The Officine 
         Ferroviarie Meridionali, first became involved in the Italian aircraft 
         industry in 1923, beginning manufacturing activities two years later by 
         the licensed construction of Fokker designs. In 1934 Societa Anonima 
         Industrie Aeronautiche Romeo was formed to to takeover the aeronautical 
         activities of the Officine Ferroviarie Meridionali (Aeroplani Romeo). 
         In 1936, the Societa Anonima Industrie Aeronautiche Romeo absorbed all 
         the industrial activities of the Officine Ferroviarie Meridionali and 
         changed its name to Industrie Meccaniche e Aeronautiche Meridionali 
         (IMAM).
         In 1934 the company 
         (then the Societa Anonima Industrie Aeronautiche Romeo) had started 
         design and production of a two-seat fighter/reconnaissance biplane 
         under the designation Romeo Ro.37. This was an unequal-span single-bay 
         biplane of mixed wood and metal construction. Its design included fixed 
         tailwheel landing gear (with all three wheels being provided with speed 
         fairings), a braced tail unit incorporating a variable-incidence 
         tailplane and accommodation for two in tandem enclosed cockpits. Power 
         was provided by a 600 hp (448 kW) Fiat A.30RA Vee 12-cylinder inline 
         engine which was prone to overheating in the hot, dry areas of northern 
         and eastern Africa, of which the aircraft principally operated in.
         An improved Ro.37bis 
         was developed subsequently, and this introduced an optional radial 
         powerplant comprising either the 560 hp (418 kW) Piaggio P.IX RC.40 
         9-cylinder air-cooled supercharged radial engine or a 700 hp (522 kW) 
         Piaggio P.XR 9-cylinder air-cooled supercharged radial engine, both 
         rated for maximum output at a lower altitude than the Fiat A.30RA 
         inline engine on the previous model. Both models proved popular for 
         their day, with production of the Ro.37 and Ro.37bis exceeding 160 and 
         475 respectively, and export orders were received from Afghanistan, 
         Hungary and from countries in Central and South America.
         The Ro.37bis first saw 
         combat in Spain, where it was a favourite of the specialist, Cadena 
         or 'Chain' ground-attack units, especially the Spanish Fascist Grupo 
         4-G-12 and the 120a Squadriglia, XXII Grupo Autonomo "Linci" 
         of the Italian Aviazione Legionaria. Cadena was a tactic that 
         allowed mutual defence against fighter attack and, more importantly, 
         nearly continuous fire against the chosen ground target. The 'chain' 
         was setup so that at least one aircraft was always attacking while the 
         others climbed away or approached in a dive. The tactic kept return 
         fire from the ground to a minimum and let each aircraft cover the tail 
         of the aircraft in front. But it was also very risky, because the 
         aircraft followed a fairly predictable flight path during successive 
         attacks. Some cadena units removed the rear gunners position and 
         operated the aircraft as a single seater, reasoning that the lighter 
         weight would give better performance and maneuverability. The 
         advantages outweighing the loss of a single machine-gun that only gave 
         limited protection.
         Ro.37 and Ro.37bis 
         aircraft were involved in the Spanish Civil War from October 1936 and 
         were used extensively by the Regia Aeronautica during Mussolini's 
         invasion of Abyssinia between October 1935 and May 1936 and during the 
         Italian occupation of that country until 1941. Some 275 Ro.37bis 
         aircraft were in service with the Regia Aeronautica when Italy became 
         involved in World War II, and these saw first-line service in the East 
         and North African campaigns and in the Balkans as the standard 
         reconnaissance aircraft of the Squadriglie da Osservazione Aerea. 
         After withdrawal from first-line service they found a variety of uses, 
         but all had been retired before Italy's armistice with the Allies on 8 
         September 1943.
         Variants
         Meridionali Ro.37 - The 
         initial production type powered by a 600 hp (448 kW) Fiat A.30RA Vee 
         12-cylinder inline engine. This engine proved unreliable in the 
         conditions the aircraft operated in. Originally designed to keep drag 
         to a minimum, the faired propeller spinner gave minimal frontal area, 
         but this was offset by the large cooling radiator. As a fighter, it was 
         obsolete from the start, but did serve fairly well in the close support 
         role.
         Meridionali Ro.37bis - 
         An aerodynamically improved production version incorporating a 560 hp 
         (418 kW) Piaggio P.IX RC.40 9-cylinder air-cooled supercharged radial 
         engine or a 700 hp (522 kW) Piaggio P.XR 9-cylinder air-cooled 
         supercharged radial engine, both giving better low level performance.
