Tag Archives: Fascist Italy

Stipa-Caproni

italian flag Italy (1932)
Experimental Aircraft – One Prototype Built

In the history of aviation, there have been many projects that on paper promised outstanding flight capabilities, or offered other technical advantages. The time before the Second World War saw aviation advance at a breakneck pace, and is well known for such experiments. The so-called Stipa-Caproni was one such project, being an intriguing, and somewhat bizarre, experimental aircraft designed by Italian aeronautical engineer Luigi Stipa, and built by Caproni during the interwar period. It was characterized by its tubular fuselage, hence earning it the nickname Flying Barrel.

The unique design Stripa-Caproni experimental aircraft. Source: Wiki

History

In 1927 a young Italian aircraft engineer Luigi Stipa began working on an unusual tube-shaped aircraft. Like many other aviation enthusiasts, Stipa was very interested in how aircraft could achieve better performance through exploring unorthodox construction methods. Thanks to his studies in thermodynamics, he was aware of the so-called Venturi effect, named after Italian physicist Giovanni Battista Venturi. In essence, this effect describes the reduction of fluid pressure and increasing velocity when it’s moving through a cylinder of decreased diameter. In theory, using this principle, a special type of aircraft could be created that could achieve significantly higher speeds than the conventional models of the time. Stipa theorized that for this purpose, such an aircraft would have to have a tube-shaped fuselage with the engine being positioned near the front. After finding it theoretically possible, he moved forward to test if the Venturi effect could be implemented in his airplane concept. For this purpose, he began a series of different tests inside a wing tunnel, carried out at the Aerodynamic Laboratory in Rome, from 1928 to 1931. The main focus of this testing period was to find the adequate shape, and leading edges, of the tube-shaped fuselage. This also included finding the right position of the engine, its position inside that tube, and the ideal propeller rotation speed. Following a series of wind tunnel tests, Stipa concluded that it was possible to build a full-scale prototype by using a single tube-shaped fuselage.

Luigi Stipa in his younger years. Source: Wiki

At the end of his research, he concluded that such a project was viable and set the task of building a working prototype. To gain interest in his project, he wrote about his work in the Rivista Aeronautica journal in 1931, and even built a small working replica. The next logical step was to write to the Italian Minister of Aviation, in the hope of getting approval for the realization of his project. Luckily for Stipa, his work came to the attention of General Luigi Crocco, the Air Ministry’s director. Stipa’s work was well received and the project received a green light. To test the concept, a working prototype had to be constructed.  It is important to note, that both Stipa and the Italian Air Ministry were aware that this project was merely to test his theories, and would not entail any further development of the prototype. In addition, both were aware that Stipa’s proposed principle was only practical on larger aircraft types.

For this purpose, the prototype was to be powered by a small 120-hp engine. The reason behind this decision lay in the fact that this aircraft was primarily built for evaluation and academic purposes. The Italian Air Ministry was not quite willing to invest huge monetary resources in it, beyond those necessary for the construction of the working prototype.

To help build the test aircraft, the Caproni aircraft manufacturer from Milan Taliedo was chosen. It was designated as Stipa-Caproni (sometimes referred to as Caproni-Stipa) referring to its designer and constructor. The prototype was built quickly and was ready for testing in October 1932.

It is perhaps a little surprising that such an unusual design would receive the necessary support for its realization. However, the exploration of new and unorthodox ideas in aviation was very popular in pre-war Europe. During the 1930s, Italy led the way in this aspect, perhaps even more than other countries, testing many unorthodox designs. What’s more, the Italian Fascist regime even encouraged different and unusual projects like this one, although many of them did not produce any meaningful results.

The Stipa-Caproni prototype was used for testing during 1932 and 1933. Source: en.topwar.ru

Technical specification

The Stipa-Caproni was a two-seater, mixed-construction aircraft, designed to have the simplest and thus cheapest fuselage. Its fuselage consisted of a tube which internally consisted of two large wooden round-shaped rings at the nose, followed by a series of similar but smaller rings. All of them were then connected with horizontal ribs which in turn were covered in fabric. The outer wooden rings served as the foundation, on which the wing and the cockpit would be connected. The fuselage design was, in effect, a large tube shaped airfoil.

A close-up view of the Stipa-Caproni internal fuselage construction. The two larger wooden rings serve as a base to which wings and the cockpit would be attached. Source: www.thevintagenews.com

The wings were mounted centrally on each side of the fuselage. These had a simple wooden construction, and were covered in fabric. They were also connected to the fuselage through metal bracing wires, which as a consequence increased the aircraft’s drag.

To the rear, a fairly large tail assembly was placed. During the design work of this aircraft, Stipa intentionally placed the rear control surfaces as close to the slipstream as possible. He hoped that this arrangement would greatly improve the aircraft’s handling and maneuverability.

On top of the fuselage, an elevated two-seat cockpit was placed. These were top-open with a small windshield placed in front of each position. There were also a pair of small doors that opened on the left side to give access to the seats.

The 120-hp de Havilland Gypsy III engine was placed inside this fuselage. It was centrally positioned and suspended using several steel bars that held it strongly in place. This was necessary to do so, as a weaker mounting could potentially endanger the aircraft during flight. The engine propeller was the almost the same diameter as the tube-shaped fuselage.

Given its overall design, and the position of the propellers inside the fuselage, the landing wheels were small and quite close to the ground. It consisted of three fixed road wheels. Two larger on the front and one smaller on the rear. Initially, wheel fairings were used but at some point, and for unclear reasons, these were removed.

A front view of the unusual engine installation. The engine itself was held in place by several metal bars. Source: Wiki
It was provided with a small and fixed three-wheel landing gear. Source: en.topwar.ru

Testing and Final Fate

With this project approved, a prototype was constructed and air tested in October 1932 at the experimental field at Monte Celio near Rome. Despite its odd design, the prototype was able to take to the sky without any major problems. Furthermore, it made several successful flights around Taliedo and Guidnia. It was even presented to the Italian Air Force for future test flights. During this period the aircraft was jokingly nicknamed Flying Barrel or Aereo Botte (Eng. Wooden wine barrel aircraft) or Aereo Barile (Eng. Fuel-Barrel aircraft).

The weight of the aircraft during these flights was 800 kg (1,874 lb), while the calculated wing loading was 44,73 kg/m² (9,16 lb sq.ft.). The maximum speed achieved was 133 km/h (83 mph), and it needed 40 minutes to climb at a height of 3, 000 m. It needed an 800 m long airfield to be able to take to the sky.

The Stipa-Caproni during one of many test flights. Source: www.historynet.com

Despite Stipa’s hopes that the position and shape of the tail control surfaces would improve its mobility, several problems were noted by the test pilots. Firstly the elevator worked very well, which ironically proved to be a major problem. Even with a slight movement of the command control stick by the pilots, the aircraft could prove very sensitive to elevator inputs. On the other hand, the rudder controls were quite stiff,  as a consequence the pilot had to use considerable force in order to use it effectively.  Analyzing this problem showed that the rudder’s large surface area was to blame for its stiff control. But besides the two problems, the aircraft was reported to be easy to fly when being used in a gliding flight. These defects  were of a more or less technical nature, which were not necessarily irremediable through further development of the overall design.

The design of the rear tail assembly proved somewhat problematic. Specifically, the elevator control was overly sensitive while the rudder was quite the opposite. Source: en.topwar.ru

The final results of evaluation flights showed that the Stipa-Caproni does not have any particularly great advantages compared to other more standard aircraft designs.  In addition, Stipa-Caproni’s overall aircraft shape offered limited space within the fuselage for passengers or payload.

As Stipa predicted from the start, his principles would not offer any major advantage over a standard smaller-dimension aircraft. The real application of the Stipa-Caproni design was only feasible on larger aircraft. Stipa hoped that his further research would enable him to construct large aircraft powered by two to three tube-shaped engine mounts. Unfortunately for him, after a series of test flights during 1932 and 1933 the interest in his work died out. It was briefly used in various Italian aviation propaganda publications before being scrapped in 1939.

Despite being in general an unimpressive design, the French showed interest in it. Particularly the company ANF Lex Maureaux, which went so far as to acquire a license for the design in 1935. According to initial plans, a two-engine variant was to be built for testing and evaluation. The project did not go beyond basic work was later canceled.

Lastly, an interesting fact is that many people considered Stipa-Caproni to design some sort of proto-jet engine. Whether this was the case or not, Stipa felt his work was overlooked, and according to some sources, he remained bitter throughout his life until he died in the early 1990s.

Stipa hoped that with more resources he would be able to test his principle on a much larger scale, but ultimately nothing came of it. Source: L. Stipa, Stipa Monoplane with Venturi Fuselage

Replica

In 1996, aviation enthusiast Guido Zuccoli began working on a smaller replica of this aircraft.  However, the death of Zuccoli in a landing accident caused a delay in the replica’s final delivery. It was finally completed in 2001 when numerous small flights were achieved. The aircraft, powered by a 72 hp Simonini racing engine, managed to achieve a flight distance of 600 m (1,968 ft). After that, the aircraft replica was stored as an exhibit at the Zuccoli Collection at Toowoomba, in Australia.

A smaller-scale replica was built and flight-tested in 2001. Source: www.uasvison.com

Conclusion

The Stipa-Caproni represented an intended for the purpose of testing his new concepts in practice. While surely an interesting and unusual concept, Stipa-Caproni’s overall design was not that practical in reality, offering little improvement over a standard aircraft design of similar dimensions.

 

Stipa-Caproni  Specifications

Wingspans 14.3 m / 46 ft 10 in
Length 6.04 m / 19 ft 10  in
Height 3.2 m / 10  ft 7  in
Wing Area 19 m² / 204 ft²
Engine One 120 hp (89.5 kW) De Havilland Gipsy III
Empty Weight 595  kg / lbs
Maximum Take-off Weight 850 kg / 1,874 lbs
Maximum Speed 133 km/h / 83 mph
Landing Speed 68 km/h / 42 mph
Climbing speed to 3,000 m 40 min
Maximum Service Ceiling 3,700 m / ft
Crew 1 to 2 pilots
Armament
  • None

Illustration

 

Credits

  • Written by Marko P.
  • Edited by Henry H. & Ed J.
  • Illustration by Godzilla

Source:

 

 

 

Savoia-Marchetti S.M. 79C/T

italian flag Italy (1936-1943)
Racing Aircraft – 6 Built

The line-up of the Savoia Marchetti S.79C and the Fiat Br.20A (last two) in Istres before the start of the race on 20 August 1937. [modellismoitalia.altervista.org]
The Savoia-Marchetti S.M. 79 was a three-engine medium aircraft developed by Savoia-Marchetti, also known as the Società Idrovolanti Alta Italia (SIAI) later SIAI-Savoia. Initially developed as a fast passenger transport aircraft, it was later adapted for use as a racing aircraft, and later as a medium bomber. From 1936 until 1939 it broke several records, both in the civil and military spheres with the Regia Aeronautica (Italian Royal Air Force), also becoming the fastest medium bomber in the world at the time. It was one of the most produced aircraft by Italy during the Fascist dictatorship and was used by 12 different air forces, both civil and military and remained in service until 1951 as a bomber for the Aeronautica Militare (Italian Air Force), and until 1959 as a bomber for the Lebanese Air Force.

History of the Project

During the 1930s, the Italian Air Force was among the world’s leading air forces, with cutting-edge manufacturing and designers.

Italo Balbo, a fervent fascist and Air Marshal, managed to break several records aboard several seaplanes of the Società Idrovolanti Alta Italia (Northern Italy Seaplane Company). In 1928 he made a bold request for the time, asking SIAI for an aircraft capable of taking off from Italy and reaching any location in Libya carrying 8 to 10 passengers. All in the shortest possible time.

It must be emphasized that the Italian fascist regime tended to support domestic efforts in any field or industry in order to bolster publicity and popular support, which is why Italo Balbo required a fast plane, to be able to outcompete French and British air transports on Africa-bound routes to Libya, Somalia, and Eritrea.

In early 1933, Australian nobleman Sir Mac Pherson Robinson created a challenge to reach Melbourne from London in a single intercontinental flight. In 1933 the SIAI decided to compete for the Mac Robinson Cup, and at the same time to satisfy Balbo. Seasoned engineer Alessandro Marchetti (1884-1966) was put at the helm of the project.SIAI put so much emphasis on the project, that Marchetti’s initial blueprints for the new S.79 were dated February 21, 1933.This cutting-edge project featured low wings, retractable landing gear, Handley Page flaps and three Isotta Fraschini Asso 750 engines of 900 hp each.

Subsequently Marchetti was forced to modify the blueprints, first with three FIAT A. 59 RC engines developed by the American Pratt & Whitney R-1690, finally ending up on Piaggio P. IX R.C. 40 engines of 610 hp developed from the French Gnome-Rhône 9K ‘Mistral’.

History of the Civilian Prototype

In May 1934, the last modifications to the project, and design of the first prototype were completed. The new plane was identified as S.79P or Passeggeri ( Passenger). It received the serial number 19001 and codename I-MAGO.

Through August and September of 1934, various parts of the aircraft were produced in SIAI factories in Sesto Calende in Lombardy, and were sent to the Novara Air Base in Piedmont . After being reassembled on October 8, 1934, and with SIAI test pilot Adriano Bacula and engineer Merizzi at the controls, the 19001 prototype made its first test flight.

The first Savoia-Marchetti S. 79 prototype, the I-MAGO with Piaggio engines at Cameri in the winter of 1934. [stormomagazine.com]
The aircraft proved promising during the tests. There were excellent results as the aircraft had excellent handling, was easy to fly, and had a comfortable passenger cabin. On the other hand the engines, with only 610 hp at maximum power was not enough for SIAI and Alessandro Marchetti.

Piaggio sent one of its technicians during flight tests, engineer Risaliti, to try to increase the power of the engines, but he failed, managing to bring the aircraft to only 360 km/h at an altitude of 100 meters, and 390 km/h at 3,000 meters, while carrying 3 tons of ballast.

These results were impressive for the time, the Junkers Ju 52 for example had a top speed of 290 km/h, but not enough for a modern plane like the S. 79.

These problems forced the Italian technicians to change the engines with more powerful and reliable ones.

This decision was taken also because the Piaggio P. IX R.C. 40 engines led to two different incidents. The first occurred on 28 October when they attempted a record Novara-Rome route which had to be canceled due to engine failures and the plane returned to Novara.The second accident led to the fire of the engines which fortunately was shut down before the prototype was destroyed.

SIAI therefore decided to remove the Piaggio engines in February 1935, and replaced them with the 650 hp Alfa Romeo 125 RC.35, developed from the British Bristol Pegasus.

Due to the larger diameter, the engines received a new cowling, and finally, on April 5, 1935 Bacula and Merizzi took the re-engineered prototype into the air again.

The new tests yielded very favorable results and the plane claimed several records, the first was to be the first three-engine civil transport to break 400 km/h, and the second to travel from Novara to Rome (500 km) in just 70 minutes, which they accomplished on May 10, 1935.

In Rome, Adriano Bacula had the opportunity to familiarize some Italian pilots on the S. 79. Interestingly a delegation of French aviators led by Minister of the Air Denain with the aces Mermoz and Rossi was in the Italian capital. The French pilots admired the new three-engine plane for its modern design and maximum velocity.

Among the Italian aviators who tested the aircraft there were Maggior Biseo and his colleagues, elites of the 1st Experimental Center who expressed much praise for the Chief of Staff of the Regia Aeronautica, General Valle, on the new vehicle.

Returning to Novara to receive some modifications, such as increased range, on May 26, 1935 the S. 79 was back in Rome with all the required changes including 2 new tanks in the wings for a total of 820 liters of fuel.

The aircraft was registered by the Royal Air Force MM. 260 (Matricola Militare /Military Serial Number) and assigned on June 14 to the 1st Experimental Center.

On August 1, 1936 General Valle flew from Rome to Massawa, Eritrea in just 12 hours of actual flight with a stopover in Cairo for refueling, and returned to Italy 4 days later.

On October 3, 1935 the Kingdom of Italy start the invasion of the neutral Ethiopian Empire to colonize it. The Savoia-Marchetti S. 79 prototype was deployed as liaison plane by General Valle.

The second flight was made on January 6, 1936 when the plane carried General Valle, Biseo, Tondi as well as technicians and specialists Gadda, Ghidelli and Bernazzani.

During the representative trip to Ethiopia which ended on January 18 in Grottaglie, Puglia, the plane traveled 15,000 km proving to be very fast and efficient.

The prototype, MM. 260, was assigned to the Experimental Center but was employed by the 12° Stormo Bombardamento Terrestre (12th Ground Bombing Wing), and was modified to carry 6 100 kg bombs. It was tested on 20 May 1936 by Lieutenant Colonel Biseo and Captain Lippi on the Furbara shooting range.

The tests were repeated with captains Paradisi and Moscatelli of the 12° Stormo who demonstrated that the aircraft was an excellent platform for bombing.

Bomber Variant

A pair of Savoia-Marchetti S.M. 79M flying in formation over Sicily during the Second World War. [Wiki]
In December 1935, SIAI-Savoia proposed a military version of the S. 79 powered by the powerful Gnome-Rhône 14K Mistral Major 14 cylinders with a output of 725 hp at 2,000 rpm, hence the name of the prototype S. 79K. However, the General Staff of the Regia Aeronautica rejected the idea of powering their bombers with foreign engines, and ordered 24 S. 79Ms (M for Militare / Military) to be equipped with Italian-made engines.

Schematic showing the differences between the Savoia-Marchetti S.M. 79C and the Savoia-Marchetti S.M. 79M. [Facebook]

S.M. 79 Racing Aircraft or Medium Bomber?

From the first batch of the S.M. 79M, 5 aircraft were modified during production to be used in the civil field, and initially renamed Savoia-Marchetti S.M. 83C, and then returned to the designation Savoia-Marchetti S.M. 79C for Corsa (Racing).

The Savoia-Marchetti flown by pilots Tondi and Moscatelli

This variant flew without armament, the observer gondola and bomb bay also lost its characteristic hump to increase the aerodynamics of the fuselage.

The autopilot system was then enhanced, the on-board instrumentation adjusted, the door on the left side replaced by a smaller hatch above the wing, and its range was increased by adding tanks instead of the bomb bay for a total of 7,000 liters of fuel.

Other improvements concerned the compressors which, when upgraded, allowed the use of 100 octane petrol Also the transceiver system was replaced with a Telefunken model of greater power and reliability. The propellers were substituted with new variable pitch propellers produced by the French Ratier. New larger radiators were added to better cool the engines and finally, the landing gear was fitted with tires capable of withstanding the maximum weight of the plane fully loaded.

This version was created to participate in the tender organized by the French Aero Club for August 1937 which was to fly to the Istres (Southern France) – Damascus – Le Bourget (near Paris) route for a total of 2,900 km.

For the race it was planned to involve a Caproni Ca. 405 ‘Procellaria’ and two FIAT B.R. 20 but due to delays the Ca. 405 could not participate and the SIAI-Savoia produced a sixth S.M. 79C.

Flying the six aircraft were all pilots of the 205ª Squadriglia da bombardamento “Sorci Verdi” of the 12° Stormo Bombardamento Terrestre, the only Italian pilots who had received a pilot’s license for this aircraft.

Apart from the eight Italian aircraft, there were four French aircraft, a Bloch M.B.160, a Farman F.223, a Caudron C-640 and a Breguet 470 Fulgur, the only English one, the De Havilland D.H.88 Comet.

