one scavenging pump
Cooling system: air-cooled
Reduction gear: direct drive
Power output: rated maintained up to 2,750 m (9,000 ft), at 2,200 rpm 270 kW (360 hp)
Power output: maximum continuous at 2,200 rpm 300 kW (400 hp)
Power output: take-off at 2,020 rpm 330 kW (440 hp)
Compression ratio: 6.4:1
Specific fuel consumption: 255 g/(kW.h) (0.562 lb/(hp.h))
Oil consumption: 8.7 g/(kW.h) (0.23 oz/(hp.h))
Avia Rk.12
As well as producing aircraft and building Hispano-Suiza and Lorraine aero-engines under licence, Avia also designed and built their own radial engines. One of Avia’s own designs, the 1930s Avia Rk.12 was a 7-cylinder supercharged radial engine with a rated output of 150 kW (200 hp), built in Czechoslovakia.
It was a conventional air-cooled radial: nitrided steel barrels with integral fins were screwed into heat treated Y alloy heads. The pistons were also of heat treated Y alloy. The crankcase was cast from aluminium alloy, with some minor parts using magnesium alloy. The single throw two piece crankshaft was linked to the pistons with an I-section Y alloy master rod, with a single piece big end, which carried the other six piston rods.
The Rk.12 was used in the Avia 51.
Specifications:
Type: 7-cylinder air-cooled radial
Bore: 130 mm (5.12 in)
Stroke: 130 mm (5.12 in)
Displacement: 12.08 L (737 cu in)
Length: 1,047.5 mm (41.24 in)
Diameter: 1,110 mm (43.7 in
Dry weight: dry, with ancillaries, without propeller hub 215.5 kg (475 lb)
Valvetrain: one inlet and one exhaust valve per cylinder, operated by push rods via rocker gear. Six cam push rod disc drive.
Supercharger: impeller drive ratio 10.7:1
Fuel system: single barrel Zenith 70P or Stromberg NAR68 carburettor
Ignition system: Scintilla magnetos, automatic advance
Fuel type: petrol, 74 Octane
Oil system: dry sump, with one pressure and one scavenging pump
Cooling system: air-cooled
Reduction gear: direct drive
Power output: rated, maintained to 3,000 m (9,840 ft), at 2,200 rpm: 150 kW (200 hp)
Power output: maximum continuous 195 kW (260 hp)
Power output: take-off 210 kW (280 hp)
Compression ratio: 5.3:1
Fuel consumption: 62 L/hr (13.64 Imp gal/h, 16.4 US gal/h)
Oil consumption: at cruising speed, 2 kg/h (4.4 lbs/h)
Avia B-634

The B 634 represented the ultimate in the aerodynamic development of the basic B 34 single-seat fighter biplane design, and was to be numbered among the cleanest aircraft in its category ever flown. Tested in 1936, the B 634 was powered by an Avia-built HS 12Ycrs engine mounting a 20mm Oerlikon FFS cannon, two 7.7mm Model 30 machine guns being installed in the upper fuselage decking. There was virtually no commonality of components between the B 634 and the B 534.1 from which it was derived. By comparison with the earlier fighter, the upper wing of the B 634 featured increased chord while the lower wing had reduced chord, the wingtips were redesigned, the ailerons were broader, the gap was reduced (increasing the splay of the interplane struts), the stagger was greatly increased, and cut-outs were introduced on the lower wing roots. The curvature of the engine cowling and cockpit sill was refined, cantilever undercarriage legs were adopted and the radiator bath was faired cleanly between the leg roots. Despite a substantial reduction in drag, performance offered an insufficient improvement over that of the B 534 to warrant series production, the disappointing results provided by the B 634 being due primarily to a substantial increase in structural weight.
Two prototypes were built. The second had an enclosed canopy and different undercarriage. Both B-634 were pressed to service in 1938.
B.634
Engine: 1 x 850hp Avia-Hispano Suiza 12Ycrs
Wingspan: 9.40 m / 31 ft 10 in
Length: 8.35 m / 27 ft 5 in
Height: 3.06 m / 10 ft 0 in
Max take-off weight: 2340 kg / 5159 lb
Empty weight: 1710 kg / 3770 lb
Max. speed: 415 km/h / 258 mph
Cruise speed: 362 km/h / 225 mph
Ceiling: 11000 m / 36100 ft
Rate of climb: 960 m/min / 3150 ft/min
Range: 500 km / 311 miles
Armament: 1 x 20mm, 2 x 7.7mm
Crew: 1

Avia B-534

The B.534 featured a fixed undercarriage and biplane wings. Fuselage construction of the Avia B.534 was a mix of fabric-covered steel-structured wing assemblies. Armament was two or four 7.7mm synchronized machine guns and six 44lb bombs. Only some machines of the Nos I-II batches had a cockpit canopy.
The B-534 prototype was flight-tested in August 1933.
The operational flight ceiling was over 30,000 ft.