         Meridionali Ro.43 - 
         Contemporary with the Ro.37/37bis, the Meridionali Ro.43 was designed 
         and developed as an attractive looking two seat fighter/reconnaissance 
         floatplane for the ship based service. It was an unequal-span 
         single-bay biplane with foldable wings, the upper and lower wing 
         centre-sections being built integrally with the fuselage. Basic 
         structure was of mixed steel-tube and wood, with light alloy and fabric 
         covering, and the landing gear consisted of a large single-step central 
         float of wood, with small stabilising floats mounted beneath each 
         wingtip. Tandem cockpits were provided for the pilot and 
         observer/gunner, and power was provided by a 700 hp (522 kW) Piaggio 
         P.XR 9-cylinder air-cooled supercharged radial engine. A single forward 
         firing 7.7 mm (0.303 in) Breda-SAFAT machine-gun and another 7.7 mm 
         (0.303 in) Breda-SAFAT or Lewis machine-gun on a trainable mount in the 
         rear cockpit made up its armament. Weight empty 3,924 lbs (1780 kg) 
         with a maximum take-off weight of 5,291 lbs (2400). Maximum speed 186 
         mph (300 km/h) at 8,200 ft (2500 m); service ceiling was 21,665 ft 
         (6600 m); flight endurance 8.5 hours; range 932 miles (1500 km); Span 
         38 0 3/4 in (11.60 m); length 31 ft 9 3/4 in (9.70 m); height 11 ft 5 
         3/4 in (3.50 m); wing area 359.10 sq ft (33.36 sq m). 
         When Italy entered the 
         war in June 1940, the Ro.43 was the Italian navy's standard ship-based 
         catapult-launched floatplane with approximately 105 still being in 
         service out of the 125 aircraft built. About 48 of these were still on 
         strength at the time of the armistice on 8 September 1943. A small 
         number of Ro.43s supplied to neutral Spain were used for air/sea rescue 
         operations throughout World War II.
         Meridionali Ro.44 - 
         Some 40 generally similar aircraft were built as Ro.44 single-seat 
         fighter floatplanes, these having the observer's position faired over 
         and his armament and equipment removed, while two forward-firing 7.7 mm 
         (0.303 in) Breda-SAFAT machine-guns replaced the standard single gun of 
         the Ro.43. A number of Ro.43s and Ro.44s were used for shore-based 
         defence of the Aegean islands serving with with 161a Squadriglia 
         Caccia Marina dell-Egeo.   
         (Meridionali Ro.37bis)
         Type: Two Seat 
         Fighter, Ground Attack, Observation, Liaison & Ambulance 
         Accommodation/Crew:
         Pilot & Observer/Gunner 
         Design: Societa 
         Anonima Industrie Aeronautiche Romeo Design Team 
         Manufacturer: 
         Societa Anonima Industrie Aeronautiche Romeo. In 1936 the Societa 
         Anonima Industrie Aeronautiche Romeo absorbed the all industrial 
         activities of the Officine Ferroviarie Meridionali and changed its name 
         to Industrie Meccaniche e Aeronautiche Meridionali (IMAM). 
         Powerplant: One 
         560 hp (418 kW) Piaggio P.IX RC.40 9-cylinder air-cooled supercharged 
         radial engine. An alternative 700 hp (522 kW) Piaggio P.XR 9-cylinder 
         air-cooled supercharged radial engine was also used.
         Performance: 
         (Ro.37) Maximum speed 199 mph (332 km/h) at 13,120 ft (4037 m), landing 
         speed 67 mph (112 km/h), service ceiling of 21,976 ft (6762 m). (Ro.37 
         bis Piaggio P.IX) Maximum speed 205 mph (330 km/h) at 16,405 ft (5000 
         m); cruising speed 155 mph (250 km/h); service ceiling 23,620 ft (7200 
         m).
         Range: (Ro.37) 
         726 miles (1212 km) on internal fuel. (Ro.37bis) 696 miles (1120 km) on 
         internal fuel.
         Weight: Empty 
         3,494 lbs (1585 kg) with a maximum take-off weight of 5,335 lbs (2420 
         kg).
         Dimensions: Span 
         36 ft 4 1/4 in (11.08 m); length 28 ft 1 in (8.56 m); height 10 ft 4 in 
         (3.15 m); wing area 337.46 sq ft (31.35 sq m).
         Armament: Two 
         fixed forward firing 7.7 mm (0.303 in) Breda-SAFAT machine-guns and 
         another 7.7 mm (0.303 in) Breda-SAFAT or Lewis machine-gun on a 
         trainable mount in the rear cockpit plus up to 397 lbs (180 kg) of 
         bombs on underwing racks. Loudout normally consisted of twelve 33 lbs 
         (15 kg) light bombs. On a small number of aircraft two 12.7 mm (0.50 
         in) Breda-SAFAT heavy machine-guns were used instead of the smaller 
         calibre guns.
         Variants: Ro.37, 
         Ro.37bis, Ro.43 (two seat naval floatplane), Ro.44 (single seat naval 
         floatplane).
         Equipment/Avionics: 
         None.
         History: First 
         flight (Ro.37) 6 November 1934.
         Operators: Italy 
         (Regia Aeronautica), Afghanistan, Ecuador, Hungary, Uruguay, Spain 
         (Ro.43).