The Fiat G.55 Centauro 
         (centaur) was and all metal low wing monoplane single seat fighter 
         designed by Giuseppe Gabrielli, and represented a great improvement by 
         comparison with the previous Fiat monoplane fighter to go into 
         production, The G.50 Freccia. Great care was taken to blend an 
         aerodynamically advanced airframe with a structure which was robust and 
         would lend itself to mass production. Its configuration included a 
         fully retractable landing gear and a raised cockpit providing an 
         excellent view. Fast and manoeuvrable, the type proved popular with its 
         pilots.  
         
           
         The first of three 
         prototypes was flown on 30 April 1942. The third (MM 493) was the only 
         to carry armament, comprising one engine mounted cannon and four 
         fuselage mounted machine guns. It was evaluated under operational 
         conditions from March 1943, but by then the Italian air ministry had 
         already decided on mass production of the G.55. However, only 16 G.55/0 
         pre-production and 15 G.55/I initial production aircraft had been 
         delivered to the Regia Aeronautica by September 1943, production 
         thereafter being for the Fascist air arm flying alongside the 
         Luftwaffe. Before wartime production ended 274 more were completed and 
         a further 37 were abandoned at an advanced construction stage. 
         
           
         Before the armistice of 
         September 1943, G.55s had participated in the defence of Rome with the 
         353 Squadriglia of the Regia Aeronautica. The post armistice operations 
         were mainly with the Fascist air arm's Squadriglia 'Montefusco' based 
         at Veneria Reale, then with the three Squadriglie which formed the 2nd 
         Gruppo Caccia Terrestre, but losses were heavy, as a result mainly of 
         Allied attacks on the airfields. While the war was still in progress, 
         Fiat flew two prototypes of the G.56, which developed from the G.55 to 
         accept the more powerful Daimler Benz DB 603A engine. Built during the 
         spring of 1944 they incorporated minor structural changes and had the 
         fuselage mounted machine guns deleted. The first prototype survived the 
         war and was used subsequently by Fiat as a testbed. 
         Fiat reinstalled the 
         G.55 assembly line after the war, using wartime manufactured assemblies 
         and components to produce the G.55A single seat fighter/advanced 
         trainer of which the prototype was first flown on 5 September 1946. If 
         differed from the G.55 only in instrumentation and armament. The 
         armament comprised of either two wing mounted plus two fuselage mounted 
         12.7 mm (0.50 in) machine guns, or two 20 mm Hispano-Suiza cannon plus 
         two fuselage mounted 12.7 mm (0.50 in) machine guns. The Italian 
         Aeronautica Militaire procured 19 G.55As and 30 were supplied to 
         Argentina, which returned 17 in 1948 for resale to Egypt, these being 
         armed with four 12.7 mm (0.50 in) Breda-SAFAT machine guns. A two seat 
         advanced trainer variant of the G.55 had been flown in prototype form 
         on 12 February 1946 under the designation G.55B. The Italian 
         Aeronautica Militaire aquired 10 of these, and 15 were sold to 
         Argentina in 1948.  
         specifications (Fiat 
         G.55/I Centauro "Centaur") 
         Type: Single Seat 
         Fighter  
         Design: Ingeniere 
         Giuseppe Gabrielli of Aeronautica D'Italia S.A. (Fiat)  
         Manufacturer: 
         Aeronautica D'Italia S.A. (Fiat) in Turin  
         Powerplant: One 1,475 
         hp (1100 kw) Fiat RA.1050 RC.58 Tifone 12-cylinder inverted Vee engine 
         (license built version of the Daimler Benz DB 605A-1). 
         Performance: Maximum 
         speed 391 mph (630 km/h); climb to 19,685 ft (6000 m) in 7 minutes 12 
         seconds; service ceiling 41,665 ft (12700m). 
         Range: 746 miles (1200 
         km) with internal fuel. 
         Weight: Empty equipped 
         5,798 lbs (2630 kg) with a maximum take-off weight of 8,197 lbs (3718 
         kg). 
         Dimensions: Span 38 ft 
         10 1/2 in (11.850 m); length 30 ft 9 in (9.37 m); height 10 ft 3 1/4 in 
         (3.13 m); wing area 227.23 sq ft (21.11 sqm) 
         Armament: One engine 
         mounted 20 mm Mauser MG 151/20 cannon and two similar wing mounted 
         cannon, and two fuselage mounted 12.7 mm (0.50 in) Breda-SAFAT machine 
         guns plus provision for two 353 lbs (160 kg) bombs on underwing racks. 
         Variants: G.55 
         (prototype), G.55/0 (pre-production), G.55/I (initial production), 
         G.55A (single seat advanced trainer), G.55B (two seat advanced 
         trainer), G.56 (two prototypes with the DB 603A engine). 
         Operators: Italy (Regia 
         Aeronautica, Aeronautica Nazionale Repubblicana), Argentina, Egypt.  |