All took off from 1725 hrs on 20 August 1937, the first plane to land in Damascus was the I-FILU after 6 hours and 51 minutes at an incredible speed of 426.42 km/h.

Partial ranking in Damascus
Pilots Aircraft Name Racing Number Qualified Average Speed
Biseo and Mussolini I-BIMU I-5 Terzo
Cupini and Paradisi I-CUPA I-11 Secondo 415 km/h
Fiori and Lucchini I-FILU I-13 Primo 426.42 km/h
Lippi and Castellani I-LICA I-7 Ottavo 352 km/h
Rovis and Trimboli I-ROTR I-12 Quinto
Tondi and Moscatelli I-TOMO I-6 Quarto

The partial ranking podium was all Italian, in fact in Damascus five to six of the S. 79Cs arrived before the other aircrafts, the sixth and seventh were the FIAT B.R. 20s with an average speed of 299 km/h and 382 km/h.

I-LICA had problems with the constant pitch of the right propeller forcing the drivers Lippi and Castellani to travel the Istres-Damascus route for another six hours with only two engines.

The ninth plane to arrive in Damascus was the De Havilland D.H.88 Comet with an average of 356 km/h while the first French plane landed with an average speed of 305 km/h.

During the stop, the planes refueled and fixed the propeller. Due to bad weather it was decided to change course for the return and to fly in formation, thus loading an additional 500 liters of fuel.

One of the six S. 79Cs refueled at Damascus, though unfortunately it’s impossible to determine which one it is. In the background the French four-engined Bloch M.B.160 is visible. [modellismoitalia.altervista.org]
During take-off, one of the two FIAT B.R. 20 experienced rudder damage while the unfortunate I-LICA ended up hitting a pothole on the runway with the left wheel, breaking the landing gear and yawing violently to the left and making take-off impossible.

One hour after departure, the I-TOMO reported that it had a deficiency of 2,000 liters of fuel, while I-ROTR reported that it had to land in Ronchi due to excessive fuel consumption.

It was therefore decided to have the three remaining SM-79s arrive in Paris in formation. The plan was about to succeed, in fact I-BIMU sighted I-FILU and the I-CUPI but due to the lightning storms masking the transmissions, they could not make radio contact.

Biseo and Bruno Mussolini then decided to overtake the other two S.M. 79 to be recognized and make the formation, but when they reached the Alps they had to climb to 6,500 meters. However in doing so, they were forced to reduce the pitch of the propeller, and during the movement the central propeller went to the minimum pitch and jammed.

The two pilots then decided to land in Cameri where there were technicians who could repair their Ratier propellers. However, after a careful examination, during which the plane was refueled, the two pilots were informed that the propeller problem could not be repaired quickly. It was therefore decided to bring the central propeller to maximum pitch and the plane that had stopped for about 30 minutes took off again towards Paris.

The I-ROTR was unable to reach Ronchi due to lack of fuel and had to land in Pula where, after refueling, it was unable to restart because the electrical circuit of the starter magnet of the central engine had been damaged by hail.

Having repaired the fault, the plane continued the next morning to Bourget and was classified in 8th and last place.

The I-TOMO was unable to reach Ronchi and, again due to bad weather, had to land at the Lido of Venice where it ran aground, as the field was reduced to a quagmire by torrential rain, but thanks to the joint efforts of the airport staff and crew, the aircraft was able to leave after refueling.

The two FIATs also had to land due to problems.

Despite the bad weather and the unsatisfactory reliability of the propellers, at Le Bourget there were three S.M. 79s in the first three positions. The I-CUPI arrived at 1547 hrs on the 21st and circled up to 1602 hrs before running out of fuel, waiting in flight for the I-BUMU as the victory of Benito Mussolini’s son would have been a great benefit for the fascist propaganda. Then it was the turn of the I-FILU which landed at 1617 hrs, and finally at 1637 hrs Biseo and Mussolini arrived who, despite the stop, took a significant third place.

Four ground crew members ran to the I-11 S. 79C piloted by Cupini and Paradisi. [modellismoitalia.altervista.org]
Fourth was the De Havilland D.H.88 Comet which landed at 1701 hrs; fifth the Fulgur Breguet at 1737 hrs; then came the Bloch 160, but having started much earlier than the I-TOMO which arrived at 2002 hrs it was ranked seventh, while the I-TOMO was sixth. The others were all withdrawn or unclassified.

Final ranking in Paris
Pilots Aircraft Name Racing Number Qualified Average Speed
Biseo and Mussolini I-BIMU I-5 Third
Cupini and Paradisi I-CUPA I-11 First 350 km/h
Fiori and Lucchini I-FILU I-13 Second
Lippi and Castellani I-LICA I-7 Unqualified
Rovis and Trimboli I-ROTR I-12 Eighth
tondi and Moscatelli I-TOMO I-6 Sixth

On 29 August from 1500 hrs to 1530 hrs all the Corsa type planes and the I-MAGO, which had been brought to Paris to witness the triumph of the other S.M. 79 returned to Italy at the Littorio Airport.

From Damascus, however, on 22 August, the organization of the return of the I-LICA to Italy began. The plane was disassembled and the fuselage, engines, tailings and systems were recovered and sent to Beirut, Lebanon and embarked on a merchant ship bound for Italy. The wing, not transportable by road, and other material, was sold in Damascus.

The victory was celebrated in Italy as overwhelming as both the Savoia-Marchetti S.M. 79C and FIAT B.R. 20A were bomber aircraft adapted to racing aircraft while British and French aircraft were specially developed aircraft for air racing.

Italian pilots and ground crew members that participated in the race near the I-ROTR plane. Source: [modellismoitalia.altervista.org]
Despite the victory there were, especially abroad, those who criticized the planes, claiming that the Savoia-Marchetti S.M. 79C would not have been able to participate in the New York – Paris (race which was canceled in favor of Istres – Damascus – Paris).

The front page of the French newspaper Paris-Soir with the news of the Italian victory [modellismoitalia.altervista.org]
SIAI brochure celebrating the victory of the Istres – Damascus – Le Bourget race [modellismoitalia.altervista.org]

The Decisive Test: Rome – Dakar – Rio

It was decided for various reasons to make a second record setting flight with the Savoia-Marchetti S.M. 79C. This was mainly to disprove some articles that appeared in newspapers and magazines of the sector of foreign nations that had stated that the S.M. 79 were:

“expressly built for a vain policy of prestige and therefore unsuitable for military uses, difficult to maneuver, excessively loaded, too delicate: in short, devices unable to withstand comparisons of practical use with similar foreign ones”

The French newspapers accused the Savoia-Marchettis saying that they could never win in a Paris – New York race due to limited range.It was also decided to test the possibility of transporting passengers and letters from Italy to South America with land based planes.The 3 S.M. 79Cs, I-BIMU, I-FILU and I-CUPA were taken and modified by SIAI-Savoia technicians, Direttorato Generale Costruzioni Aeree or DGCA (General Directorate of Aeronautical Construction) and the aeronautical military engineers.

The changes concerned the replacement of the propellers with the classic SIAI-Savoia propellers, a complete overhaul of the engines, an enlargement of the fuel fillers to reduce refueling time, improved radio, navigation aids, and autopilot.

The maximum take-off weight of the new version, now renamed Savoia-Marchetti S.M. 79T for Transatlantico (Transatlantic) was now nearly 14,000 kg, 3.5 tons more than the S.M. 79M.

After numerous test flights and tests carried up to December 1937, it was decided that the flight could be done.

The three aircraft were reassigned to different teams of pilots, Biseo and Paradisi took the I-BIMU now renamed I-BISE (MM. 359). Bruno Mussolini and Mancinelli took the I-FILU renamed I-BRUN (MM. 356) while Moscatelli and Castellani took the I-CUPA now named I-MONI (MM. 358).

The I-BISE during the Rome – Dakar route. [modellismoitalia.altervista.org]
On the morning of January 24th and at 0728 hrs, the three S.M. 79T took off from Guidonia airport for Dakar, the first leg of the Italy – Brazil.

The planes would have been in constant radio contact with Guidonia and Rio de Janeiro, periodically communicating their position.

At 0830 hrs the planes reported that they had flown over Capo Carbonara in Sardinia and at 0915 hrs they flew over Bona starting to fly over the mountains of the Saharan Atlas. At 1130 hrs the formation commander announced that he had slightly changed the planned route, turning north due to strong wind. At 1330 hrs the devices signaled strong wind with sand clouds and at 1530 hrs they communicated that they were within sight of the Atlantic at Villa Cisneros. At 1630 hrs they flew over Port Etienne and at 1745 hrs San Louis.

Landing in Dakar took place regularly at 1845 hrs Italian time. All navigation took place at an altitude ranging between 4,000 and 5,000 meters where the engines gave maximum power.

The actual distance traveled by the aircraft was over 4,500 km in 10 hours and 50 minutes, the average speed of 419 km/h.

After refueling in Dakar the I-BISE it’s ready to start the transoceanic flight. [modellismoitalia.altervista.org]
On the morning of January 25 at 0910 hrs (Italian time) the three planes left Dakar for Rio de Janeiro with a wing load of 220 kg due to the greater quantity of fuel and lubricant transported.

The navigation was done in close formation, which took place at an average altitude of 3,800 meters, but was disrupted in the central area of ​​the Atlantic by thunderstorms, headwinds, lightning and sudden showers of rain that forced the pilots to instrumental flight.

The I-MONI, due to a failure of the usual propeller, was forced to continue the flight with only two engines for 2,000 km of the crossing, significantly slowing its average speed to 312 km/h.

At 1730 hrs I-BISE and I-BRUN sighted the Brazilian coast and continued towards Rio de Janeiro, arriving at 2245 hrs at Dos Afensos airport in the midst of a crowd of people who arrived to celebrate the event.

Following a direct order from the commander of the I-MONI formation it headed to Natal where it landed at 1919 hrs for the necessary repairs. It should be noted that the plane could have made it to the finish line without any problems but the crew, tired from the crossing, preferred to land and repair the plane.

I-BISE and I-BRUN had thus completed an effective route of over 5,350 km (of which 5,150 km offshore) in 13 hours and 35 minutes at an average speed of 395 km/h.

The Rome – Rio de Janeiro connection took place within 39 hours and 17 minutes with 24 hours and 22 minutes of actual flight for an average of about 406 km/h on a route of 9.800 km. The I-MONI departed from Natal at 1158 hrs on January 28, and arrived regularly in Rio de Janeiro at 1742 hrs on the same day.

This showed that the Savoia-Marchetti S.M. 79 were not “too delicate” aircraft as foreign press had claimed, capable of reaching South America even with a failed engine.

Photos of the crew of the three S.M. 79T that had made the transoceanic flight. Compare the propeller cap with the photos of the S.M. 79Cs and you could clearly see the difference from the SIAI-Savoia propellers and the Ratier ones. [modellismoitalia.altervista.org]
It should be emphasized that the crossing was not a mere move by fascist propaganda, in fact, it was specifically chosen to lengthen the journey going from Dakar to Rio de Janeiro (5,350 km) instead of Natal (3,150 km).

Another factor was the speed, an average of 406 km/h for 9,800 km had never been sustained, in a single crossing the S.M. 79T broke two records, the speed one on the Rome – Rio de Janeiro route and the highest average speed one on the 5,000 km journey.

Brazil

After the 24 January 1938 race, the three S.M. 79 Transatlantico were then presented to the Aviacao Militar Brasileira (Brazilian Military Aviation). On 27 April 1938 I-BISE, I-BRUN were bought and renumbered K-422, K-420 while I-MONI was donated by Italy and renumbered K-421.

On 9 May 1938 they were assigned to the Escola de Aviacão Militar (Military Aviation School), where Maggiore Nino Moscatelli acted as instructor on at least three flights on 28 June (serial not reported) and then 1 July 1938 with K-421 and 8 July 1938 with K-420 before to returning in Italy acting as a bomber pilot.

On 28 October 1938 K-420 (Italian military serial number MM. 356) was flown by Brazilian pilot Loyola Daher, experienced an accident during a take off but luckily was later repaired, for it was recorded as flying in September 1941. The K-420 retired from service from the Escola de Aviacão on 12 February 1943.

On 9 July 1939 an unidentified S.M. 79T flown by Major Rubens Canabarro Lucas set a speed record by flying from Porto Alegre to Rio in 2 hours and 50 minutes at an average speed of 423 km/h (263 mph).

On 29 June 1943 was the last flight of an S.M. 79T for the Brazilian Air Line made by K-422 piloted by pilot Maldonado.

The service of the S.M. 79T as a training aircraft ended on 25 October 1944 when K-421 and K-422 were officially grounded by the Escola de Aeronautica.

Civil Service

The I-TOMO, I-ROTR and the reconstructed I-LICA aircraft were modified with a cabin for 4 passengers, the rest of the plane was used for cargo transport. They were used for the Rome – Rio de Janeiro route since 1939 by the Italian civil airline Linea Aerea Transcontinentale Italiana or LATI (Eng: Italian Transcontinental Airlines) part of the Ala Littoria.

The three aircraft, whose name does not seem to be clear since some sources call them Savoia-Marchetti S.M. 79C, others S.M. 79T and others S.M. 79I, were used mainly for the transport of mail on the route Rome – Seville (Spain) – Lisbon (Portugal) – Villa Cisneros (Morocco) – Ilha do Sal (Cape Verde) – Recife (Brazil) – Rio de Janeiro.

At least one was diverted to the Regia Aeronautica in June 1940 when the Kingdom of Italy joined the Nazi Germany in the Second World War. The aircraft, I-ALAN was requisitioned by the Regia Aeronautica and used to transport military equipment from Italy to Abyssinia (Italian name for Ethiopia) while maintaining its civilian livery.

Unfortunately only 6 days after the beginning of the war, on the 16th of June 1940 the I-ALAN had some problems during a take-off from Benghazi in Libya and was forced to abort the departure.

During re-landing the undercarriage collapsed and the aircraft crashed on the runway without causing too much damage and without casualties.

The aircraft, impossible to repair due to lack of parts, was moved to the side of the runway and probably cannibalized for spare parts to be used on other Savoia-Marchetti.

The carcass of the I-ALAN remained abandoned on the side of the runway of Benghazi for a long time and the British troops found it there in February 1941 when they conquered the Libyan city.

The I-ALAN among numerous other abandoned fuselages at Benghazi Airport in 1941. [sites.google.com/site/lgarey/benghazigraveyard]
The I-ALAN when the British troops conquered the Benghazi Airport in 1941. [sites.google.com/site/lgarey/benghazigraveyard]
Not much is known about the other two aircraft, but they were probably used on the Atlantic route together with the Savoia-Marchetti S.M. 83 (civil version of the S.M. 79) and the Savoia-Marchetti S.M. 75.

At the beginning the crossing was carried out weekly: departure on Thursday from the Italian territory and collecting the Italian mail on the way, then, landing in the two Iberian countries, the Spanish and Portuguese mail was collected, arriving in Brazil, the Brazilian mail directed to the three European countries was loaded and the return journey was made.

After June 10, 1940, with the Italian declaration of war against France and the United Kingdom, the transatlantic flight had to be reduced to only one crossing per month. They were finally stopped on December 19, 1941 as a result of the entry into war of the United States, which controlled the Atlantic airspace and especially because the US government forced Brazil to break all diplomatic relations with Fascist Italy and therefore also to block the possibility of using their airports.

Italian civil airline Ala Littoria’s Savoia-Marchetti S.M. 79C in 1939 in the standard blu and white livery. [Wiki]

Camouflage and Markings

The planes were painted in a very flamboyant livery: Ruby Red with green and white lines.

The rudder had the Italian tricolor with the Savoia coat of arms in the center.

The lictor beams, symbol of the Italian Fascist Party, were painted on the engine cowlings, while on the fuselage, under the cockpit was written “S.M. 79. Savoia-Marchetti”.

In the center of the fuselage, the aircraft codes were written on the sides, inside a white rectangle with black borders.

Also on the sides were painted three green mice intent on laughing at each other, this was the symbol of 205ª Squadriglia da bombardamento “Sorci Verdi”, and in fact, in Italian, “Sorci Verdi” means green mice.

This symbol will then also be painted on the S.M 79M of the squadron during the Spanish Civil War and the Second World War.

On the Savoia-Marchetti S.M. 79T the livery was the same except for the codename written bigger without the white rectangle, and also because on the tail was added a small white rectangle with the codename of the aircraft during the first race.

After being delivered to the Aviacao Militar Brasileira, the aircraft were repainted green, with a yellow rudder. Brazilian serial numbers were then applied, painted in black on the sides and the “Brazilian Stars” on the wings.

The livery of S.M. 79C converted for civilian use was on an ivory white background with a blue line on the side.

Behind the cockpit was the inscription ‘ALA LITTORIA S.A. LINEE ATLANTICHE’, S.A. stands for “Società per Azioni” in English Joint-stock Company, the identification mark (in that case) I-ALAN and a Kingdom of Italy flag on the tail.

Gallery

Savoia-Marchetti S.M. 79 Transatlantico former I-BRUN in service with the Aviacao Militar Brasileira
Savoia-Marchetti S.M. 79C, I-ALAN converted in mail plane before June 1940.
Savoia-Marchetti S.M. 79 Transatlantico former I-FILU piloted by Bruno Mussolini and Mancinelli during Rome – Dakar – Rio Race
Savoia-Marchetti S.M. 79 Corsa with the livery of Cupini and Paradisi plane for the Istres – Damascus – Le Bourget Race
Savoia-Marchetti S. 79 prototype, the I-MAGO

Credits

  • Written by Arturo Giusti
  • Edited by Henry H. & Ed J.
  • Illustration by Godzilla

Sources

Fiat G.50 in Independent State of Croatia Service

Independent State of Croatia flag Independent State of Croatia (1942)
Fighter –  16 Operated

In NDH service the Fiat G.50 did not receive any modifications, with the original Italian camouflage remaining. The only change was the addition of Croatian military markings and new identification numbers. [Wiki]
Following the creation of the Nezavisna Država Hrvatska (Independent State of Croatia), its Air Force was plagued with many problems from the start, including a lack of modern aircraft. While generally heavily reliant on the Germans to provide them with better equipment, they were unwilling to secure any deliveries of aircraft. To resolve this issue the NDH’s Air Force officials managed to persuade Italy to sell them 10 Fiat G.50bis fighters, which remained in use up to 1945.

A Brief History of the NDH

Following the end of the First World War, Kraljevina Srba Hrvata i Slovenaca (The Kingdom of Serbs, Croats, and Slovenes – SHS) was formed in December of 1918 with the aim of uniting all Southern Slavs. This new state was, at least in theory, based on the principles of equality for these three nationalities. In reality, this Kingdom was a politically and ethically divided country. During the 1920s, there were huge political disagreements between the major parties which brought about questions regarding the continued existence of the Kingdom of SHS. This division was especially noted between the Serbian and Croatian politicians, which ultimately culminated in the assassination of several Croatian Peasant Party members, including the leader, Stjepan Radić, by a Serbian Politician in 1928.

On 6th of January, 1929, King Aleksandar Karađorđević, in an attempt to avoid the incoming political crisis, led the country into a dictatorship by abolishing parliament. He also introduced a number of political changes, including changing the name of the country to Kraljevina Jugoslavija (Kingdom of Yugoslavia.) This essentially did not resolve any of the existing problems, as inter-ethnic tensions persisted. During the early 1930s, the first mentions of Croatian Ustaše (the precise meaning is unknown, but could be roughly translated as insurgent) ultranationalist revolutionary organizations began to appear in Yugoslavia. Their main aim was the liberation of the Croatian people from Yugoslavia, by all means necessary, even by force. One of the most prominent figures of this organization was Ante Pavelić.