The Nos I-II batches being built from Feb 1935 were equipped by wooden propellers, the Nos III-IV batches with composite ones.
Two machine guns were typical for the first 100, in the lower wing they were mounted into both sides of the fuselage. The No IV batch cockpit was covered by a canopy and hooded wheels. Aircraft of all the batches were equipped by racks for small splinter bombs.

The 190th production B-534 fighter was the fourth one armed by four machine guns. In addition to two side-fuselage-mounted machine guns, the Bk-534 was armed also by a HS No 402 via propeller-axle shooting canon.

The B-534 turned out from 1936 were of higher empty as well as take-off weight, top speed, service ceiling and climb up to 5 000 m.

Because all three Aeroplane Works within a range of German bombers were, a new plant was built at the village of Kunovice in South Moravia. B-534s were turned out there in 1937.
Avia B.534’s would eventually see combat against the invading German forces, for the conquering German forces against the Soviet Union and ultimately phased out of service after completing several, less note-worthy, roles.
The Czechoslovakian Avia B.534 series of biplane was highly regarded. Such was the performance of the machine that the German Luftwaffe would briefly setup a fighter squadron utilizing captured B.534 aircraft.
A total of 445 were built.
Avia B-534
2nd batch
Engine: Avia HS 12 Ydrs 750 hp
Wingspan: 9.4 m
Length: 8.1 m
Empty weight 1385 kg
Take off weight: 1913 kg
Armament: two machine guns.
Avia B-534
Engine: Avia HS 12 Ycrs
Empty weight: 1631 kg
Loaded weight: 2222 kg
Top speed: 375 kph
Range: 500 km
Rate of climb: 15m/sec
Service ceiling: 9500 m
Avia B.534-IV
Engine: 1 x Hispano-Suiza HS 12Ydrs, 850hp.
Length: 26.90ft (8.2m)
Width: 30.84ft (9.40m)
Height: 10.17ft (3.10m)
Maximum Speed: 245mph (394kmh; 213kts)
Maximum Range: 360miles (580km)
Rate-of-Climb: 2,953ft/min (900m/min)
Service Ceiling: 34,777ft (10,600m)
Armament:
4 x 7.7mm synchronized machine guns
6 x 44lb bombs
Crew: 1
Hardpoints: 6
Empty Weight: 3,219lbs (1,460kg)
Maximum Take-Off Weight: 4,674lbs (2,120kg)


Avia B-234
A 1932 single-piston-engine one-seat biplane fighter (prototype only).
Avia B-158
A 1938 twin-engined medium bomber, prototype only
Avia B-122 / Ba.122 / Bs.122 / B.222 / B.322 / Ba.422

In the spring of 1934 the Czechoslovak Army Command decided that some Czechoslovak Air Force pilots would participate in the international aerobatic competition Coupe Mondial. For this purpose, the Czechoslovakian aircraft manufacturer Avia was given a task to design and construct an aircraft. Designed by František Novotný as a development of the Avia BH-22, the prototype, B.122 Vosa (“Wasp”) was presented after a mere six weeks time, powered by a 260 hp Walter Kastor.
The fuselage had a frame of welded steel tube and linen covered. The wings were all wood, the upper and lower wing span the same. On the lower wings were the ailerons. The wheels were attached to the semi-axes split in the tops of the pyramids, including pneumatic oil shock absorbers.
The first flight was on May 12, 1934, testing was carried out by Captain Novak. The test results were quite satisfactory, although he considered that the area of the vertical stabilizer should be increased. Twelve days later, the second plane was ready.
The Czechoslovak pilots had only a few weeks to learn and master the aircraft as the competition was to be held in July 1934. Luckily, the design was quite successful and the Czechoslovak pilots managed to win the 4th (Novak) and the 8th place (staff-captain Ambrus) in the competition. After that, Novak appeared several times on the new aircraft with demonstration flights in Portugal, Austria, Spain, Romania and Yugoslavia.

