Entirely developed and 
         produced by the Swedish aeronautical industry, the J.22 fighter was the 
         result of an emergency program launched in order to overcome the 
         embargo placed on the export of aeronautical products by the United 
         States in October 1940. At the time, Sweden had ordered a total of 292 
         combat planes (consisting of fighters and fighter-bombers) from the 
         North American aeronautical industry. The fact that these were not 
         delivered literally caused a crisis in the country's air force (Svenska 
         Flygvapnet), which was urgently in need of reinforcements. Founded in 
         1926, the aircraft which it had in service were mainly British and 
         Italian in origin. 
         
           
         An emergency programme 
         was established to design and build a single-seat fighter relying upon 
         domestic industry and talent. The project (designation P.22) for the 
         J.22 was entrusted to a group of technicians led by Bo Lundberg and a 
         special centre, the FFVS (Flygförvaltningens Verkstad, or Aeronautical 
         Studies Workshop), was created to supervise and run the industrial 
         program. The production programme involved over 500 sub-contractors, 
         hardly any with experience of aircraft construction. Lundberg had as a 
         primary objective simplicity of manufacture and in this he succeeded. 
         Studies for the new aircraft began on 1 January 1941, and the first of 
         two J22 prototypes, built by Flygtekniska Försöksanstalten (FFA) near 
         Bromma, flew for the first time on 21 September 1942, from Bromma 
         airport, where the final assembly plant had been set up in a hanger. 
         Both prototypes crashed, one probably due to oxygen starvation of the 
         pilot, the other due to engine failure during landing.  
         The J.22 was a slender 
         single-seater monoplane, whose lines recalled those of the German 
         Focke-Wulf Fw 190, built following the simplest construction techniques 
         possible. In fact, its airframe was a mixture of wood and metal, while 
         the fuselage consisted of steel tubes covered in plywood. The forward 
         landing gear receded into the fuselage, and the tail wheel was also 
         retractable. It was powered by an SFA STWC3-G radial engine, which was 
         simply a 1,065 hp (794 kW) Pratt & Whitney SC3-G Twin Wasp produced on 
         license by the Swedish aeronautical industry. 
         The cycle of tests and 
         evaluations did not bring to light any serious faults, and the program 
         went ahead on the basis of an initial order for 60 production series 
         aircraft issued prior to the prototype's maiden flight. The first 
         production series aircraft was tested in September 1943, and the units 
         began to receive the new fighter in October. Deliveries went ahead 
         gradually and the J.22 could be considered fully operative in 1944. By 
         the end of the year, 75 had been built and they gradually replaced the 
         various Fiat CR.42s, Reggiane Re. 2000s, and Gloster Gladiators still 
         in service. In all, up till April 1946, 198 J.22s were completed in two 
         versions. These differed from each other solely in their armament. The 
         J.22A was provided with two 7.9 mm (0.31 in) and two 13.2 mm (0.52 in) 
         machine guns, while the J.22B had four 13.2 mm (0.52 in) weapons. 
         This fighter, which 
         remained in service until the 1950s, was used mainly by the units of 
         the Swedish air force based (F3 and F9 wings of the Swedish air arm), 
         based at Malmslätt and Gotenburg. In service, the J.22 proved to have a 
         good overall performance and, above all, to be extremely manoeuvrable. 
         Its only weak point was its lack of visibility while taxiing on the 
         ground. Experience gained in building the J.22 proved invaluable in 
         establishing Sweden's postwar aviation industry. 
         Specifications (FFVS 
         J.22B) 
         Type: Single 
         Seat Fighter  
         Design: FFVS 
         Design Team led by Bo Lundberg  
         Manufacturer: 
         Flygförvaltningens Verkstad (Aeronautical Studies Workshop) in 
         Stockholm  
         Powerplant: One 
         1,065 hp (794 kW) SFA STWC3-G 14-cylinder radial engine. 
         Performance: 
         Maximum speed 357 mph (575 km/h) at 11,485 ft (3500 m); service ceiling 
         30,510 ft (9300 m). 
         Range: 789 miles 
         (1270 km) on internal fuel. 
         Weight: Empty 
         equipped 4,453 lbs (2020 kg) with a maximum take-off weight of 6,250 
         lbs (2835 kg). 
         Dimensions: Span 
         32 ft 9 3/4 in (10.00 m); length 25 ft 7 in (7.80 m); height 8 ft 6 1/4 
         in (2.60 m); wing area 172.23 sq ft (16.00 sq m). 
         Armament: 
         (J.22A) Two 7.9 mm (0.31 in) machine guns and two 13.2 mm (0.52 in) 
         machine guns. (J.22B) Four 13.2 mm (0.52 in) machine guns. 
         Variants: J.22A, 
         J.22B (See Armament), S.22 (nine J.22A aircraft converted to 
         reconnaissance). In 1945 J.22A was redesignated J.22-1, J.22B into 
         J.22-2 and S.22 became S.22-3. In 1947 the nine S.22-3 aircraft were 
         converted back into fighters. 
         Avionics: None. 
         History: First 
         flight (prototype) 21 September 1942; first deliveries October 1943; 
         last delivery April 1946; retired from service 1952. 
         Operators: 
         Sweden (Flygvapnet).  |