Ante Pavelić was a high-ranking Ustaša member from the start, and later de facto leader of the NDH. [Wiki]
The Ustaše organization participated in the assassination of the Yugoslav King, Alexander Karađorđević, in Marseille in 1934. This assassination backfired to some extent for the Ustaše organization. Not only did it not lead to the collapse of Yugoslavia, but relations with Italy also improved under the Regent Prince Pavle Karađorđević in the following years. This led the Italian authorities to effectively end their support for the Ustaše and even arrested some of its members, including Pavelić.

After years of inactivity, the Ustaše benefited when the Yugoslavian government, which supported the Axis, was overthrown by pro-Allied officers in a military coup at the end of March 1941. Adolf Hitler almost immediately issued an order that Yugoslavia should be occupied. The Italians, preparing to join the war against Yugoslavia, began to support the Croatian Ustaše movement once again. With the collapse of the later Kingdom of Yugoslavia during the Axis invasion after the short April War of 1941, Croatia, with German aid, was finally able to declare independence, albeit becoming a fascist puppet state. Ante Pavelić was chosen as the leader of this puppet state. Officially, the NDH was announced on 10th April 1941. The new state received a significant territorial expansion by annexing most of western Yugoslavia, including Bosnia, parts of Serbia, and Montenegro. The Adriatic coast, while nominally part of the NDH, was actually controlled by the Italians until 1943.

The NDH took over a large portion of the Yugoslavian territories. [Wiki]

Formation of the NDH Air Force

Following the collapse of the Kingdom of Yugoslavia, NDH began organizing its newly-created armed forces. Its Air Force was created on the 19th of April, 1941. The leadership of the new Air Force was given to Colonel Vladimir Kren. Immediately, work began on creating adequate structural organization, acquiring manpower, and procuring equipment. Initially, plans for arming this Air Force were ambitious, including some 140 modern aircraft, such as the Ju 88 and Me 109. Its officials were quite disappointed as Germans were not willing to provide these. Instead, the NDH officials had to make do with the leftovers of the Former Royal Yugoslav Air Force, which was in German hands. NDH officials made a request that included over 50 aircraft. The Germans once again disappointed them and gave NDH only those aircraft that were mostly obsolete, while transferring the better aircraft, like the Hurricanes, to Romania instead. The only other way to acquire more capable aircraft was to ask the Italians. This is what the NDH Air Force officials did in early 1942.

The NDH Air Force was initially equipped with surviving Yugoslavian aircraft, in this case, Rogožarski P.V.T. [The Croatian Air Force In The Second World War]

The Fiat G.50 brief history

During the thirties, the Italian Ministry of Aviation (Ministero dell Aeronautica) was interested in adopting a new, all-metal monoplane fighter and ground-attack aircraft for the Italian Air Force. In April of 1935, engineer Giuseppe Gabrielli began working on a new low-wing, all-metal plane named G.50. On 28th September 1935, Gabrielli submitted his project to the Ministry of Aviation. Military officials were impressed by the design and asked him to proceed with its work. As Fiat’s production capacities were overburdened, work on this new project was instead moved to the CMASA works at Marina di Pisa, part of Fiat since 1931. Giuseppe Gabrielli was finishing his last drawings and the list of needed materials and equipment in June 1936.

The prototype was finally ready at the beginning of 1937 and was transported to the city of Turin for further testing. This prototype, under registration number MM 334, made its first test flight on 26th February 1937. Once accepted for service, the Fiat G.50 would become the first Italian all-metal fighter. Between 1938 to 1943 some 774 to 791 of all versions of the G. 50 would be built. These saw combat service starting from the Spanish Civil War, until 1943 when the few surviving aircraft were reassigned to secondary roles.

A G.50 flying together with a German Bf-110, possibly during the Battle of Britain. [Wiki]

In Yugoslavia

The Fiat G. 50 participated during the short Invasion of Yugoslavia in April 1941. Two fighter groups, the 24th, and 154th, which had 53 G.50 fighters in total were allocated for this operation. They mostly performed a few escort missions. Due to the rapid collapse of Yugoslavia’s Royal Army, these saw limited actual combat use, if any. Afterward, the Fiat G.50 was allocated to other fronts. During 1942 and 1943, limited numbers of these aircraft were used for ground attack operations against the Yugoslavian Partisans.

In NDH’s Hands

By 1942, most of the available aircraft in NDH Air Force were in poor condition, mostly due to a general lack of spare parts. NDH Army officials approached Italy with a request for 9 improved Fiat G.50 and one two-seater version. The Fiat G.50bis were slightly modified versions that had an increased fuel load, a redesigned rear fuselage and vertical stabilizer, better glazing of the cockpit, and other minor changes. But in essence, it did not offer many improvements compared to the basic version. The G.50 B bipost (two-seater) was a modified G.50 fighter version with a new cockpit and dual controls for a pilot and trainer. The front section of the cockpit was fully enclosed, in contrast with the rear which was open. The main armament was removed on the G.50 B. This version was very successful, as it was easy to build and offered almost the same flying performance as the single-seat version.

The Fiat G.50 B version with a longer cockpit design for the instructor and the student. [alieuomini.it]
A group of six NDH pilots was sent to the Fiat company in Torino for training in January 1942. The entire acquisition process of new aircraft took several months to complete. The 9 Fiat G.50bis (serial number MM.6178 to 6186) were finally allocated to the NDH. These arrived in Croatia in April 1942. The Fiat G.50B two-seater took even more time to be delivered, arriving in late June 1942. These would be stationed on the Borongaj airfield near Zagreb. Initially, these were used for pilot training. Due to the poor condition of the airfield, two were lightly damaged during landing.

The Fiat G.50bis in NDH service. [asisbiz.com]
For the necessary pilot training, one modified Fiat G.50B two-seater was also acquired. [The Croatian Air Force In The Second World War]

Combat Use

Almost from the start, the new NDH regime began the persecution of all non-Croatian citizens. The Serbian, Roma, and Jewish populations were especially targeted, with numerous atrocities and arrests. Croatians who did not agree with this regime were also persecuted. In response to the NDH’s actions against Yugoslavian civilians, resistance movements began to emerge on its territory. Their Air Force was used in various roles during this time, but due to generally obsolescence of equipment, their impact would be quite limited.

The acquisition of more aircraft like the Fiat G.50 offered a slight increase in its offensive capabilities. Once in service, these received new registration numbers ranging from 2501 to 2509. The single Fiat G.50B received the 3510 designations. In July, five would be allocated to the Rajlovac airfield near Sarajevo. In September three were moved to the Banja Luka to be part of the 16th squadron.

After April 1943 most were pulled back to Zagreb where they were attached to the 1st Squadron. When Italy capitulated to the Allies, all warring parties in Yugoslavia rushed in to take over the abandoned Italian weapons, armored vehicles, and a few remaining aircraft. At Zadar airfield, there were six Fiat G.50 aircraft. These would be captured by the NDH forces. Three of them received 5686, 5956, and 5186 designations. The newly acquired fighters were primarily positioned at Kurilovac and Velika Gorica airfields.

By 1944 it was becoming obvious that the Axis would lose the war, as a result many soldiers and pilots from the NDH Army and Air Force tried to escape to the Partisans. On the 2nd of September 1944, air force pilot Andrija Arapović with a Fiat G.50 (reg. Num. 3505) escaped to the island of Vis, under the control of the Yugoslav communist Partisans. Partisan forces put the captured G.50 to use during the war and it would remain in service up to 1946. An interesting fact about Andrija Arapović’s G.50 aircraft is that it still exists today and can be seen in the Belgrade Military Aviation museum near the Nikola Tesla Airport in Serbia. This is the only surviving example of a G.50 in the world. Another Fiat G.50 escaped joining the Allies in Italy.

The Fiat G.50bis was piloted by pilot Andrija Arapović. On the 2nd of September 1944, he fled to the Partisan side. [The Croatian Air Force In The Second World War]
By this point the Allies had achieved almost complete air supremacy over southern Eastern Europe, thus flying the slower Fiat G.50 became quite dangerous. In April 1944 several NDH aircraft, including two Fiat G.50, were destroyed in an Allied bombing run on Borongaj. Due to their obsolescence, even the NDH’s best fighters could do little against Allied bombers. In addition, the chronic lack of fuel led to a reduction in combat flights. By mid-September 1944, only 7 aircraft were listed as operational. In October most were allocated to the 2nd Squadron, which was also equipped with MS 406 fighters. When the Partisans liberated Zagreb, some 9 aircraft in various conditions would be captured. Some would be put to use after the war, but their use would be limited.  These would be removed from service by the 1st of April 1946.

The Fiat G.50bis were often used to protect Zagreb but could do little against more modern Allied bombers. [The Croatian Air Force In The Second World War]

Technical Characteristics 

In NDH service no known modifications were made on the Fiat G. 50. The G.50 was a single-seat, low-wing, all-metal fighter plane. The main fuselage was made from four angular-shaped longerons. The wing construction consisted of a center section which was made of a steel tube connected to the lower fuselage and two metal spars connected with ribs. The fuselage, wing, and tail were covered with duralumin sheets. The only fabric-covered parts were the movable control surfaces in the wings and the tail. It was powered by the 840 hp (626 kW) Fiat A 74 RC 38, a 14-cylinder radial piston engine. An all-metal three-blade propeller produced by Fiat was used.

The G.50 was equipped, like most modern aircraft of the time, with inward retracting landing gear, but the rear tail wheel was fixed. In later improved versions, the rear tail wheel was changed to a retractable type.

The main armament consisted of two forward-firing 12.7mm Breda-SAFAT heavy machine guns, with some 150 rounds of ammunition for each machine gun. The guns were placed behind the upper engine cowl and were synchronized in order not to damage the propeller.

Conclusion

The Fiat G.50 was one of few modern fighters available for NDH service. Their use would be greatly hampered by ever-increasing Allied Air supremacy, lack of fuel, and fear of their pilots defecting. Despite being acquired in relatively small numbers many of them would survive the war albeit in poor condition, while some would see a few more years of service by the newly created Yugoslav Air Force.

Fiat G.50 Specifications
Wingspan 10.9 m / 35 ft 11 in
Length 8 m / 26 ft  3 in
Height 3.28 m / 10 ft 7 in
Wing Area 18.25 m² / 196.5 ft²
Engine One 840 hp (626 kW) Fiat A.74 RC.38, 14 cylinder radial piston
Empty Weight 1,975 kg / 4,350 lbs
Maximum Takeoff Weight 2,415 kg / 5,324 lbs
Fuel Capacity 316 l
Maximum Speed 470 km/h / 292 mph
Range 445 km / 267 mi
Maximum Service Ceiling 10,700 m / 35,100 ft
Climb speed Climb to 6,000 m (19,700 ft) in 7 minutes and 30 seconds
Crew One pilot
Armament
  • Two 12.7 mm Breda-SAFAT heavy machine guns

Credits

  • Written by Marko P.
  • Edited by Henry H. & Ed J.
  • Illustrated by Haryo Panji

Sources:

  • D. Nešić (2008), Naoružanje Drugog Svetsko Rata-Italija, Beograd.
  • G. Cattaneo, The Fiat G.50, Profile Publications number 188
  • P. Verganano (1997), Fiat G.50,, La Bancarella Aeronautica – Torino.
  • D. Monday (1984, 2006), The Hamlyn Concise Guide To Axis Aircraft Of World War II, Aerospace Publishing Ltd.
  • V. V. Mikić, (2000) Zrakoplovstvo Nezavisne Države Hrvatske 1941-1945, Vojno  istorijski institut Vojske Jugoslavije.
  • T. Likso and Danko Č. (1998) The Croatian Air Force In The Second World War, Nacionalna Sveučilišna Zagreb.
  • I. Černiševski (2012) Maketar Plus, IPMS Srbija

 

Reggiane Re.2002 Ariete

italian flag Italy (1940)
Fighter Bomber – 48 Built

An Re.2002 belonging to the 239 Squadriglia stationed at Tarquinia airfield in Italy during June 1943. [vvsregiaavions.com]
Following the failure of the Re.2000, the engineers from Reggiane tried to design a new aircraft to fill the role of ground attack aircraft. This would lead to the development of the improved Re.2002 aircraft. While the Regia Aeronautica (Italian Air Force) ordered 500 of this version, due to problems with production, only about half of that number were ever built.

History

In the late 1930s, Italian aircraft manufacturer Reggiane was attempting to gain attention from the Reggia Aeronautica with its Re.2000. While this aircraft initially showed good flying performance, it was not adopted for service. For this reason, Reggiane’s chief engineer, Roberto Longhi, set out to develop a new aircraft that would fulfill the role of a fighter-bomber aircraft, which the Italian Air Force was in desperate need of. Roberto Longhi made sure to address the shortcomings of the Re.2000’s fuel tanks when designing the new aircraft. These were prone to leaks, so he replaced them with conventional fuel tanks. For this new aircraft, that would later be known as the Re.2002 Ariete (Ram), a large 1,175 hp Piaggio P.XIX R.C.45 Turbine (Whirlwind) – D 14 cylinder air-cooled radial engine was chosen. The Piaggio P.XIX R. engine was still in the development phase at that time and not yet ready for service. The choice of using an engine still in the development phase would have a great negative impact on the later production of the aircraft. A radial engine was preferred over an inline liquid-cooled engine due to the fact that it was durable and less vulnerable to ground anti-aircraft fire. The new aircraft had a number of similarities to Reggiane’s earlier designs, possessing the overall shape of the Re.2000, and the Re.2001’s internal construction.

First Test Flight

The maiden flight of the Re.2002 (M.M. or MM 454) prototype took place in October 1940. It was flown by test pilot Mario de Bernardi. After the first flight, the pilot noted that the Re.2002 had good general flying performance, but there were problems with the engine overheating. After several more test flights, constant engine overheating problems forced further flights to be halted, and the aircraft was returned to Reggiane for necessary engine modifications. After a number of upgrades to the engine were completed in March 1941, the test flights continued. During these tests, the Re.2002 managed to achieve a top speed of 417 km/h (260 mph).

The first prototype, ready to take to the sky. The picture was taken at the Guidonia airfield in April 1941. [vvsregiaavions.com]
Front view of the prototype. While it was chosen for production by the Italian Air Force, the production aircraft received some modifications. These included the use of a Re.2001 canopy and the addition of a fixed rear landing wheel. [vvsregiaavions.com]

Technical Characteristics

The Re.2000 was designed as a low wing, all-metal construction single-seat ground attack plane. The fuselage consisted of a metal frame covered with aluminum sheets held in place by using flush-riveting. The elliptical wings were built using a metal frame covered with a stressed skin duralumin structure. One fuel tank was located in each wing, with an additional third one placed just behind the pilot. If needed, additional auxiliary fuel tanks could be added under the fuselage or the wings.

Side view of the Re.2002 prototype. The most obvious change compared to later production planes was the removal of the rear glazed part of the canopy. [vvsregiaavions.com]
The landing gear system was unusual, but standard for Reggiane aircraft. When it retracted backward, the wheel rotated 90° before it retracted into the wheel bay. For better landing, the landing gear was provided with hydraulic shock absorbers and pneumatic brakes. The smaller rear wheel was initially retractable, but was changed to a fixed type at the start of production. The Re.2002 was powered by a 1,175 hp Piaggio P.XIX R.C.45 Turbine-D 14 cylinder air-cooled radial engine derived from the french Gnome-Rhône 14K Mistral Major. This engine was equipped with a three-blade variable pitch Piaggio P. 1001 propeller made by Piaggio.

The initial cockpit canopy was unchanged from the Re.2000 and opened to the rear. The production version had a canopy taken from the Re.2001. This canopy opened to the side.

Rear view of the Re.2002. [vvsregiaavions.com]
The Re.2002 possessed the same offensive capabilities as its Re.2001 cousin. It consisted of two Breda-SAFAT 12.7 mm heavy machine guns mounted in the engine cowling. The ammunition load for the left machine gun was 390 rounds, with 450 rounds for the right. Two additional 7.7 mm Breda-SAFAT machine guns were placed in each wing. The ammunition load for the right machine gun was 350 rounds and 290 rounds for the left.

Being designed to act as a ground attack plane, the Re.2002 was equipped with one bomb rack placed under the fuselage with an additional rack placed under each wing. The central bomb rack could carry up to 650 kg (1,430 lb). The smaller wing racks could each carry up to 160 kg (350 lb) of payload.

The Reggiane family tree line. While the Re.2002 shared many visual similarities with the Re.2000, its construction was more similar to that of the Re.2001. [Reggiane Fighters in Action]

Production for the Italian Air Force

The first production aircraft, which was built in October 1941.[vvsregiaavions.com]
Following the completion of test flights, the Italian Air Ministry (Ministerio dell’Aeronautica) gave an order for 200 Re.2002s to be produced. The first production aircraft were completed in October 1941. Due to engine production difficulties, the distribution of new aircraft to front line units was only possible in late 1942. While the initial order of 200 was increased to 300, only between 48 to 147 (depending on the source) were built for the Italian Air Force by September 1943. Initially a production order of 200 was placed in March 1942, which would be increased to 300 later in 1943. The sources unfortunately disagree about the number of produced aircraft. For example, sources like J. F. Bridlay (Caproni Reggiane Re 2001 Falco II, Re 2002 Ariete and Re 2005 Sagittario) listed a production number of 147 aircraft, which is the highest number listed in the sources. Other like Duško Nešić (Naoružanje Drugog Svetsko Rata-Italija) and David Monday, (The Hamlyn Concise Guide To Axis Aircraft OF World War II) gives us a number of 50 aircraft. While George Punka (Reggiane Fighters In Action) gives us a number of 48 aircraft. All previous numbers do not include later aircraft, especially built for the Germans which is often listed as around 60 or so. The lower production numbers were due to many reasons, lack of production capabilities, scarce resources, supply problems with engines, among others. The disagreement among sources may be the consequence of confusing the number of produced versus actually delivered aircraft.

 

Further Development

With only a small number of aircraft ever built, there were only a few known modifications and proposals for the Re.2002. One was an experimental version created by combining the Re.2002’s fuselage with the Re.2005’s wings. This aircraft was known as Re.2002 bis, but was never truly completed. The second version was to be used on two Italian aircraft carriers, the Aquila and Sparviero. While catapult launch tests were conducted on at least one Re.2002, due to the cancellation of the Italian aircraft carriers, construction of this version was never pursued. One Re.2002 was tested in the Re.2003 two-seater reconnaissance aircraft configuration. As the Re.2003 was not adopted for service, only one prototype was built. The last proposal included a torpedo carrier version, but this was never implemented. The majority of these do not appear to have received any special designation.

In Italian Service

After the introduction of the Re.2002 into service, some additional changes were made in comparison to the prototype. These include: improvements to the engine cowling, introducing a fixed rear tail wheel, and changing the canopy with a new one based on the Re.2001. The improved engine cowling actually caused some issues during dive-bombing runs, as the engine would sometimes simply stall. From the 17th aircraft onward, a new lower engine mount was tested with a different cowling type.

Delivery of the first operational Re.2002 for military  use was only possible in November 1942. The Re.2002s were allocated to the 102º Gruppo, with its 209ª and 239ª Squadriglia, stationed at Lonate Pozzolo. This unit had experience operating ground attack aircraft, previously operating German-supplied Ju-87 dive bombers. The next month, the 101º Gruppo, with its 208ª and 238ª Squadriglia, also began to receive their first Re.2002s to replace their outdated FIAT C.R. 42 biplanes.