Afterwards, the aircraft was modified, based on the pilots’ inputs, and this resulted in the improved version Ba 122. In 1935, the plant produced the first two Avia advanced aircraft modifications Ba-122. It increased the area of the keel and installed a new biplane box. The ailerons were located on the top and on the lower wing connected by rigid rods. The Ba.122 was equipped with a more powerful engine. This version went into production and 35 aircraft were built. The final two B-122 featured a Townend ring but without any advantage they were removed.
At the end of 1935 motor improvments went on in parallel on two fronts. One plane put had a Kastor IIA engine with a new carburettor, and another machine mounted a much more powerful 385 hp Air Rk-17 motor. The Avia engine biplane made its first flight 23 January 1936 and tests were successful. The plant began to build in parallel both variants in small batches. The Ministry of Defense ordered 35 biplanes with the Rk-17 to train fighter pilots. One machine with a Kastor IIA was used the German personal air attaché in Czechoslovakia. It was registered on the Czechoslovak civil register.
At the Olympic Games 1936, held in Berlin, the program included contests and aviators, Czechoslovakia enrered three pilots – Nowak, Ambrus and Wide. They all received brand new Ba-122. One of them was Kastor powered, and the other two – Rk-17. Broad took the second place, Novak – the third, Ambrus – the eighth.
In 1937, Avia powered the Ba-122 with 325 hp Walter Polluk motors. Three of these machines were sent to the International Flying Meeting in Zurich in July/August, along with five aircraft with Rk-17 engines. This allowed two different categories of engines volumes. The individual competition in categories B and C was won by Novak. His colleagues also took third and fourth places. These successes led to export orders from the Soviet Union and Romania. Czech pilots demonstrated three -122s in Moscow on October 15, 1936. The pilots were invited after the Soviet Military Group had paid a visit to the Czechoslovak Republic in summer of the 1936 year. The Soviets ordered fifteen Walter Castor powered A-122 aicraft.
A modification of the Ba-122, the B-222, took to the air 31 September 1937. The Rk-17 engine received an elongated NACA hood, and the wheels in a teardrop-shaped fairing. This machine remained the property of Avia and was intended for demonstration purposes.
In Czechoslovakia, by this time there was a new version of the Bs-122. The Ministry of Defence has ordered 45 of these aircraft for training units, flight schools and, especially, for the Higher School of aerial acrobatics in Prague. Bs-122 feature a rounded keel and cut-outs in the bottom of the fuselage at the wing to improve visibility downwards. Series tests started on 10 October 1936, completed them in July 1937. All the Bs-122 but one were equipped with Kastor PA engines. One of the planes of this order was a B-322 with Rk-17 engine in a Townend ring and with a closed canopy. The first flight of this machine was made Oct. 24, 1937.

For competition in France in 1938, Novak assembled improved B-122, later called the B-422. On it to improve visibility up and down the designer changed the upper wing shape. Two were made, the second an alternate. Both had an Rk-17 engine. The first B-422 went on March 4 and the second on April 7, 1938 to the competition in Saint-Germain. Novak came second.

After his return to Czechoslovakia, Novak organized an aerobatic team of nine airmen for various events. At the Munich crisis, all acrobatic planes went into the Air Force. Earlier, they were considered the property of the Czechoslovak Aeroclub, though they were flying military pilots and service technician aerobatic teams Air Force specialists. During the negotiations in Munich, Czechoslovakia was forced to comply with the Germans. In less than a year, the German army occupied the entire territory of Czechoslovakia. The entire fleet of the Czechoslovak Air Force was captured. What exactly the Germans did with the captured B-122 aircraft is unknown. Among the captured equipment included a total of 76 training and acrobatic aircraft.
Most of the Ba-122 and Bs-122 were sold to allies of Germany. A number of these biplanes got to Romania. In late 1939, the Germans offered to sell Bulgaria former Czechoslovak Army equipment, including aircraft. At the Merseburg airport a commission of Bulgarian pilots and engineers arrived. They selected a large number of aircraft of various types, including 12 Bs-122. Later, apparently made other purchases, since only the Bulgarian Air Force of 27, including one B-322. In Bulgaria, these planes were called ‘Osa’. The largest number of them operated in 1942-43 at a flight school in Lovech, training fighter pilots.
Quite a few aircraft were left in Slovakia, which became an ally of Germany. Slovaks got almost all the equipment of the 3rd Regiment, whose headquarters is located in Bratislava. It is composed of a training squadron, a unit of which were scattered across three different airfields. At the beginning of 1940 were 10 Slovak Air Force Ba-122 and 13 Bs-122. At the end of 1940, the majority of these machines went to a flight school, organized in the town of Trencincal Biskupiec. In August 1943, the school moved to the Three Oak airfield. There, they lived almost to the end of the war. In August 1944, the Slovak army, united with the guerrillas, attacked German garrisons. It began a Slovak National Uprising. Part of the Slovak aviation aircraft flew over the front line and sat on Soviet airfields. Others remained in their native land and began supporting rebels from the air. Among them the aircraft on the Three Oak airport. At that time there were three 122 and one Bs-122. Apparently, the machines were destroyed during German air raids.