During the Allied invasion of Sicily in July of 1943, the Italian Air Force stationed there had only 165 operational aircraft. Two groups, equipped with some 32 Re.2002 in total, were also present as part of the 5º Stormo. The first combat action was on the day of the invasion on the 10th of July, when Re.2002s managed to sink an Allied transport vessel called Talamba. Four aircraft and the commander of the 5º Stormo Colonel Guido Nobili were lost during this action. The next day, a group of 11 Re.2002s began a new attack on the Allied ships stationed near Augusta-Syracuse. The British battleship HMS Nelson was damaged with a 250 kg (551 lbs) bomb, with the mission resulting in the loss of two Re.2002s. In retaliation, the Allies bombed the Re.2002 airfields a few hours later. Due to losses, the surviving Re.2002s were repositioned to Manduria. After receiving reinforcements, the Re.2002s attempted another attack on July 19th, but lost six aircraft in the process. On 20th and 26th July, transport ships Pelly and Fishpool were sunk.

An Re.2002 during its short operational life with the Italian forces in Sicily. [vvsregiaavions.com]
In early September 1943, Allied forces landed in Southern Italy. The Italian command, in despair, dispatched a small group of aircraft supported by 15 Re.2002s in an attempt to drive them back. On 8th September, 1943, due to immense Allied pressure and rising military losses, the Italians surrendered. By this time, the 101º and 102º groups had only 24 Re.2002s, but only half were combat ready. During the two months of fighting, some 32 aircraft were lost. While 19 were lost in direct combat, the remaining were destroyed in Allied bombing actions or accidents.

In early September 1943, the 50º Stormo, with its 158º and 159º Groups, was undergoing the process of conversion to the Re.2002. But, due to Italian capitulation, only the 159º Group received Re.2002s which were not used operationally.

In German Hands

The Germans operated around 60 Re.2002 aircraft. These were mainly used against the French resistance movement. [vvsregiaavions.com]
Following the Italian capitulation, Germany launched Operation Achse (Axis) with the aim of capturing a large portion of the territory of their former ally. This included a number of production facilities, such as the Reggiane factories. The Germans seized some 14 fully completed aircraft, and around 10 more which were under construction. As there was sufficient material available, the production of the Re.2002 continued for some time under German supervision. Due to the same persistent engine delivery problems, Reggiane officials proposed mounting the 1,600 hp BMW 801 engine in the Re.2002, along with other modifications such as an updated wing design. One engine mount was tested in Germany, which led to a production order of some 500 new aircraft in late 1943. However, as the Reggiane factories were destroyed in early 1944 by an Allied bombing raid, the delivery of this modified version was impossible. In the meantime, some 60 aircraft were produced by Caproni under German supervision. Reggiane was actually owned by Caproni, thus all the necessary tooling and equipment for the continued production of this aircraft was available. Not all 60 were accepted for service by the Germans. Due to the Allied advance in April 1945, around 25 were seized by the Germans, while the remaining airframes were destroyed. Additionally, two aircraft were built at Biella. Unfortunately, the exact use of these aircraft by the Germans is not well documented. For example, it is unknown if they were ever used against the Allies in Italy. It is known that these were used by Geschwader Bongart against French resistance around Limoges, Vercors, and Aisne in 1943 and 1944.

Former Italian Re.2002 that was seized or produced for the Germans received the standard German markings, including a Balkenkreuz and a Swastika. [vvsregiaavions.com]

On the Allied Side

Smaller groups of around 40 Re.2002s, that were previously used by 5º Stormo, were operated by the new Aeronautica Cobelligerante Italiana (Italian Co-belligerent Air Force) in cooperation with  the Allies. In October 1943, these were used to form the Gruppo Tuffatori, a dive-bombing group. In 1943, they saw action in supporting the Italian Resistance Movement in Northern Italy, an area which was controlled by the Germans. In 1944, they were also employed in attack operations across the Adriatic Sea, towards the Yugoslavian coastline. One of the last combat missions of the Re.2002 was a bombing run against Axis targets in Dubrovnik on 29th March, 1944. While the Co-belligerent Army lost 9 aircraft in combat, further combat missions had to be aborted due to a general lack of spare parts, their operational life lasted less than 12 months. The surviving aircraft were reallocated to the Fighter Training School at Lecce-Leverano in June 1944. There, they were used for pilot training for a few months, before they had to be discarded, once again due to a lack of parts and poor mechanical condition. 

The Esercito Cobelligerante Italiano had close to 40 Re.2002 aircraft in its inventory. These would be used sometimes to support Italian Partisans in Northern Italy and on the Yugoslavian coastline. [vvsregiaavions.com]

Production Versions

  • Re.2002 (MM 454) – Prototype aircraft
  • Re. 2002 – Production version

Prototypes and Proposed Versions

  • Re. 2002 bis – An experimental version created by combining the Re.2002’s fuselage with the Re.2005’s wings. One built, but never used operationally.
  • Re. 2002 Aircraft Carrier Version possibly one modified for this role
  • Re. 2002 – Proposed torpedo carrier version
  • Re. 2002 – Powered by a 1,600 hp BMW 801 engine. While the engine mount was tested and a production order was given, no aircraft were ever fully completed
  • Re.2002 – One aircraft modified and tested as Re.2003

Operators

  • Kingdom of Italy – 147 aircrafts were delivered to Regia Aeronautica
  • Germany – After the Italian surrender to the Allies, Germany seized around 60 aircraft.
  • Esercito Cobelligerante Italiano – Operated some 40 Re.2002 aircraft

Surviving Aircraft

Today, there are only two surviving Re.2002 aircraft. One was located at the Italian Air Force Museum. The second incomplete Re.2002 can be seen at the French Musée de la Résistance et de la Déportation of Limoges.

The only fully surviving Re.2002, located at the Italian Air Force Museum. [Wiki]
The partly complete Re.2002 located at the French Musée de la Résistance et de la Déportation of Limoges. [Musée de la Résistance]

Conclusion

While the Re.2002 proved to be able to fulfill the role of fighter-bomber that the Italians were lacking. Due to a number of factors, its production was severely hindered. While work on the Re.2002 began in 1940, the production could not start before late 1942. Due to engine delivery problems, only a small number of aircraft were ever delivered to the Italian Force. Its first action against the Allies in Sicily ironically proved to be their last under the Fascist regime. While some would be used up to the war’s end, due to a lack of spare parts, most would be used as training aircraft until finally being discarded.

Re.2002 Specifications

Wingspans 36 ft 1 in / 11 m
Length 26 ft 9 in / 8.16 m
Height 10 ft 4 in / 3.15 m
Wing Area 220 ft² / 20.4 m²
Engine One 1,175 hp Piaggio P.XIX R.C.45 Turbine (Whirlwind)-D 14 cylinder air cooled radial engine
Empty Weight 5,270 lbs / 2,390 kg
Maximum Takeoff Weight 7,140 lbs / 3,240 kg
Climb Rate to 6 km In 8 minute 48 seconds
Maximum Speed 267 mph / 430 km/h
Cruising speed 250 mph / 400km/h
Range 683 miles / 1,100 km
Maximum Service Ceiling 36,090 ft / 11,000 m
Crew 1 pilot
Armament
  • Two 0.5 in (12.7 mm) heavy machine guns and two 0.31 in (7.7 mm) machine guns
  • One 1430 lb (650 kg) and two 350 lb (160 kg) bombs

Gallery

Illustrations by Carpaticus

Re.2002 in the Italian Royal Air Force (Regia Aeronautica Italiana)
Re.2002 from Esercito Cobelligerante Italiano (Italian Co-belligerent Army)
Re.2002 in German Luftwaffe Service

Credits

  • Written by Marko P.
  • Edited by Stan Lucian & Ed Jackson
  • Illustrations by Carpaticus
  • Duško N. (2008) Naoružanje Drugog Svetsko Rata-Italija. Beograd.
  • M. Di Terlizzi (2002) Reggiane RE 2000 Falco, Heja, J.20, Instituto Bibliografico Napoleone.
  • G. Cattaneo (1966) The Reggiane Re.2000, Profile Publication Ltd.
  • J. W. Thompson (1963) Italian Civil And Military Aircraft 1930-1945, Aero Publisher
  • G. Punka (2001) Reggiane Fighters In Action. Signal Publication.
  • Re.2002 Photographic Reference Manual
  • C. Shores (1979) Regia Aeronautica Vol. I, Signal publication.
  • J. F. Bridlay (1972) Caproni Reggiane Re 2001 Falco II, Re 2002 Ariete and Re 2005 Sagittario, Profile Publications
  • David. M, (2006) The Hamlyn Concise Guide To Axis Aircraft OF World War II, Bounty Books.
  • Images: Rod’s Warbirds Reggiane Re-2002 Ariete II –  http://www.vvsregiaavions.com/RegiaHTML/rre20021.htm

 

Breda Ba.65

italian flag Italy (1935)
Ground Attack Aircraft – 218 Built


 

The Ba.65 was ultimately an unsuccessful design, and was built in relatively small numbers. [warbirdphotographs.com]
The Breda Ba.65 was an Italian ground attack aircraft that first saw action during the Spanish Civil War. It was built in both single and two-seat configurations, and was exported to various nations prior to the outbreak of the Second World War, but only saw large-scale combat operations with the Regia Aeronautica in Northern Africa.

History

During the thirties, the Italian aircraft manufacturer Breda began working on developing several ground attack plane designs based on the theoretical principles set by World War One veteran fighter ace Colonel Amadeo Mecozzi. According to Colonel Mecozzi, the best use of aerial forces was the quick neutralization of military targets deep into enemy territory by using fast and very agile aircraft. Per his request, the major Italian aircraft manufacturers were to present their aircraft proposals for future use by the Italian Air Force (Regia Aeronautica).

The first aircraft design that tested Mecozzi’s idea was the Caproni A.P. 1 monoplane. It was utilized in small numbers during the Spanish Civil War, but the overall performance was underwhelming and, besides the small numbers built, it was not adopted for larger scale service. In the early thirties, Breda built a prototype of a ground attack plane named Ba.64, an all-metal low-wing aircraft powered by a single 700 hp Bristol Pegasus radial engine, license-built by Alfa Romeo. It was armed with four 7.7 mm (0.311 in) Breda-SAFAT guns in the wings, with one additional mounted in the rear gunner position, and a bomb load of around 400 kg (880 lb.) The Ba.64 was built in small numbers and by 1939, only 27 aircraft were reported in the Italian Air Force, which were used for second line duties only.

Side view of the Ba.65 K-14 two seat version. [warbirdphotographs.com]
A new improved design was built under the designation Ba.65 as a multi role aircraft, but it would end up being used mostly for ground attack. The prototype made its first flights in September 1935, piloted by Ambrogio Colombo. After a series of test flights, the prototype was handed over to the Air Force for further trials on the 27th October. The Ba.65 prototype made a flight from Milan to Rome, where it was to be handed over to the military, with an average speed of 412 km/h (256 mph). During its evaluation, a doctrinal problem emerged. Neither the Air Force Command staff, nor Mecozzi precisely specified what kind of performance specifications a ground attack aircraft should achieve. In order to solve this dilemma, the Air Force requested that the Ba.65 be flight tested with the results to be compared with those of the Fiat CR.32 biplane. The performance tests were held at the Guidonia Experimental Center near Rome. While the CR.32 biplane proved to have better handling, the Ba.65 was faster.

The production of the first group of 81 aircraft was started in 1936, and as the Ba.65 was produced in sufficient quantities, these were slowly adopted for service. Immediately after introduction to the Air Force, the Ba.65 proved to be a problematic design. From the beginning, pilots had significant problems learning how to control it, which resulted in several accidents, many fatal. Due to these accidents, the Ba.65 gained a bad reputation with Italians pilots. The main causes of the Ba.65’s difficulties mostly lie with poor pilot training, insufficient preparation, poor organization, and a lack of adherence to regulations.

Technical Characteristics

The Ba.65 was designed as a low-wing, single-engine, mixed-construction multi-role aircraft, including light bomber, attack aircraft, reconnaissance, and interceptor. The Ba.65’s fuselage was constructed of welded chrome-molybdenum steel tubes. The front fuselage and cockpit area (and the rear gunner area in the two-seat versions) were covered with sheet metal panels. This was done to make engine, or any other forward fuselage repairs much easier. The remaining fuselage was covered with fabric.

The wings were built using chrome-molybdenum steel tube spars, which were additionally connected with diagonal steel tubes. The leading edge of the wings consisted of duralumin sheets while the rear part was fabric covered. The ailerons and tail were also built using metal tubes covered in fabric. The tail consisted of two parts, the cantilever fin and the strut-braced tailplane.

Breda Ba.65 K-14 (MM 75085) two seat version equipped with the rear turret, which was armed with a Breda-SAFAT 7.7 mm ( 0.311 in) machine-gun. The Ba.65 was a relatively heavy aircraft, so the rear machine gun position was removed in the hope of reducing weight. [warbirdphotographs.com]
The Ba.65 had a then-modern retractable landing gear. It consisted of two larger front wheels, both of which retracted to the rear under-wing fairings. The landing gear system could be operated hydraulically or mechanically if needed. The smaller rear tail wheel was fixed. The landing gear was usually protected from damage by metal covers, but in some cases these were removed, probably due to damage, or to make repairs easier.

The cockpit was well placed, with ample forward visibility. It was protected by a large fully glazed canopy which could be opened to the rear. The canopy did see a number of design changes during the Ba.65’s service life. Beside the standard control panel, the Ba.65 was also equipped with oxygen tanks, a voicepipe for communication between the pilot and the rear gunner (two-seat version only,) an electric generator, and fire extinguishers. There was space inside the cockpit for additional equipment, such as a radio or cameras, but these were never installed in any Ba.65. In the two-seat versions, the rear position housed the gunner/observer (depending on the mission.) The rear position would also undergo many design changes during the Ba.65’s operational service life, from being protected by a fully enclosed turret, to being open and later even removed in the hopes of reducing weight.

Isotta Franschini K 14
Fiat A 80

The engine used on the prototype and the first series of 81 planes was the 870 hp Isotta Fraschini K-14 fourteen-cylinder engine. There are differences in the engine strength depending on the source, with some indicating, 700 hp, 870 hp, or even 900 hp (D.. Monday, G. Garello., J. W. Thompson., respectively) Later, it was replaced with the stronger 1,000 hp (746 kW) Fiat A.80 RC.41 eighteen-cylinder engine. The engine was placed in a steel housing that was connected to the fuselage by four bolts.

The aircraft’s fuel was held into two tanks located behind the pilot, with a total capacity of 650 l. An additional fuel tank could be added in the bomb bay with a capacity of 370 l. With the standard fuel tanks, the Ba.65 had a flight endurance of 3 hours and 25 minutes. With the additional fuel tank, flight time increased to 5 hours. The main fuel tank was equipped with a “Semape” self-sealing system.

The two left wing machine guns. [warbirdphotographs.com]
The main armament consisted of two 12.7 mm (0.5 in) Breda-SAFAT heavy machine guns and two 7.7 mm (0.311 in) Breda-SAFAT machine guns. The machine guns were placed in the central parts of the wings. For the two-seat version, one additional 7.7 mm (0.311 in ) machine gun was placed in a ring mounted turret. During development, there were several different rear turret designs, either partially or fully enclosed. There is some disagreement in the sources about the designation of these turrets. Gabrielo G. named the fully enclosed version as type M and the partially enclosed one as the type L. Author David M. mentions the enclosed turret as type L. The standard ammunition load was 350 rounds for the heavier machine guns and 500 for the smaller caliber machine guns (without the rear machine gun). According to some sources, the type L turret was armed with one 12.7 mm (0.5 in ) heavy machine gun.

The interior bomb bay could be equipped with either four 50 kg (110 lb) or two 100 kg (220 lb ) bombs placed vertically. Another optional loadout consisted of a container with 168 smaller 2 kg (4 lb). Additionally, 200 kg (440 lb) of bombs could be carried on the bomb racks located under the wings, but these were not always used. The theoretical maximum bomb load was 2,200 lb (1,000 kg) but, due to the plane’s excessive weight and the poor engine performance, this loadout was never used operationally nor in combat. The bombsight was located in the cockpit.

Further Development

Due to its poor performance, the Italian Air Force formed a commission with the aim of determining if the Ba.65 could be modified or improved to justify its continued production. The commission was made up of five Air Force officers and was led by Engineer Parano. After a short analysis, the commission noted that the Ba.65’s two-seat configuration was too heavy. This, combined with an underpowered engine, were the main reasons for the Ba.65’s poor flight performance. The commission made several modification suggestions which would be implemented in the second Ba.65 production series.

Engine Cowling for the K14
Engine Cowling for the A80

The previous K-14 engine was replaced with a stronger 1,000 hp eighteen cylinder Fiat A.80 engine. This resulted in an increase in the overall performance during climbing, take-off and cruising at top speed. The maximum speed with the stronger engine was 430 km/h (270 mph) with an effective range of some 550 km (340 mi ) and a service ceiling of up to 6,300 m ( 20,700 ft). The two engines had different cowling designs. The K-14 had 28 (14 pairs) smaller cylinder covers, and the A.80 had 18 longer cylinder covers. The new improved version is often designated simply as Ba.65 A.80 but, in some sources, it is also called “Ba.65 bis”.

The Ba.65 was also tested with the Piaggio P.XI engine, which was some 100 kg (220 lb) lighter than the K-14. The overall flight performance was improved, but due to the high cost, the proposal that all aircraft should be equipped with this engine was rejected. Additionally, a Pratt and Whitney R-1830 engine was allegedly tested on the Ba.65 (intended for Chinese export), but it is unknown if it was actually installed, or just planned.

Other improvements were made to the A-80 version. The rear machine gun mount was replaced with a new ring mounted machine gun turret. The landing gear was redesigned and improved. Great attention was given to reducing the weight as much as possible. To solve the problem with the overloaded wings, two Handley-Page slats were installed at the wings’ leading edges, which also improved the flight performance. On the tail, additional weighted ballasts were added to help with stability during flight.

Despite these modifications, the newly produced Ba.65 was criticized by pilots who were unhappy with its flying performance. There were also a number of accidents which forced the Air Force to issue special orders in October 1938, according to which it was forbidden to fly unnecessary aerobatics unless it was approved or for training purposes. By April 1939, the Italian Air Force Command, in the hope of finally solving the problems with weight and flight performance, ordered the removal of the rear machine gun position and equipment. In July, additional orders extended this modification to the older Ba.65 K14 versions. Despite these modifications, the Ba.65 never achieved the potential the Air Force High Command hoped for, and the Italians entered the Second World War without a dedicated ground attack aircraft.

Training Version

Small numbers of Ba.65, together with Ba.64 and A.P.1 planes, were used for a short time as trainers at the Foggia Flying School. As the concept of ground assault was abandoned by the Regia Aeronautica in November 1939, all remaining Breda aircraft at this school were scrapped.

In Italian Operational Service

In Italian military service, the Ba.65 saw action in small numbers during the Spanish Civil War, while the only other major engagement was in North Africa. Allegedly, according to author J.W. Thompson, it was also used during the Axis forces attack on the Kingdom of Yugoslavia in April 1941, but this is unlikely as there is no proof to corroborate this.

Pre-War Use

Front view of the Ba.65 (MM 325) prototype aircraft. [warbirdphotographs.com]
In June 1936, the Ba.65 (MM.325) prototype was allocated to the 160a Squadriglia (Squadron) stationed near Ciampino for operational use. After the flight testing at Furbara, the first production aircraft was allocated to the 167a Squadriglia. At this time, the Italian Air Force began reforming the “Assalto” (attack) units into the 5a Brigata Aerea, which consisted of 5° and 50° Stormo (regiment) commanded by Colonel Mecozzi himself. At the time of formation, the 5a Brigata Aerea was equipped with older Caproni A.P.1 and Ba.64’s.

Due to slow production of the Ba.65, by 1937 only 20 were available for operational service. In 1938, the newer and improved Ba.65 A.80 version was ready for service. Immediately after sufficient numbers of the A.80 were produced, the 5° and 50° Stormo were reequipped with them and the older K-14 versions were given to 2° Fighter Stormo.

The improved A.80 version, stationed at Lonate Pozzolo. [warbirdphotographs.com]
In May 1938, during Adolf Hitler’s visit to Italy, a live strafing exercise was organized at the Furbara airfield with 18 Ba.65 and 7 A.P.1 aircraft. During this exercise, a single Ba.65, piloted by Lieutenant Colonel Savarino, was flight tested with a payload over 1,000 kg (2,500 lbs) of equipment and bombs) of 1,160 kg (2,560 lb). After his first test flight, the pilot noted that it was nearly impossible to fly the fully loaded Ba.65. In a second test, the load was reduced to 900 kg (1,990 lb). This time, the flight was more successful, but the aircraft was still reported as uneasy and unpleasant to fly.

During 1938, there were many flight accidents in which eight pilots lost their lives. This forced the Air Force to ground all Ba.65 from October 1938 to January 1939. Because of this decision, training of all pilots in the ground attack role was reduced, which affected combat readiness. At this time, the order for a further 33 aircraft was put on hold until a final decision was made about the fate of these units and the type of aircraft with which they should be equipped. The introduction of the new Breda Ba.88 (which turned out to be an even more disappointing design) persuaded the Italian Air Force Command to replace the Ba.65 with this aircraft. The 5° Stormo was reequipped with the new Ba.88, while 50° Stormo still operated Ba.65 aircraft in a limited role by early 1939.

A Ba.65 flying above Rome during a training flight. These were part of 5° Stormo. [warbirdsphotographs.com]

In Spain

During the Spanish Civil War, Italy and Germany actively supported Francisco Franco’s fascist forces by sending significant military support which consisted of military equipment like small arms, tanks, aircraft, troops, engineers and trainers. This war would be used as a testing ground for many new military aviation designs, including the Ba.65.

In April 1937, the first group of 13 single seat Ba.65 K-14 arrived in Seville. They were attached to the 65a Squadriglia (Sq) Aviazione Legionaria under the command of Captain Desiderio. This unit’s entry into operational service would be delayed until August 1937. This unit was later relocated to Tudela in order to help fascist forces during the battle of Teruel in late December 1937. During this battle, the 65a Sq, under the new leadership of Captain Fanali, performed large, aggressive sorties against Republican forces. The 65a Sq was also very active during the Republican Ebro offensive in July 1938. The battle ended after 115 days with a Republican defeat, with over 80,000 casualties and the loss of large numbers of planes. The Ba.65s were used during the capture of Barcelona in late January 1939.

As the Spanish Civil War ended, the Ba.65 crews were sent by ship to Italy, with the remaining 11 aircraft given to the new fascist Spanish state. During the war, Italy sent around 23 Ba.65 aircraft, of which half were lost. Only three Ba.65 aircraft were destroyed by enemy action. The Breda was used in several different roles during the war. It performed poorly in the role of interceptor due to its inadequate handling and the slow climb rate. Due to stiff controls, lack of an oxygen mask, and the ensuing physical fatigue of the pilots, high altitude scouting missions were also unsuccessful. The only real success was achieved in the fighter-bomber role.

During the war, the Italian crews added bomb racks under the wings. The bomb load was increased with two 100 kg (220 lbs) bombs which were dropped at an angle of 30-35°. An additional 168 smaller 2 kg (4 lb) fragmentation bombs (carried in the position of the second crew member) could be dropped during the climb. After the bomb load was dropped, the Ba.65 could engage ground targets with its four machine guns (two were heavy machine guns). During the Spanish Civil War the single seat version was mostly used, with the exception of a few missions when a rear observer or specialist was requested.

In Africa

Routine aircraft maintenance was necessary during the North African campaign. This picture was taken near Tobruk in November 1940. [warbirdphotographs.com]
Prior to the beginning of the War in Africa against the British, the 50° Stormo was plagued by a general lack of adequate training, poor organization, and bad mechanical condition of the Ba.65 aircraft. By June 1940, the Italians had around 160 Ba.65 aircraft, but only 11 were actually fully operational and could be used for front line service.

The 50° Stormo was moved to Benghazi in Libya. Once there, mechanical problems cropped up as the A.80 proved to be prone to overheating and the desert sand caused significant issues for the engines. In Libya, a series of accidents forced Air Marshal Balbo to order the Ba65 removed from operational frontline service. All Ba.65 were dismantled and were to be sent to Italy, with assault units to be equipped with any available aircraft capable of assault sorties. The only planes fit the role were the Caproni Ca.310, a twin-engined bomber trainer aircraft, which was far from ideal, and the older Fiat CR.32 biplane.

The 50° Stormo (with no Ba.65) was relocated to Sorman airfield near Tripoli in order to provide support to the ground forces during attacks on Tunisia. Due to the rapid British advance, this unit (with only seven Ca.310B) was moved to the T.2 military airfield near Tobruk. The Ca.310B proved to be inadequate for the task, and after only two bombing attacks on the British armored columns in June, they were removed from these units. Due to this, the Italian Air Force commander in North Africa, General Porro, was forced to order the return of all available Ba.65 planes to operational service.

The A.80 version, possibly somewhere in North Africa. [warbirdphotographs.com]
They were to be relocated from Benghazi to the T.2 airfield as soon as possible. Besides the 50° Stormo, the Ba.65 would be supplied to 12° (150th and 160th Squadrons) and 16° (167th and 168th Squadrons) Gruppo (Group). The 12° Gruppo saw heavy action and high attrition rate, and by the end of June only five Breda Ba.65 and five Fiat CR.32 were operational. In July, the 16° Gruppo arrived at T.2 airfield equipped with the CR.32 and a few older Ba.65 K-14 collected from Italy. These units achieved great success when attacking the British forces near Sidi Rezegh (25-27 July 1940), inflicting heavy damage. In August, six Ba.65 A.80 (with fighter cover of unknown type and numbers) attacked a British supply depot but were intercepted by British Gladiators. The engagement ended with three lost Gladiators, but the Italian losses (if any) are unknown. During General Graziani’s short offensive action toward Sidi Barrani in September, all Ba.65 equipped units were active. By the end of the Italian offensive, only 10 Ba.65 and 18 CR.32 were still operational.

On 18th October, a formation of six Ba.65 and seven CR.32 managed to attack a British airfield far behind the front line, in Egypt at Siwa Oasis. This air raid was repeated on 7th November 1940, with six Ba.65 and eighteen CR.32. Bombing actions continued throughout November. By the end of the month, the 12° Gruppo was sent to the rear for rest, recreation, and aircraft overhauls. At the same time, the British launched Operation Compass, which eventually led the attacking Italian Army to collapse. The 12° and 16° Gruppo were allocated to the A.3 airfield near Amseat.

In early December, Britain’s 7th Armoured Division under the command of General O’Connor managed to break the Italian line of defense and began racing to the west. The 50° Stormo, along with all its planes, was dispatched to stop British armored attacks. This attempt failed and the unit lost all its aircraft. The same fate was met by the 16° Gruppo, which was evacuated to Italy on 2nd January 1941, without any operational aircraft. The 12° Gruppo lost most of its aircraft in January and, by the 14th of February, it also was relocated to Italy. With its departure, the Ba.65’s combat service ended.

In Foreign Service

After World War I, Italy became known around the world for the production and export of aircraft, especially during the thirties. This was mostly achieved due to a successful commercial strategy in the international aviation market. Despite the Ba.65 being an unsuccessful design, several countries showed interest in buying this type of aircraft, but their use was very limited. These include Iraq, China, Portugal and Chile. Italians also presented the Ba.65 to the Kingdom of Yugoslavia, but nothing came from this.

In Iraqi service

Iraq was under the great political and military influence of Great Britain, which meant that they were more or less forced to accept any British Foreign Office decision, including the acquisition of weapons. For a long time, the Iraqis wanted to break away from British influence, or at least reduce it. For this reason, the Iraqi Air Force Chief of Staff Colonel Jewad visited Italy in 1937, in the hopes of concluding a contract for the purchase of new aircraft types which would be used to equip the Iraqi Air Force. During the negotiation with the Italian Aeronautical Export Committee (AEROCONS) in 1938, it was agreed that Iraq would buy 15 (25 according to David M.) Breda Ba.65 aircraft, two of which were the dual control version. In addition, 25 A.80 engines were also bought. All combat aircraft were two-seaters, equipped with the rear mounted Breda turret.

These aircraft were shipped and disassembled into smaller parts, arriving by ship in Iraq. Along with them, a group of Breda engineers under the leadership of Lieutenant Guza, were sent to help with assembly. The transportation process was slow due to the long distance, and the need to test each aircraft after assembly meant that these planes could not enter operational service before November 1938. After this, the process of training the Iraqi pilots began. The Iraqis did not have any problems adapting to the Ba.65 and only one accident was recorded with the loss of the pilot’s life. In May, Guza and his team returned to Italy, with a positive report about the Ba.65 in Iraqi service.

In 1941, there was an uprising led by Rashid Ali, who, with the promise of Axis support, began preparations to expel the British Forces from Iraq. During the Anglo–Iraqi War in May of 1941, all Ba.65s were allocated to the 5th Squadron. This unit saw action against the British forces, but after several attacks only two were left operational. The Italians sent a CR.42 squadron to help the Iraqis but it arrived too late to change the war’s outcome. This unit, seeing the poor Iraqi situation, returned home after a short time. The fate of the surviving Ba.65s is unknown.

Production Attempts in China

For some time, the Italians were trying to negotiate with Chinese authorities about opening an aviation production factory in China. After initial negotiations in June 1934, the Chinese signed a contract with the Aeronautico Italiano per la China (Aerocina). This company was owned by the Italian Government in conjunction with Caproni, Breda, Fiat and SIAI. According to this contract, the Italians were to build the SINAW (Sino-Italian National Aircraft Works) factory in Nanchang. With this agreement, the Italians were to provide tooling, parts, and machines necessary for the factory to work. The head of the soon-to-be factory was the Italian Luigi Acampora and the Director was General Chu Lin. The production of the first operational aircraft was to begin from July 1937 and all Italian personnel were to return to Italy after five years of cooperation.

SINAW officially started production in November 1936 with six Savoia-Marchetti SM.81B bombers. Future plans included local assembly of 30 Breda Ba.65s and 50 Fiat G.50s. Immediately after the start of the Italian-Chinese corporation, there was a disagreement about the assembly of the Ba.65. The Chinese officials insisted that it should be powered by the Pratt and Whitney R-1830 engine in place of the Italian K-14. The Italians were against this, but there was a compromise to equip them with the stronger A.80 engines. Despite this, the Chinese later on insisted on the Pratt and Whitney engines which led to delays in the realization of the project.

The factory was slightly damaged during the Japanese bombing action of Nanchang on the 20th of October, 1937. By November, the Italian Government made a decision to discontinue any further cooperation, and stopped all further deliveries of equipment and materials. This was done mostly due to Japanese military actions, and poor relations with the Chinese side. By early December 1937, all Italian personnel returned home, and the deal with the Chinese was abandoned without a single Ba.65 being built.

In Chilean Service

Rear view of a Chilean Ba.65. Chile bought 17 single-seaters and 3 dual control training versions in 1938. These were powered by the Piaggio P.XI engine instead of the weaker K-14 and armed with 12.7 mm Madsen type heavy machine guns. [warbirdphotographs.com]
In the summer of 1937 representatives of the Chilean Air Force force were sent to Italy to begin negotiations for the purchase of several different Italian aircraft designs. These negotiations were successfully completed, and a purchase was arranged for nine Nardi 305 trainers and seventeen single engine and three dual control training versions of the Ba.65. These were to be powered by Piaggio P.XI engines instead of the K-14. Also, the Chileans demanded that the 12.7 mm (0.5 in) Breda SAFAT heavy machine guns be replaced with Madsen machine guns of the same caliber. Due to these changes and the long voyage to Chile, the Bredas reached their destination on 14th December, 1938. The aircraft were stationed at El Bosque airfield, awaiting the training of the pilots to begin, but due to many delays this only began in March 1939. During these training flights, there were two accidents due to pilot errors. The Chilean Air Force was under great pressure from the press about the quality of these planes, which eventually led to the suspension of any further flights of the Breda. These accidents were caused mostly due to the poor quality of pilot training. Not willing to admit their mistake, the Chilean Air Force began negotiation with the Italians to exchange the Ba.65 with the CR.32. But the negotiations were delayed and were never resolved as the war in Europe broke out. The Ba.65 would be used up to the end of 1941, when the last flight was recorded. These would be replaced with more modern American planes later on.

In Portuguese Service

In January 1937, the Portuguese showed interest in the Ba.65. After some negotiations, the Portuguese Air Force ordered 10 Ba.65 A.80, some of which were equipped with the Breda M turret. The inexperienced Portuguese pilots were to be sent to Italy for extended flight training.

The Ba.65 would be used in the coming year, but due to the lack of resources and maintenance, the Portuguese had problems keeping them in working condition. In February 1941 a heavy storm caused the hangar that all the Bredas were stored in to collapse. As all were damaged beyond repair, the Portuguese Air Force ordered them to be scrapped.

Production and Modifications

Besides the prototype, serial production of the Ba.65 began in 1936, with an initial production run of around 81 (MM 75091-75161) being produced by Breda. The second and the last production series was completed by July 1939. In the second series, Breda produced an additional 80 with an additional 57 built by Caproni. The total production run was 218 operational aircraft, in addition to the single prototype. Of the total produced, around 60 were sold to Iraq, Chile and Portugal.

Only one major modification to the original aircraft was ever made on the Ba.65, as it was used for only a short time.

  • Ba.65 – Prototype
  • Ba.65 K-14– Single and two seat versions
  • Ba.65 A.80 – Single and two seat versions
  • Ba.65 Trainer Version – Small numbers were used as training aircraft for a short time before being scrapped
  • Ba.65 P.XI – One aircraft was tested with the 1.000 hp Piaggio P.XI engine, but was not adopted for service.

Operators

  • Italy – Operated less than 160 Breda Ba.65 in total.
  • Iraq – Bought around 15 A.80 aircraft, of these two were modified as dual control trainers.
  • China –There were negotiations with Italy to domestically assemble thirty Ba.65s, but this was never achieved.
  • Fascist Spain – Used all surviving Ba.65s left by the Italians after the end of the Civil War.
  • Chile – Bought some 17 single-seaters and 3 dual control training version in 1938. These were powered by Piaggio P.XI engines and armed with 0.5 in (12.7 mm) Madsen type heavy machine guns.
  • Portugal – Bought 10 mostly two-seat versions, while some were equipped with the Breda M turret.

Breda Ba.65 A.80 Specifications

(Single Seat Version)

Wingspan 39 ft / 11.9 m
Height 10 ft 2 in / 3.10 m
Length 32 ft 4 in / 9.9 m
Wing Area 252.96 ft² / 23.50 m²
Engine One 1,000 hp (746 kW) Fiat A.80 RC.41 18-cylinder radial piston engine.
Empty Weight 5,510 lb / 2,500 kg
Maximum Takeoff Weight 6,950 lb / 3,150 kg
Fuel Capacity 650 + 370l
Maximum Speed 267 mph / 430 km/h
Cruising Speed 220 mph / 350 km/h
Range 340 mi / 550 km
Maximum Service Ceiling 20,670 ft / 6,300 m
Crew 1 Pilot
Armament
  • Two 0.5 in (12.7 mm) Breda-SAFAT heavy machine guns and two 0.311 in (7.7mm) Breda-SAFAT machine guns.
  • Four 110 lbs (50 kg) or 220 lbs (100 kg) bombs
  • 168 smaller 4 lb (2 kg) bombs
  • Additional two 220 lbs (100 kg) bombs carried under the wings

Gallery

Ba.65 during the Spanish Civil War
Ba.65 from 2° Stormo 1938
Ba.65 from 5° Stormo
Ba.65 from the 2° Stormo

Credits

  • Article by Marko P.
  • Edited by Stan L. & Ed J.
  • Illustrations by Pavel
  • D. Monday (1984, 2006), The Hamlyn Concise Guide To Axis Aircraft of World War II, Aerospace Publishing
  • G. Garello (1997), Breda Ba 65, La Bancarella Aeronautica – Torino
  • D. Nešić (2008) Naoružanje Drugog Svetsko Rata-Italija,, Tampoprint S.C.G. Beograd.
  • V.Kotelnikov (1995 ), Samoletuep Olya Boya Vtoroi Mirovoi, Library Moscow
  • Lennart A. (2008) A History Of Chinese Aviation Encyclopedia Of Aircraft And Aviation in China Until 1949, AHS of ROC.
  • J.W. Thompson (1963), Italian Civil And Military Aircraft 1930-1945. Aero Publishers
  • Vojislav V. M.(1998), Italijanska Avijacija U Jugoslaviji 1941-1943, Vojno istorijski institut Vojske Jugoslavije Beograd.
  • Nico S. (1979), Italian Aircraft Of The World War II, Squadron/Signal Publications.
  • Photos: http://www.warbirdphotographs.com/vvsregiaavions/regiaindex.html

Re.2005 “Sagittario”

Kingdom of Italy flag Kingdom of Italy (1941)
Fighter Aircraft – 32 ~ 48 Built

The Re.2005 was one of the better and more modern Italian WWII fighter designs. It was developed by Reggiane in 1941. Due to the lack of DB.605 engines, the development and production process of the aircraft was too slow and, by the time of the Italian surrender to the Allies, less than 50 had been built.

Re. 2005 Source: Pinterest

History

Officine Meccaniche Reggiane SA (hailing from Reggio Emilia in Northern Italy) was a WWI era aircraft manufacturer. However, following the First World War, it was not involved in any large aircraft production or design work. Rather as a company, it focused primarily on the Rail and Agriculture sectors primarily building locomotives and agricultural equipment. Its production efforts only returned to aircraft during the thirties when Reggiane became a subsidiary of the much larger Caproni aircraft manufacturer, which was led by the well-known Engineer Gianni Caproni. Thanks to this, Reggiane was aided by Caproni with a larger and more qualified aircraft design department. Reggiane and Caproni were involved with several experimental pre-war designs, like the Ca.405 Procellaria and P.32bis version, in addition to their license production of the S.M.79.

By 1941, the Italian Air Force was in a very desperate state, as it lacked an effective fighter design that could engage the increasing Allied bombing actions against Italian cities. The only modern design, the Macchi C.202, could not be produced in sufficient numbers to make a difference. For this reason, the Italian Air Force initiated the development of the so-called Serie 5 fighter designs that would eventually lead to the Fiat G.55, Macchi C.205, and the Reggiane Re.2005.