After the conclusion of the agreement on mutual assistance between the USSR and Czechoslovakia in 1935 in the Czechoslovak Army, Soviet commanders were trainees, including pilots. In the summer of 1936 Prague was visited by Soviet aviation delegation headed by the Chief (in a modern commander) Red Army Air Force Army Commander 2nd Rank Ya Alksnis. For her, it organized a flypast, and included a demonstration of individual and group aerobatics airplanes of various types.
In response an aviation delegation went to the Soviet Union headed by Lieutenant Colonel Beroun, commander of the 4th Regiment (Czechoslovakia in a small regiments was only five, so Beroun was not the last person in the ranking Air Force). The delegation included the aerobatic team of Novak, Broad, and Hubacheka.
Czechoslovakia and the USSR did not have a common border, so flying through Romania, Iasi through to Odessa, the Soviet border was crossed in the parade – in the middle of the three-engine Fokker, and around four Ba-122. The fourth was considered a replacement. And it was needed. Shortly after reaching Soviet territory Novaks motor failed. He made a forced landing in a field. Next to him landed Vyborny. Nowak and Vyborny were guests of the local collective farm, waiting for a new engine from Prague. The rest of the aircraft continued along the planned route. They passed through Odessa, Vinnitsa, Kiev. On the way to the cities, airfields, military units and flight schools group Novak demonstrated aerobatics. The last presentation was given on October 15 in Moscow, at the Tushino airfield.

Soviet specialists have noted good handling Ba-122. No Soviet aircraft had the necessary qualities. Even the new UT-1 could not be compared for its aerobatic capabilities. The Czechoslovak delegation returned home from Moscow, but the Red Army Air Force ordered 15 Ba-122. Ten of them had to have Kastor engines, while the remaining five Polluks. Avia fulfilled the order at the end of 1936. In the beginning of next year, all had arrived in the Soviet Union. One aircraft in 1937 was used for state tests in the Air Force Research Institute.
One machine with a Kastor engine at TsAGI was studied for the suitability of inverted flight for the Ba-122. He Czechoslovakian biplane could fly upside down for 30 minutes. To this end, it was equipped with a carburetor and fence so gasoline was produced from the center of the tank. The engine had a forced extraction of oil from the top of the crankcase.
Most biplanes apparently went into the flight schools and colleges, training pilots of fighter aircraft. Four Ba-122 (two – with Kastor and two with Polluk engines, on March 15, 1940 were in the Odessa aviation school. In the summer of the same year the school was transferred to Konotop. Another plane in the spring of 40, was with the Air Staff of the Kiev military district. The last thing that became clear is the presence of one in the Moscow Glavsevmorputi squadron. She wore a tail number N-261 on February 10, 1942. This was perhaps the last aircraft of this type in the USSR.
The aircraft was later further developed into the prototype Ba.422.

Total production was approximately 100.
Versions:
B.122
Prototype
Bs.122
Military version of the B.122
Ba.122
Improved version with Avia Rk-17 engine
Ba.222
Prototype
Ba.322
Prototype
Ba.422
Prototype, another prototype was called Ba.422.2
Operators:
Bulgarian Air Force – 12 aircraft taken over from the Czechoslovak Air Force
Czechoslovakian Air Force – 45 Bs.122 and 35 Ba.122 aircraft
Luftwaffe – 12 aircraft taken over from the Czechoslovak Air Force
Royal Romanian Air Force
Slovak Air Force (1939-1945)
Soviet Air Force – 15 Ba.122 aircraft
Specifications:
Ba.122
Engine: 1 × Avia Rk-17, 260 kW (350 hp)
Wingspan: 8.85 m (29 ft 0.5 in)
Wing area: 22.55 m² (242.7 sq ft)
Length: 6.80 m (22 ft 4 in)
Height: 2.84 m (9 ft 4 in)
Empty Weight: 1898 lb / 861 kg
Max weight: 1080 kg (2381 lb)
Maximum speed: 270 km/h (168 mph)
Cruise speed: 230 km/h (143 mph)
Service ceiling: 7,000 m (22,300 ft)
Range: 463 km / 250 NM / 288 mi
Rate of climb: to 3,000 m: 8.33 m/s (1,640 ft/min)
Crew: One
B-122
Engine: Water Kastor II, 260 hp
Wingspan: 8.85 m
Wing area: 22.00 sq.m
Length: 6.80 m
Height: 3.80 m
Empty weight: 760 kg
Normal takeoff weight: 980 kg
Max speed: 240 km / h
Cruising speed: 187 km / h
Practical range: 530 km
Service ceiling: 6000 m
Crew: 2
B-122
Engine : Avia Rk-17 385 hp
Wing span: 8.85 m
Length: 6.80 m
Empty weight: 861 kg
Top speed 270 kph
Rate of climb 4 m/s
Service ceiling: 7000 m
Range: 575 km
Avia Ba-422
Engine: Avia Rk-17, 440 hp
Span: 8.85 m
Length: 6.80 m
Empty weight: 903 kg
Service ceiling: 7000 m
Range: 460 km