One of the greatest problems that the Italian aircraft designers and manufacturers had was the lack of sufficiently strong engines. In 1938, the development of a 1200 hp Fiat A.38 engine began, but many problems appeared and the engine could not be produced in time nor in any great numbers. For this reason, the license for the production of the German DB.601 was obtained. The problem was that Alfa Romeo’s, the manufacturer of this licensed engine, production output of this engine was only around 50 to 60 per month. Due to the lack of an adequate engine, Italian General Francesco Pricolo proposed creating new designs using the German 1475 hp DB.605 engine, which was to be produced by Fiat from 1942 on. The first planes chosen to be equipped with this engine were the Re.2001 and C.202. On 23rd July 1941, a decision was made to save the entire production of the DB.601 engine for the C.202. In addition, around 1000 new DB.605 engines were ordered to be produced by Fiat. Reggiane officials, seeing a new business opportunity, devoted all their available resources in the development of the new Re.2005 model.

The name

In various sources, this plane is marked by different but similar designations. These include RE 2005, Re 2005, or Re.2005. This article has and will use the Re.2005 designation. In early January 1943, the Re.2005 received its ‘Sagittario’ (name of the Constellation Archer) nickname, which is very well known today.

Re.2005 beginnings

In order to design the future Re.2005, a team was chosen under the leadership of Giuseppe Maraschini. His team decided that, instead of simply improving earlier models, they would design and build a brand new aircraft prototype. Carryovers from previous vehicles included the wings, which were similar to previous models but were made of a single piece. The armament was increased to two 0.5 in (12.7 mm) machine-guns and one 0.78 in (20 mm) cannon firing through the propeller hub, with two additional 0.5 in (12.7 mm) machine guns to be placed in the wings. A new outward retracting landing gear was to be installed. The radiators were placed under the fuselage. The building of the wooden fuselage mock-up was completed by the end of October 1941. The wings were completed by early November 1941. Preparation for the construction of two working prototypes (MM.494 and 495) began soon after.

However, there were delays due to the lack of promised DB.605 engines, that were not ready for license production yet. There was also a possibility that all future produced DB.605 engines would be delivered to Fiat and Macchi designs only. Despite these setbacks, the work on an operational prototype continued and, in February 1942, the factory was visited by the High Technical-Military Inspectorate commission. This commission gave good remarks for the Re.2005 design but asked to move the wing-mounted machine guns into the fuselage. As this would cause many technical problems and delays, nothing was done on this matter and the machine guns remained in the wings. By this time, the required shipments containing the armament (Mauser 0.78 in/20 mm MG 151 cannons), canopies, and windscreens (same as on the MC.205) were yet to arrive, as there were constant delays.

Once completed, the first test flight of the MM.494 prototype was made on 9th (or 7th, depending on the source) May 1942. For the main test, pilot Major Tullio De Pranto was hired by Reggiane, for the payment of 140.000 lire. This flight lasted around 5 minutes and was without problems. The following day, Major De Pranto made another flight with the MM.494 prototype. At first, it was fine but then the landing gear mechanism on the right leg broke down, which forced the pilot to make an emergency landing. The prototype was damaged but repaired and the flight tests continued during June and July 1942. By this time, over 6 hours of flight were achieved. In late July, the plane was transported to the Guidonia test center for further testing. There, during dive testing, a maximum speed of some 560 mph (900 km/h) was achieved. But there were again problems with the landing gear and also with the cockpit design and, for these reasons, it was returned to Reggiane for modifications. During August, modifications on the cockpit were made, mostly on the design of glass surfaces and the length of the windscreen, which was considered to be too long for the pilot. In September, the flight tests continued, but there were some issues with the engine malfunctioning and the MM.494 pilot was forced to make an emergency landing. By late September, many pilots had the opportunity to fly on the Re.2005 prototype.

The first prototype, MM.494, in preparation for a series of test flights. Source: Pinterest

At the start of October 1942, the second prototype was moved to the Guidonia test center for testing. There, the problem with the landing gear persisted, in addition to problems with fuselage vibrations that were also noted. By the end of October, the Re.2005 was used in a mock fight with the Fiat G.55. During the firing of its 0.78 in (20 mm) cannons, there were ammunition feed problems. For these reasons, in combination with the previous notes, the MM.495 prototype was returned to Reggiane for further modifications. In late December 1942, an Air Force Commission was formed to examine the Re.2005 prototype overall flying performance, armament, production speed, etc. The Re.2005 was noted to be inferior to the MC.205 but better than the Fiat G.55. While the final decision was not clear, the development of the Re.2005 continued on.

 

The second MM.495 prototype stationed at Reggio Emilia. Source: http://www.warbirdphotographs.com/vvsregiaavions/regiaindex.html

The next step in Re.2005 testing was the addition of bomb loads. During these tests, no major problem was recorded, but the take-off run was increased by some 657 ft (200 m) due to the extra weight. While piloted by Captain Enzo Sant’andrea, instead of releasing the 1410 lb (640 kg) bomb, the release harness mechanism failed and the bomb remained stuck to the plane. He was forced to land with the bomb, but luckily it did not explode and the landing was successful. Various tests were carried out with the original German engine and equipment from April to June 1943.

The Re.2005 prototype was used to supplement a mixed unit in the defense of Rome on 27th May 1943. During this flight, the Re.2005 was piloted by Lieutenant Giorgio Berolaso. While no enemy aircraft were detected, he managed to test the main armament. He later wrote, “ … It was a terrific experience! Such was the recoil that I had the impression that the entire aircraft slowed down…”.

Reggiane fights for production orders

In January 1942. Italian Air Force Officials decided to adopt the Macchi C.202, C.205, and the Fiat G.55 for mass production. The fate of the Re.2005 was, for some time, uncertain. Only in August 1942 did Reggiane receive orders to prepare machine tooling for the possible production of the Re.2005. In October, Reggiane petitioned for the production of 16 Series-0 Re.2005 aircraft. This petition was accepted by Italian Air Force officials and an order for 16 Series-0 (MM.092343-092358) planes was placed in November. Engineer Roberto Longhi was tasked with the construction of the first Series-0 aircraft. As numerous modifications were required, he immediately began working to improve the Re.2005’s performance. The fuselage skin was reinforced, along with the wing spar caps, skins, and internal structure.

As Engineer Roberto Longhi was working to improve the Re.2005, a special Air Force committee rejected it for serial production. Instead, the Re.2005’s improved wings were to be applied to the Re.2002 to serve either as an advanced fighter or as a fighter-bomber. It was also proposed to reequip the Re.2005 with the weaker DB.601 due to a lack of DB.605 engines. For some time, there were fierce discussions between Reggiane officials and the Italian Air Force about the Re.2005. The Reggiane officials even managed to involve Benito Mussolini in this discussion. Eventually, Reggiane managed to obtain a production order for 100 Re.2005 in January 1943, with an additional 18 of the Series-0. In late January 1943, it was increased to 600 aircraft with a monthly production of 70. In order to achieve such high production orders, other manufacturers were to be included in Re.2005 production, like Breda, Caproni, and Aerfer. Eventually, an order for 1000 aircraft was sent with Reggiane, but these numbers were never achieved due to a lack of engines and the war ending for the Italians.

When the production began in early March 1943, it was decided that, from the 24th produced plane onward, bomb racks would be added and the planes were to be used solely as fighter-bomber aircraft.

Technical characteristics

The Re.2005 was designed as a single-engined, low wing, all-metal fighter plane. The fuselage was made using a reinforced sheet metal construction covered with an aluminum alloy skin. The fuselage around the cockpit was additionally strengthened in case of a crash landing.

The landing gear had a simpler design than previous Reggiane designs. It consisted of two outward retracting wheels which were operated hydraulically. The rear tail wheel retracted into the fuselage and was enclosed by two small metal doors. The rear tail wheel could also be steered by the pilot if needed.

To speed up and ease production, the wings were made of one semi-elliptical piece. The wings were made using light alloy materials. They consisted of three double ‘T’ shape spars connected with sheet metal ribs. The split flaps made of metal were extended to under the fuselage. The ailerons (Frise type) were made using a combination of fabric and light alloy materials.

The cockpit had a canopy that could be opened to the right side. For better pilot protection, his seat was made using an 8 mm steel plate. The cockpit was provided with standard Italian equipment, like an Allocchio-Bacchini 30 radio, San Giorgio reflector collimator, Patin telecompass, etc.

Close lock of the Re.2005 cockpit interior. Source: http://www.warbirdphotographs.com/vvsregiaavions/regiaindex.html

The engine used was the German Daimler Benz DB.605A-1 1.475 hp that was being produced under license in Italy as the R.A.1050 RC.58 Tifone (Typhoon). A Piaggio P.2001 three-bladed, mechanically controlled metal propeller was used. The engine was placed in a specially designed mount that was connected to the rest of the fuselage. The Re.2005 oil radiators and coolant were placed on the sides.

The total fuel load was 580 l (or 536 l, depending on the source) stored in four fuel tanks placed in the wings. Access to the fuel tanks was done by removing metal plate panels held in place by screws. Three additional external fuel tanks could be added if needed, one larger with 240 l under the fuselage and two 100 l tanks under the wings.

For Italian standards, the Re.2005 was heavily armed with German supplied cannons. Its armament consisted of one 0.78 in (20 mm) MG 151 cannon firing through the propeller center and two 0.45 in (12.7 mm) Breda SAFAT machine-guns were placed in the front fuselage. Depending on the availability, two 0.45 in or two 0.78 in cannons could be placed in the wings. The total ammunition load was 550-600 (for all three) rounds for the cannon and 700 rounds for the two machine guns. Different bomb load combinations were tested, with a maximum load under the fuselage of 1410 lb (640 kg) and 350 lb (160 kg) under each wing.

 

The center of the propeller has an opening for the internal 0.78 in (20 mm) MG 151 cannon. Source: http://www.warbirdphotographs.com/vvsregiaavions/regiaindex.html

In Operational service

Due to the small number built, the Re.2005 saw only a limited number of actions with the Italian Air Force. All surviving Re.2005 were captured by the Germans, who put them to use. The last operator was the Aeronautica Nazionale Repubblicana, which had only a few Re.2005, but if any were ever used operationally is not known. There were attempts to sell the Re.2005 to Sweden, but nothing came from this.

In Italian Service

The delivery of the Re.2005 to operational units was slow, maximally up to four planes per month. The first unit to be supplied with this aircraft was the 362° Squadriglia which was part of the XXII Gruppo Caccia commanded by Captain Germano La Ferla. The first prototype, MM.494, was given to this unit in early 1943. At the start of April 1943, a group of 20 Italian fighters attacked an Allied B-24 bomber formation and managed to shoot down two bombers. One kill was credited to Re.2005. On 10th April, another attack on an Allied bomber formation was made and the Re.2005 again managed to shoot down one bomber. The next day, two more B-24 were shot down at the cost of one Re.2005. The pilot managed to survive using a parachute. On 28th April, another attack was made by a group of four Re.2005, eleven Macchi C.202 and one French captured D.520. In this action, the Re.2005 pilots shot down two more bombers. By this time, it was apparent to the pilots that the Re.2005 was far superior to the C.200 and C.202. The greatest strength of the Re.2005 was its strong firepower of up to three 0.78 in (20 mm) cannons. From May to June, there were several more flights but without any success.

A group of four Re.2005 belonging to the 362° Squadriglia. Source: http://www.warbirdphotographs.com/vvsregiaavions/regiaindex.html

The 362° Squadriglia was moved to Latina in June 1943. By this time, the 362° Squadriglia had only 8 Re.2005 with 7 operational. On 25th June, this position was attacked by Allied aircraft and four fighters were damaged.

In early July 1943, the 362° Squadriglia, with around 8 Re.2005, was relocated to Sicily in an attempt to stop the Allied advance. In the following days, the Re.2005 managed to shoot down several British Spitfires with the loss of a few aircraft. With the inevitable Axis defeat in Sicily, the Re.2005 crews were moved to Italy. The last two operational Re.2005 were lost in an air raid on the positions of the 371° Squadriglia to which they were temporarily attached.

This Re.2005 (MM.092352) was part of the 362° Squadriglia defending Rome in June 1943. Source: Pinterest

In mid-July, the 362° Squadriglia was operated from Naples with newly supplied Re.2005. By 20th July, this unit had only six Re.2005 but, in the following days two, were lost during bad landings, including the second prototype. Other units were also supplied with the Re.2005 but, in most cases, they were supplied in very limited numbers, for example to 369° Squadriglia. Through August, there were several unsuccessful flight attempts against Allied aircraft. A number of Re.2005 were lost either to Allied action or to other circumstances. By early September, due to the Italian surrender, all available Re.2005 stationed in Naples were destroyed by their crews.

The maximum number of Re.2005 ever operated by 363° Squadriglia was around 9 operational planes. By the time of the Italian surrender, in total, 19 Re.2005 were supplied for operational use to front line pilots. During the period in which XXII Gruppo Caccia was equipped with the Re.2005, it claimed to have shot down some 24 enemy aircraft, with 17 more labeled as possible. In addition, 8 to 13 aircraft were reported to be damaged by this unit. The total losses of Re.2005 amounted to 12 planes, with the deaths of 3 pilots and 4 wounded. While in service, the Re.2005 landing gear proved to be problematic and thus the ground repair crews made several field modifications in order to solve this problem.

The Re.2005 had the best firepower of nearly all Italian fighter designs. With its three 0.78 in (20 mm) cannons, its pilots managed to shoot down many Allied planes during its short operational life. Source. Wiki

In German hands

After the Italian defeat, the Germans rushed to capture any available military equipment and factories they could find. This included the Reggiane factory, along with all surviving Re.2005 in September 1943. Once in German hands, 8 Re.2005 that were under construction were completed. The Germans seemed to be satisfied with its performance and allocated them to the Luftwaffe Luftdienst Kommando Italien in October 1943. At the start of 1944, two additional Re.2005 were completed and given to the Luftwaffe.

The Germans were impressed with the Re.2005’s performance and put to use any surviving aircraft they could find. Source: http://xoomer.virgilio.it/f5avipatches/re2005%20page.html

The use of the Re.2005 by Germans is somewhat confusing, as some authors suggest that they were used in defense of Berlin up to the war’s end ( like D. Mondey). Author M. Di Terlizzi mentions that the MM.495 prototype along with MM.096105 were sent to Germany for evaluation, but what their fate was is not known. Author G. Punka even writes that the second prototype was used in defense of Bucharest. Both cases seem highly unlikely if we take into account the cost of transport, lack of spare parts which would force it to operate close to the Reggiane factory, and the small numbers of captured planes. Even if the Re.2005 were repositioned to defend Berlin, they would have made no difference due to the small number built.
In an Allied bombing raid in March 1944, three Re.2005 were lost. From March to June 1944, three more were damaged, mostly due to accidents, and were returned to Reggiane for repair. By the end of July, five Re.2005 were still operational and used by the Fliger Ziel Staffel 20. This unit was active from June to December 1944. The final fate of the German-operated Re.2005 is not clear but, by the end of 1944, all were probably lost.

Aeronautica Nazionale Repubblicana

The Aeronautica Nazionale Repubblicana had two operational Re.2005 captured at Castiglione del Lago in October 1943. It is highly unlikely that they ever saw any operational service.

Offer to Sweden

In 1942, the Chief of the Caproni commercial company (Compagnia Commerciale) made an attempt to sell the license and 50 incomplete airframes to Sweden. His offer was based on the fact that Italy had sold older Re.2000 and that Sweden had obtained a license for the production of the German DB.605 engine. By the time the Air Ministry and Mussolini allowed this arrangement, in June 1943, it was too late and the whole deal was never achieved.

Proposals and modifications

During the Re.2005’s development process, there were few attempts to overcome the problem of the lack of an adequate engine. Other different modifications were also tested, but with little to no success.

Re.2005 SF/R

In late November 1942, there were proposals to mount an additional jet engine on the Re.2005 which could help it reach a speed up to 466 mph (750 km/h), at least in theory. Due to the extra weight of some 1000 lb (310 kg) and complications with the installation, no Re.2005 was ever fitted with this engine. This proposal is often marked by Re.2005 SF, after the names of the main proponents of this project, Marcello Sarracino and Antonio Ferri. It is also marked simply as Re.2005 R, Reazione (Reaction), by some sources.

Re.2005 wooden version

Luigi Nardi made a proposal to build the Re.2005 aircraft using mostly wood. This would make the production of Re.2005 cheaper. Nardi was involved in building the first wooden wings in March, following with a fuselage in June 1943. Reggiane officials hired Nardi in late 1942 ( officially in early 1943) and gave him a team of 39 men to complete a wooden model. Little to no progress was made by 1943 and, in the end, it appears that no working prototype was ever built.

Twin fuselage Re.2005 version

There was a paper proposal in late 1942 to build a twin-fuselage heavy fighter version of the Re.2005. It was to be powered by two DB.605 engines and the pilot was to be positioned in the left fuselage. This project remains on paper only and no mock-up or working model was ever built. In 1943, Nardi proposed a similar all-wood project, but nothing came of this. If these two projects were related, it is not known. It is unknown if this version received any official designation.

Re.2005 aircraft carrier version

Due to Reggiane’s experience with shipboard aircraft designs, the Re.2005 was chosen to be used for the Aquila aircraft carrier. No progress was ever made for this version and, in the end, nothing came from it.

Re.2004

Due to the lack of DB.605 engines and the priority given to the G.55 and C.205 aircraft, Italian Air Force officials proposed in late 1941 that Reggiane adopt another solution. This included the use of the new Isotta Fraschini Zeta 1.250 hp engine still in development. This new aircraft project was named Re.2004. The development process of the Re.2004 was slow and, by late June 1943, only two prototypes were ordered to be built. The main engine was never successfully completed nor used due to huge problems with the cooling system. It is likely that only wooden mock-ups were ever built of the Re.2004. Some authors, like John F.B, note that the Re.2004 was actually based on the Reggiane Re.2001 fighter design.

Re.2006

In March 1943, the Italians managed to obtain a number of German 1750 hp DB.603 engines. Immediately, there were plans to equip the existing fighter designs with this engine, including the Re.2005. In May 1943, the Italian Air Force ordered Reggiane to construct two new prototypes (MM.540-541) using this engine. By the time of the Italian surrender, only one incomplete (or complete, depending on the source) prototype was built. After the Germans captured the Reggiane factory, they continued work on the Re.2006 by using some components taken from the Re.2005 (the fuselage). The work on it was never finished by the Germans. It was captured by the Allies, who showed no interest in it, and the incomplete Re.2006 was scrapped in April 1946.

Production

Despite promising performance and an official production order for more than 740 aircraft, only small numbers were actually ever built. The number of production aircraft depends on the sources: According to author Christ C. 37 were built, while D. Mondey and Nešić, D claim 48 being built.
Author John F.B. gives information that 2 prototypes, 16 Series-0 and 18 pre-production aircraft were built, in total 36. Author Gregory A. notes that, by September 1943, 32 Re.2005 were built. These include 2 prototypes, 29 Series-0 and a single Series-I aircraft. He also notes that an additional one was under construction but never finished.

  • Re.2005 Prototype – two prototypes (MM.494 and 495) built
  • Re.2005 Series-0 – 16 to 29 were built and used for testing and in combat.
  • Re.2005 Series-I – 1 to 18 built with some structural modifications.

Proposals and modifications

  • Re.2005 SF – Proposed version equipped with an extra jet engine, none built.
  • Re.2005 wooden version – Proposed version to be built using wood, only limited progress made.
  • Twin fuselage Re.2005 – Paper project only.
  • Re.2005 carrier version – Proposed version to be used on the Aquila aircraft carrier, no prototype was ever built.
  • Re.2004 – Experimental fighter project equipped with the Isotta Fraschini Zeta 1.250 hp engine, possibly only a mock-up built.
  • Re.2006 – Proposed fighter plane powered with Daimler Benz DB 603 and to be built using Re.2005 components, only one incomplete model built.

Operators
Italian Regia Aeronautica – Operated less than 22 aircraft during the war.
Aeronautica Nazionale Repubblicana – Operated two Re.2005.
Germany – Rebuild 10 Re.2005 which were used by the Luftwaffe.
Sweden – There were proposals to negotiate a deal with Sweden for license production. Nothing came from this.

Surviving Re.2005

One Re.2005 captured in Sicily was allegedly put on display in the American National Aircraft Show in November 1946. There is little to no evidence that proves that this ever happened. Today, only a part of a Re.2005 is the rear fuselage and tail of  MM.092352362-2,  restored by GAVS Milan. It can be seen at the Gianni Caproni Museum of Aeronautics near Milan.

Conclusion

While the Re.2005 had the potential to be a good fighter design, its development process was plagued by the lack of engines, problems with vibrations, and the indifference of the Italian Air Force officials. While it was used in combat, it was built in small numbers and too late to have any influence on the war.

Re.2005 Specifications

Wingspans 36 ft 1 in / 11 m
Length 28 ft 7 in / 8,7 m
Height 10 ft 4 in / 3.15 m
Wing Area 220 ft² / 20.4 m²
Engine One Fiat R.A.1050 RC.58 12-cylinder 1475 hp engine
Empty Weight 5732 lbs / 2.600 kg
Maximum Takeoff Weight 7.960 lbs / 3.610 kg
Fuel Capacity 580 + 440 l
Climb to 8 km (19,700 ft) 7 minutes 50 seconds
Maximum Speed 390 mph / 630 km/h
Cruising speed 319 mph / 515 km/h
Range 776 mile / 1.250 km
Maximum Service Ceiling 39.370 ft / 12,000 m
Crew 1 pilot
Armament
  • Three 0.78 in (20 mm) cannons and two 0.5 in (12.7 mm) heavy machine guns
  • One 1,410 lb (630 kg) bomb, and two 252 lb (160 kg)

Gallery

Re. 2005, Illustration by Pavel Alexe

Source:

  • D. Nešić. (2008). Naoružanje Drugog Svetsko Rata-Italija. Beograd.
  • D. Mondey (2006). The Hamlyn Concise Guide To Axis Aircraft OF World War II, Bounty Books.
  • G. Punka, Reggiane Fighters In Action. Signal Publication.
  • J. W. Thomson (1963) Italian Civil And Military Aircraft 1930-1945, Aero Publisher
  • G. Alegi. (2001) Reggiane RE 2005, SATE Zingonia.
  • M. Di Terlizzi (2001) Reggiane RE 2005 Sagittario, IBN Editore
  • John F.B. (1972) Caproni Reggiane Re 2001 Falco II, Re 2002 Ariete and Re 2005
  • Sagittario, Profile Publications
  • N. Sgarlato (1979) Italian Aircraft OF World War II, Squadron Signal Publication.
  • C. Dunning (1998) Courage Alone The Italian Air Force 1940-1943, Hikoki Publication

Reggiane Re.2000 Falco

Kingdom of Italy flag Kingdom of Italy (1937)
Fighter Aircraft – 158 ~ 170 Built

The Falco being prepared for a shipboard catapult test launch [Colorized by Michael Jucan]
The Re.2000 was one of many Italian pre-war fighter aircraft developments. Despite having overall decent flying performance, it was never adopted for Italian service. It did see export success, to Sweden and Hungary.

History

The prototype, MM 408, in its natural metal finish. [Rod’s Warbirds]
Officine Meccaniche Reggiane SA (Reggio Emilia in Northern Italy) was a WWI-era aircraft manufacturer. However, after the war, the Reggiane was not involved in any aircraft production or design work. Things started moving only during the thirties, when Reggiane became a subsidiary of the much larger Società de Agostini e Caproni and Società Caproni e Comitti aircraft manufacturer, which was led by well-known Engineer Gianni Caproni. Thanks to him, Reggiane was provided by Caproni with a larger and well qualified aircraft design department. Reggiane and Caproni were involved in several experimental pre-war designs, like the Ca.405 Procellaria and P.32bis, in addition to the licence production of the S.M.79 bomber.

In 1938, the development of the Re.2000 began at the request of the Italian Aviation Ministry (Ministero dell Aeronautica) under the codename “Programme R”, which aimed to upgrade the Italian Air Force (Regia Aeronautica) with new and modern designs. Special care was given to the development of new single wing fighter designs. At that time, several different fighter designs were in various states of development (like the Fiat G.50, Caproni-Vizzola F.5, Macchi C.200 etc.). The Reggiane officials wanted to participate in this, and ordered the design team to begin developing a fighter plane.

The similarities in external design between the Italian and American aircraft are easy to see. [UH.edu]
A team was formed, led by the Technical Director Antonio Alessio and Engineer Roberto Longhi, who immediately began work on the new design. Due to a lack of time to properly design the new fighter, a solution was proposed to simply buy a licence from the Americans, but this was rejected by chief Ing. Caproni. The new design was, surprisingly, soon finished. This was achieved by utilizing some elements of design of an American Seversky P-35 aircraft. The main reason why the Re.2000 was influenced by the American design was Roberto Longhi. He had spent some time working in the aviation industry in America before returning to Italy in 1936. While the two planes look very similar, there were some differences, like the cockpit, landing gear etc.

Technical Characteristics

Re.2000 rear view. [Rod’s Warbirds]
The Re.2000 was designed as a low wing, mixed construction (mostly metal), single seat fighter plane. The fuselage consisted of a round frame covered with metal sheet held in place by using flush-riveting. The Re.2000 wings had a semi-elliptical design, with five spars covered with stressed skin. The central part of the wing held two integral fuel tanks. The front position had a capacity of 455 l (120 US gallons), while the smaller rear one could hold around 240 l (63 US gallons). The wings were equipped with fabric covered Frise type ailerons. The rear tail had a metal construction with the controls covered with fabric.

The landing gear system was unusual. When it retracted, it rotated 90° (a copy from the Curtiss model) before it entered the wheel bays. For better landing handling, the landing gear was provided with hydraulic shock absorbers and pneumatic brakes. The smaller rear wheel was also retractable and could be steered if needed.

Two Italian Re.2000, possibly stationed in Sicily. [Rod’s Warbirds]
The Re.2000 engine was the Piaggio P.XI R.C.40 14-cylinder air cooled radial engine, a licensed derivative of the French Gnome-Rhône Mistral Major 14K, providing 985 hp (840 hp depending on the source), equipped with a three blade variable pitch propeller made by Piaggio.

The cockpit canopy opened to the rear and the pilot had a good overall view of the surroundings. For pilot protection, a rear 8 mm (0.3 in) thick armor plate was placed behind the seat. The pilot was provided with an oxygen tank and a type B.30 radio. The Re.2000 had an option for installing wing gun-cameras, but this was rarely done.

Re.2000 (MM 5068) first series side view. This aircraft was one of the few used by the Italian Air Force. [Rod’s Warbirds]
The Re.2000 possessed weak offensive capabilities, as it was armed with only two Breda-Safat 12.7 mm (0.5 in) heavy machine guns. The machine guns were placed above the front fuselage and fired through the propeller arc. For each machine gun, 300 ammunition rounds were provided. The machine guns could, depending on the combat situation (lack of ammunition, for example), be fired together or individually. There were plans to add two more machine guns (unknown caliber) to the wings but nothing came of this.

The Re.2000 also had two small bomb bays placed in each central wing section. Each bomb bay had a payload of twenty two 2 kg (4.4 lb) anti-personnel or incendiary bombs. The bombs were electrically released individually or in larger groups.

Tense Start

The Re.2000 dashboard. [Rod’s Warbirds]
The first operational Re.2000 prototype (serial number MM.408) was completed in early 1939. It made its first test flight on 24th March (or May, depending on the source) that year, piloted by Caproni test pilot Mario De Bernardi. During this flight, the Re.2000 was shown to have good flying speed and manoeuvrability. There were some modifications requested, like changes in the design of the exhaust and carburettor air intakes. The cockpit design was also requested to be changed from a round windshield to a framed model. These flight tests were followed by armament tests, which also were without any major problems. During this time, the Re.2000 was tested in mock dog-fights against the Italian Macchi C.200 and even a German Me-109E. In these mock fights, the Re.2000 proved to have better handling and maneuverability than its counterparts.

In August 1939, the prototype was moved to the Air Force Guidonia test site near Rome for further testing. The Re.2000 was flight tested by two pilots, Colonels Aldo Quarantotti and Angelo Tondi, who both gave positive remarks on its performance. Maximum speed achieved during these test flights was 515 km/h (320 mph).

Re.2000 side view [Rod’s Warbirds]
Further tests done by the Aeronautical Construction of the Air Ministry, on the other hand, stressed the important structural problems that this plane had. The main issue was the position of the fuel tanks in the wings, which was dangerous for a fighter plane. There was another huge issue with fuel tank leaks due to loosening of the rivets. The low quality of the welding and a number of internal structural defects were also noted. Despite still being in a prototype stage, meaning that these defects could possibly have been addressed, the Re.2000 program was abandoned.

Despite the proposal of the Re.2000 main designers Alessio and Longhi to redesign the fuel tanks and improve the structure of their prototype, the decision for the cancellation of the project was not changed. The small serial production of 12 planes was rejected and the preparation of the tooling equipment for the production of the originally planned 188 aircraft was abandoned.

Strangely, for some unknown reason ,the Aviation Ministry gave permission for the construction of a second prototype (MM.454). Later, this prototype would serve as a base of the Re.2002 aircraft design.

Success Abroad

While the Re.2000 proved to have good flying performance, it was difficult to maintain properly due to the harsh weather conditions in Swedish service. [Rod’s Warbirds]
Despite not being adopted for service, the Aviation Ministry did actually include the Re.2000 for the export market, where it did see some success. Even though the Reggiane lost the order for the Re.2000 serial production, their management decided to go on with production as a private venture. The idea was that, if its own Air Force did not want to adopt it, maybe another country would. Many Nations in Europe would show interest in this design, which included Hungary, Yugoslavia, Spain, Switzerland, UK, Finland and Sweden. In the end, due to the war’s outbreak, only Hungary and Sweden would receive the Re.2000.

Negotiations with the UK

In late 1939, the UK sent a delegation led by Lord Hardwick and Wing Commander H. Thornton to Caproni. The British were interested in buying a number of aircraft designs (Ca.313 and Ca.311), including 300 Re.2000. The order was confirmed in January 1940. What is interesting is that, initially, the Germans did not try to prevent these negotiations. Later, in March, the Germans tried to enforce an embargo on the Italian sale of weapons to the UK. Caproni and Lord Wardwick tried to bypass this embargo by making a deal through a Caproni Portugese subsidiary. But, as Italy attacked the French in June 1940, the negotiations between Italy and the UK were stopped.

In Swedish Service, the “J 20”

The Re.2000 was known in Sweedish service as the J-20 model. [WW2 in Color]
Sweden negotiated with Reggiane to buy a group of 60 Re.2000 aircraft. After some initial negotiations, the deal was made on the 28th November 1940. The price of these 60 aircraft was 18.7 million Swedish Krona, but was instead paid in much needed chrome-nickel metal (of the same value) instead. The 60 Re.2000 were broken into parts and sent by train through Germany and then again re-assembled at Malmen. In Swedish service, the Re.2000 was known as the J 20. While it proved to have good flying performance, due to the harsh weather conditions, it was difficult to maintain properly. During the war, the J 20 were mostly used to patrol the Swedish skies and occasionally intercept German or Allied aircraft. Only one was lost, when it was shot down by a German Do 24 in April 1945. Due to a lack of spare parts, all were removed from service in 1946. One surviving J 20 can be seen in the Swedish Air Force Museum in Linköping.

In Hungarian service, the “Héja”

A Hungarian Heja II is preparing to take a test flight on an airfield near Budapest.

For some time, Hungary acquired aircraft and aviation equipment from Italy (like the CR.32 and CR.42, for example). By the end of 1939, Hungary asked for 70 new Re.2000 in addition to the licence rights for domestic production. Once the deal was completed, the production of the Re.2000 was given to well known manufacturer MAVAG, but the start of the production process was slow. On the other hand, the 70 Italian-produced Re.2000 arrived by the end of 1941. The first Hungarian-produced Héja (Hawk, as the Re.2000 was known in Hungary) was only built and tested in 1942. By the time production stopped, in 1944 around 185-203 aircraft of this type were built.

Re.2000 in Hungarian service. The Italians supplied the Hungarians with 70 aircraft and a production license. [Rod’s Warbirds]
During their Hungarian service, the Héja’s engine was deemed insufficient, and so a new, 14-cylinder WMK-14B 1085 hp engine was used. The heavy machine guns were also replaced with Hungarian Gebauer ones of the same caliber.

The Héja were used on the Easter front with some success, managing to achieve a number of air victories. As a shipment of more advanced Me-109G arrived in Hungary from Germany in late 1943, the Héja was mostly relegated to training. But, due to the rapid Soviet advance in 1944, many were put back into frontline service in the vain hope of stopping the enemy.

Negotiation with Yugoslavia

In early 1940, the Kingdom of Yugoslavia sent an Air Force delegation led by Colonel Pavlović to negotiate an order for 50 Re.2000 aircraft. After a brief demonstration, the delegation was impressed with its performance. In March, a new delegation led by Colonel Rubčića, with two test pilots, was sent to personally test the Re.2000’s performance. In July, Yugoslavia requested a delivery of six Re.2000 aircraft without armament. Due to the outbreak of the war, none were ever delivered to Yugoslavia.

A New Chance in Italian service

The Re.2000 would see some limited service in the Italian Air Force and Navy. Due to an urgent need for modern aircraft, the Italians simply reused 28 aircraft (the numbers are different depending on the source used) which were originally intended for Hungary (20) and Sweden (8). An additional 28 aircraft were built to replace the ones requisitioned, and supplied to the respective buyers.

Shipboard Version

Re.2000 preparing to be launched from a ship catapult. Despite the testing being successful, none were ever used operationally in this role due to rapid war developments in favor of the Allies. [Rod’s Warbirds]
When Italy declared War on the Western Allies, their navy had only a small number of 44 Ro.43 and few Ro.44 floatplanes available. Thus, the Italian Navy finally showed interest in the Re.2000 as a replacement for the older models. For this reason, a Re.2000 was to be modified with catapult mounting points, so that it could be launched by ship catapults. These were piloted not by navy pilots, but instead by the Air Force. Two Re.2000 that were modified for this purpose and were lost in accidents. The first (MM.471), piloted by Cap. Giovanni Fabbri, was lost during the flight to Taranto and the second (MM.485) was damaged during transport.

The first catapult tests were carried out in late 1941 near Perugia, by Giulio Reiner. More intensive tests were carried out in early 1942 on the Italian battleships Roma and Vittorio Veneto. These tests were considered a great success and an order was placed for 10 Re.2000 to be modified for this role.

These Re.2000 saw some modifications, like the removal of the covering behind the sliding canopy in hope of improving rear visibility, a modified windshield was added, new radio and modifications to the fuselage so that it could be launched from ship catapults.

When the testing was completed, the Re.2000 were given to the 1° Squadriglia FF.NN (Forze Navali – Naval force). Two each were given to the battleships Roma, Vittorio Veneto and Littorio. Due to the rapid development of the War in the Medeterain, the Italian navy was no longer able to effectively battle the Allied navy. These Re.2000 were never used operationally on any Italian ships in its intended role. By the time of the Italian surrender (September 1943), these battleships tried to escape to the Allied side but were attacked by the German bombers, and only one Re.2000 (from the Vittorio Veneto) survived the engagement.

Depending on the source, this version was powered by a stronger 1025 hp P.XIbis engine. The Re.2000 design for the shipboard is marked as Series II. In addition, some authors (like Maurizio D.T.) name this version as Re.2000Bis.

The Re.2000 G.A. Long Range Version

The flow of supplies to the Italian colony of Ethiopia with much needed modern weapons and equipment was constantly harassed by the British navy and aviation. One of the problems for the Italians was the lack of proper fighter cover. They attempted to send S.M.82 transport planes carrying parts for CR.42 biplanes. While these attempts did see some success, a proper solution was needed. The best Italian fighter at that time was the Macchi C.200, but it lacked the needed operational range to reach this front. Someone in the Italian Air Force proposed to modify some already produced models with increased fuel load. The Italian Navy (Regia Marina) also showed interest in this project, as they were desperate to replace the aging Ro.43 and Ro.44 aircraft (carried by larger shipps for various missions). For this proposal, the Re.2000 was chosen, despite not being adopted for service.

The prototype of the Re.2000 design for longer operational range was named “G.A” (Grande Autonomia, long range). The Re.2000 G.A had an increased fuel load to 1490 l, which increased the operational range from 840 km (520 miles) to 1.300 km (807 miles). This aircraft was tested by the famous Italian Ace Col. Adriano Mantelli. The flight proved to be successful and without any problems. Despite these results, the loss of Ethiopia to the Allies in May 1941 stopped the long range fighter project.

Re.2000 of the 74° Squadriglia. [Rod’s Warbirds]
The modified Re.2000 aircraft were allocated to the 23° Gruppo Autonomo (independent group) in the spring of 1941. The 23° Gruppo Autonomo consisted of the 70° ,74° and 75° Squadriglia. This unit was stationed at Sicily under the leadership of Major Tito Falconi. As this unit had only a small number of Re.2000, it was reinforced with older CR.42.

To better test the Re.2000 G.A. version’s performance, a special experimental section (Sezione Sperimentale), a part of the 23° Gruppo Autonomo, was formed. This Section was led by Capt. Pietro Calistri. For some time, this unit had a nonoperational status, as the Re.2000 had engine problems and could not be used. As the engine problems were solved, the Re.2000 were mainly used for patrolling the Italian coast, but in a few cases even for bombing British military installations on Malta. The Re.2000 were moved to support the 377° Squadriglia in July (or August depending on the source). At that time, the 377° Squadriglia had around 13 (or up to 17) Re.2000. This unit was stationed at the Trapani Milo airfield in Sicily. From that point, this unit was mostly used for patrol and escort missions in the Mediterranean sea.

The 23° Gruppo Autonomo was, for a very short time, even used in North Africa, but without any Re.2000. In early 1942, the unit was engaged in naval escort and reconnaissance operations, but no enemy fighters were encountered. From March 1942, this unit, under the command of Capt. Marcolini, operated from Palermo in Sicily. Its objective was to protect Palermo from any possible enemy bombing attacks and to scout for enemy ships and aircraft. During one such mission, one British Blenheim bomber was shot down, which may be the only Re.2000 air victory in Italian service.

The 377° Squadriglia was engaged in supporting the Italian attacks on British convoy ships near Malta in June 1942. During this action, no victory was achieved and no losses were recorded. After more than 320 operational missions, the Re.2000 were replaced with Macchi C.200 aircraft in September 1942. The remaining Re.2000s were in such poor repair condition that it was decided to return them to the Reggiane factory. After some were repaired, they were then moved to Treviso to be used as training aircraft, but no flights were ever made. After the Italian surrender, the Germans took over these aircraft, but they were likely scrapped, as there is no record of their use by the Germans.

Future Developments

During the war, the Re.2000 would see some improvement attempts by using a new engine and improving the overall design. There were several such projects, including the Re.2001, Re.2002, Re.2003, Re.2004 and Re.2005.

Re.2001

In the hope of improving the Re.2000’s overall flight performance, in 1939 and 1940, one plane was equipped with a German Daimler Benz DB 601 engine. While it improved the performance, Alfa Romeo was unable to produce large numbers of this engine and, for this reason, only 252 were built. They were used in different roles: fighter, ground attack, shipboard and torpedo attack plane.

Re.2002

The Re.2002 was a fighter-bomber version which incorporated design elements from the Re.2000 and Re.2001. It received two additional light machine guns, bomb racks under the fuselage and under the wings. It was powered by a 1175 hp Piaggio P.XIX R.C.45 engine. Small numbers were produced for the Italians by 1943. The German captured the Reggiane factory and produced additional aircraft.

Re.2003

One Re.2000 was used as a base for the experimental two-seat Re.2003 version. After some testing and an initial order for 200 planes, it was not adopted for service.

Production

Despite being canceled for mass production, Reggiane decided on its own initiative to produce a series of 158 to 170 (depending on the source) aircraft for export sales. Most of these would be sold to Hungary and Sweden. Small numbers (less than 30, including the prototypes) did eventually enter limited service with the Italian navy.

  • Re.2000 Prototype – two prototypes built
  • I Series – Main production version
  • II Series- Shipborne fighter/scout version
  • III Series – Long range version

Prototypes and modifications

  • Re.2001 – Improved version powered with German Daimler Benz DB 601 engine, 252 were built.
  • Re.2002 – Powered with 1175 hp Piaggio P.XIX R.C.45 engine, 225 were built.
  • Re.2003 – Experimental two-seater, one prototype built.

Operators

  • Italy – Operated less than 40 aircraft
  • Hungary – Bought 70 aircraft and a licence production for the Re.2000 under the ‘Héja’ name. Total domestic production was 185-192 aircraft
  • Sweden – Bought 60 aircraft in 1940.
  • UK – Negotiated buying 300 aircraft, but the war prevented this from happening.
  • Other countries like Yugoslavia, Finland, Spain and Switzerland showed interest in buying a number Re.2000, but nothing came from this.

Surviving Re.2000

The remains of the recovered Re.2000 [Warbird News]
Two Re.2000 wrecks were recovered from the bottom of Mediterranean. One shipboard Re.2000 (MM.8287) wreckage was found by the Italian company Micoperi. It was lost in a reconnaissance flight during April 1943. What is interesting is that this plane was modified as an experimental two seater according to author Maurizio D. T. The wreckage was, after a proper desalination process, transported to the Museum of the Italian Air Force at Vigna Di Valle. This plane is currently under restoration. Another Re.2000 (MM.8281) was also recovered in late April 2012.

Conclusion

The Re.2000 had good flying performance but it did have a number of issues. The greatest one was the engine, which demanded a lot of maintenance. There were many problems with the engine overheating. While the larger forward mounted engine did provide the pilot with additional protection from enemy fire, it also affected the pilot’s front view, which was limited. The two heavy machine guns proved to be insufficient and problematic. The biggest issue was the poor quality of the fuel tanks, a problem that was never solved successfully, which was the main reason why it was never adopted for service.

Re.2000 Specifications

Wingspans 36 ft 1 in / 11 m
Length 26 ft 5 in / 8 m
Height 10 ft 4 in / 3.15 m
Wing Area 220 ft² / 20.4 m²
Engine One Piaggio P.XI RC.40 985 hp
Empty Weight 5424 lbs / 2.460 kg
Maximum Takeoff Weight 7143 lbs / 3.240 kg
Fuel Capacity 675 l (180 US gallons)
Climb to 6 km (19,700 ft) 6 minutes 10 seconds
Maximum Speed 320 mph / 515 km/h
Cruising speed 280 mph / 450 km/h
Range 522 mile / 840 km
Maximum Service Ceiling 34.450 ft / 11,500 m
Crew 1 pilot
Armament
  • Two 0.5 in (12.7 mm) heavy machine guns
  • Bomb bay with twenty two 4.4 lb (2 kg) bombs.

Gallery

Illustrations by Pavel

Italian Re.2000 used during catapult launch testings
A Hungarian V.4+V.40 Héja I belonging to the Dongo (Wasp) Fighter Squadron
Swedish J 20 (Re.2000) with 42 marking number

Credits

 

Fiat G.50 Freccia

Kingdom of Italy flag Kingdom of Italy (1935)
Fighter Plane – 774 to 791  Built

Freccia in Italian service. Colorization by Michael Jucan [monochrome-watches.com]
During the thirties, Fiat Aviazione was one of the most advanced aircraft manufacturers in Europe. With the advent of new technology at the time, it was obvious that the next stage in the development of the aircraft industry, especially in military aviation, would be centered around all-metal monoplanes. Fiat’s Chief Designer, Ing. C. Rosatelli, had been designing mixed-construction biplanes and even an all-metal bomber. As the demand for a modern, all-metal fighter plane was high, Fiat officials made a decision to hire a young aircraft engineer named Giuseppe Gabrielli, who would later design the Freccia, the first operational Italian all-metal fighter.

Giuseppe Gabrielli’s Work

The history of the Fiat G.50 began in 1931, when Fiat formed a new Aircraft Technical Bureau – Department 2 (Ufficio Tecnico Aviazione – Divisione II). The main purpose of this bureau was designing and building brand new types of modern all-metal planes. The same year, a young Italian engineer, Giuseppe Gabrielli, was hired by Fiat Chairman Senator Angelli to work for the Technical Bureau. Giuseppe Gabrielli had gained some experience in aircraft design while working for Piaggio. When he moved to Fiat, he immediately began working on several non-military aircraft projects. All of his projects were marked by the capital letter ‘G’, his initial. First was the G.2, an all-metal, three-engined plane, then the G.8 biplane trainer, and later the twin-engine passenger plane G.18.

During the thirties, the Italian Ministry of Aviation (Ministero dell Aeronautica) was interested in adopting a new, all-metal monoplane fighter and ground attack aircraft for the Italian Air Force. Some specifications for their request were: to use one radial engine, armed with at least two 0.5 in (12.7 mm) heavy machine guns with at least 300 rounds of ammunition and one 0.7 in (20 mm) gun or 1.45 in (37 mm) gun, and provisions for bombs on the ground attacker. A request was sent out to all domestic aircraft manufacturers. There were several proposals in response, but only the G.50 and the Macchi C.200 would be chosen for production. The others were either rejected (Ro.51 and A.U.T. 18) or built in limited numbers, like the Caproni F.5.

In order to solve the problem of the lack of an adequate fighter design, Fiat officials even considered the acquisition of a license to produce the American Seversky SEV-3, but nothing came of this. In April of 1935, Giuseppe Gabrielli began working on a new low-wing, all-metal plane named G.50. According to his first plans and drawings, it was to be armed with two machine guns, powered by a 550 hp radial engine (with a diameter of 39 in/1 m), weigh around 3,395 lbs (1,540 kg), and equipped with a retractable landing gear. At the same time, Fiat was testing a new FIAT A 74 RC 38 14-cylinder radial piston engine, so it was logical that Giuseppe Gabrielli decided to use it for his work. The A 74, in principle, was a direct copy of the American Pratt & Whitney R-1830 Twin Wasp which powered a large number of US planes, including the Douglas C-47, Consolidated PBY Catalina, Douglas TBD Devastator and Grumman F4F Wildcat. The expected speed of the G.50 with this new engine was around 285 mph (460 km/h) at 11,500 ft (3,500 m).

G.50 prototype (MM.334) during its first test flights. [airwar.ru]
On 28th September, 1935, Gabrielli submitted his project to the Ministry of Aviation. Military officials were impressed by the design, but ask for some modifications. These included a wingspan of 36 ft 1 in (11 m), a weight of 4,870 lbs (2,210 kg) and a maximum speed of 280 mph (452 km/h). The offensive armament was changed to two 0.5 in (12.7 mm) heavy machine guns located in the fuselage with an additional two 0.3 in (7.7 mm) machine guns placed in the wings. In addition, the G.50 was designed to carrying a bomb load of 220 lbs (100 kg) or, if needed, extra fuel tanks with 23.5 gal (90 l) capacity.

In January 1936, the Ministry of Aviation changed its original request, choosing instead to focus only on the fighter role. The Ministry of Aviation wanted to accelerate the development of the new fighter, and the proposed ground attack role was rejected. Because of this, the bomb load was deemed no longer necessary, and the main armament was reduced to only two 0.5 in (12.7 mm) machine guns with 150 rounds each. The most important requirement was that the new fighter should have the best possible flying performance.

Despite these changes, the Fiat officials decided to proceed with the G.50 project. As Fiat’s production capacities were overburdened, work on this new project was instead moved to the CMASA works at Marina di Pisa, part of Fiat since 1931. Giuseppe Gabrielli was finishing his last drawings and the list of needed materials and equipment in June 1936. In his final drawings, the armament was reduced to two heavy machine guns without the bomb load, and the plane would be powered by the new A 74 c/n engine.

The production of the first operational prototype was scheduled to begin in late summer of 1936. The prototype was finally ready at the beginning of 1937 and was transported to the city of Turin for further testing. This prototype, under registration number MM 334, made its first test flight on 26th February, 1937. The pilot was Giovanniego De Briganti, the CMASA test pilot. During initial testing, the pilot noted several faults and possible problems with the G.50. He especially pointed out the strong vibrations during flight and the aircraft’s tendency to spin.

On 22nd June, 1937, the G.50 prototype was moved to Marina di Pisa for more testing and modifications. After these modifications were completed, the prototype was sent to the Regia Aeronautica (Italian Air Force) experimental flight center near Rome. There, the G.50 prototype was tested by several army pilots. They noted that the controls were hard to work with at high speeds and a lack of climbing ability. Before the final order for mass production, Giuseppe Gabrielli was asked to solve these problems. For this reason, another prototype was made, designated MM 335.

The second prototype made its first flight on 20th October, 1937. After a series of successful flying tests, an accident occurred. On the 11th (or 8th, depending on the source) November, 1937, while flying the second prototype at high speed, the test pilot Briganti lost control of his aircraft and crashed to the ground. He did not survive the crash. His place was taken by the new chief test pilot, Enzio Guerra.

A G.50 from the 20th Group, front-side view. [wwiivehicles.com]
A combination of the accident and inferior performance that did not meet expectations, along with better overall performance of the Macchi C.200 threatened to shut down the G.50 project. But as the CMASA works were already in process of producing a series of 45 G.50’s, it was deemed a waste of resources to abandon or scrap the tooling equipment needed to produced the G.50 that had already been produced. A second reason for keeping the project running was the fact that it would take too much time for Fiat to prepare for the production of the Macchi C.200. The Air Ministry decided to go on with G.50 production, but insisted that the company correct the shortcomings of the plane by the time of production. Of the 45 ordered, the first 11 were used for many more trials. Two planes, MM 3357 and 335, the salvaged and rebuilt prototype, were sent to the experimental centre in Rome. Seven were stationed at the Pisa S.Giusto airfield and tested there. Two more ,MM 3570 and 3571, were tested by pilots Guerra, Rolandi and Cus. These trials were held in Turin and the main purpose was to investigate possible changes to the design of the G.50. The preliminary tests showed that the fully enclosed cockpit had to be changed before production, and a new design was necessary. This enclosed cockpit had several drawbacks which pilots often complained about. The closed cockpit was hard to open (especially in emergency situations), was made of poor quality plexiglass which was prone to cracking, offered poor visibility and sometimes exhaust fumes accumulated in the cockpit so the pilots were forced to fly with an open cockpit. After some testing and modifications, it was decided to used a partially enclosed cockpit. This solution was not perfect and was uncomfortable for pilots. Despite this, it was decided that all future planes would be built with an open cockpit only. More modification that were deemed necessary were the installation of a new start-up system, a better undercarriage locking system and adding a new oxygen mask for piloting at high altitude.

The G.50 was first showed to the public in October of 1937 at the International Aeronautical Show held in Milan. From 1937 to 1940, when the production was changed to the improved version, some 224 G.50 were built.

Technical Characteristics

A G.50 flying alongside a German Bf-110, possibly during the Battle of Britain [Wiki]
The G.50 Freccia, Italian for Arrow, was a single-seat, low-wing, all-metal fighter plane. The main fuselage was made from four angular shaped longerons with 17 metal frames. The wing construction consisted of a center section which was made of a steel tube connected to the lower fuselage and two metal spars connected with ribs. The four flaps were hydraulically actuated and at certain speeds they would automatically retract to their closed position. The fuselage, wing, and tail were covered with duralumin sheets. The only fabric-covered parts were the movable control surfaces in the wings and the tail.

This G.50 belonged to the 20th Group, transferred from Belgium to North Africa. [ea51.org]
The engine was placed in a tubular shaped mount made of chrome-molybdenum steel that was connected to the fuselage by four bolts. The engine and the cockpit were separated by a fireproof screen in order to protect the pilot from any possible fire outbreak, either due to engine malfunction or damage. The plane was powered by the 840 hp (626 kW) Fiat A 74 RC 38, 14 cylinder radial piston engine. With this engine, the G.50 could reach a maximum speed of 293 mph (470 km/h), with an effective range of 276 mi (445 km) and a service ceiling of 35,000 ft (10,700 m). An all-metal three-blade propeller produced by Fiat was used. One of major disadvantages of using a radial type of engine was the massive drag due to its large cross-section. In order for ground repair crews to have easy access to the engine and the fuselage interior, several access doors were added. The maximum fuel capacity was 83.5 gal (316 l.) There were two fuel tanks located in the wings 11.9 gal each (45 l) and two more in the fuselage, one larger with 26.4 gal (100 l) and a smaller one with 18 gal (68 l) with an additional auxiliary tank 13.75 gal (52 l) also located in the fuselage.

The first G.50 series had an enclosed cockpit design but as this created many issues, it was later changed to an open cockpit. Despite its disadvantages, the enclosed cockpit had an excellent rear view. Many different open cockpit designs were tested before the final design was chosen. The later version with the open cockpit had two smalls door installed to help entering or exiting the plane. The seat was adjustable, so it could be adapted to the pilot’s needs.

In front of the pilot, the dashboard was divided into three sections. On the upper section were the navigation instruments, reflector sight, fuel indicators and engine instruments. The middle section had the ammunition counter, warning lights, the position of the landing gear, compass and oxygen control panel. The lower section had the engine starter, cowling controls and compressed-air system indicator. The radio in the pilot’s cabin was the ARC 1, but the quality of the batteries was poor. A fire extinguisher system was also provided. There was also the possibility of installing one OMI FM62 camera gun.

The G.50 was equipped, like most modern aircraft of the time, with inward retracting landing gear, but the rear tail wheel was fixed. In the G.50 bis version, the rear tail wheel was changed to a retractable type. The landing gear could, if necessary, be manually operated. At first, it was of a Messier type, but it was later replaced with a Magnaghi design. The retracting landing gear was hydraulically operated, and pneumatically during lowering. In case both systems did not work for any reason, it could be manually operated. For easier and more pleasant landing, hydraulic shock absorbers were provided for both telescoping legs.

The main armament consisted of two forward-firing 0.5 in (12.7mm) Breda-SAFAT heavy machine guns, with some 150 rounds of ammunition for each machine gun. The guns were placed behind the engine top and both were synchronised in order not to damage the propeller. It is interesting to note that this gun used oil lubricant for faster firing and thus a lubricant tank was added on top of the engine. Some G.50 planes were armed with bomb racks and used in North Africa.

An Italian armourer rearming a Regia Aeronautica Fiat G.50 with ammunition gun belts at an airfield in Sardinia in June 1942. Source: reddit.com

Modifications and Prototypes

As the war progressed, the Italians realized that they were lacking planes to fulfill the different necessary roles such as fast ground attack or training. In order to save time, the most obvious solution was to try to modify existing models instead of developing new ones. The G.50 would be modified in several ways, some of which demanded major changes to the plane’s design, while others were just minor variations, like the added sand filter for the G.50 S.A.

Trainer G.50 B

The Fiat G.50 B version with the longer cockpit design for the instructor and the student. [alieuomini.it]
As the G.50 was entering production and the first operational units were formed, a trainer was needed for new pilots. As most army pilots were accustomed to flying older biplanes, retraining them for flying the monoplanes was required. For this purpose, in late 1936 the Italian Air Ministry placed an order for Fiat to developed a two seat dual control plane based on the G.50. After the mock-up was built and inspected in March 1938, it was deemed sufficient for production. By April, an order for the first prototype was placed. But due to the constant changes to the design, the production of the first prototype was frequently delayed. It was not until June 1939 when the final design with an enclosed cockpit was chosen. The plane was named G.50 B. The capital ‘B’ stands for ‘bipost,’ the Italian word for two-seater. This version was recognizable by its long glazed canopy with the rear cockpit being open from the top. The first prototype, marked 3615, would be ready in late April 1940 when it was tested by Enzio Guerra.

After only a few test flights, it was deemed adequate and was put into production. The first ten were built in 1940, with the last one built in 1943. In total, some 108 (or 100, depending on the source) G.50 B trainers were built during the war. Production by years was: 10 in 1940, 82 in 1941, 11 in 1942 and 5 in 1943.

The first series of G.50 planes produced had an enclosed cockpit design, but this was later replaced with a semi-open design. [warbirdphotographs]
The G.50 B was, in essence, a modified single-seat version with a new cockpit and dual controls. The front part of the cockpit was fully enclosed in contrast with the rear which was open. The main armament was removed on the G.50 B. This version was very successful, as it was easy to build and offered almost the same flying performance as the single-seat version.

These were used mostly by the Regia Aeronautica Fighter Schools. Smaller numbers were operated as liaison planes or even in some front based fighter units. After the Italian capitulation, small numbers, possible 20 or more, were used by the National Republican Air Force. At least one was given to the Croatian puppet state in the Balkans. The last G.50 B were used by the Flying School in Lecce for a few years after the war, up to 1948.

The Improved G.50 bis

The final decision for the mass production of the G.50 fighter was not based on its performance, but instead on the fact that CMASA had already begun producing it. The performance of the G.50 was poor compared to the Macchi C.200. In order to justify the production, the Italian Air Force requested that Fiat to improve the G.50’s overall performance. The sought modifications were adding extra fuel tanks, increasing capacity from 83.5 gal (316 l) to around 108.3 gal (410 l), redesigning the rear fuselage and the vertical tail surfaces, better glazing of the cockpit to protect the pilot from air turbulence, the addition of armor plates behind the pilot seat, and the tailwheel to be made retractable. The original ARC 1 radio, with its poor quality batteries, was only changed in October 1941 with the R.B.30.

The new improved version was designated the G.50 bis. According to Italian original plans, the first planes should have been ready by late 1938, but this was never achieved. The whole process was slow and the first aircraft was tested on 13th (or 9th) of September 1940 at Turin. As the main engine was not changed, despite the other modifications, the general flying performance was almost the same. The only improvements were easier maintenance and increased operational range. As these tests were completed, an order for production was given. From 1940 to 1943, around 439 of these versions were built by CMASA and Fiat.

G.50 S.A Ground Attacker

A G.50 somewhere in Africa, where it saw extensive combat action, in many cases as a improvised ground attack plane. [asisbiz]
A certain number of planes that were serving in North Africa were modified by adding sand filters and a bomb rack. The landing gear was also modified for easier landing.

G.50 A Ground Attacker

The G.50 A was designed to be used as a fighter-bomber on the “Aquila” aircraft-carrier which was under construction. For this modification, the G.50 B two seater version was reused. The main offensive armament was to be increased to four 0.5 in (12.7 mm) machine guns. The problem was that the wing design did not allow the installation of the new weapons directly in the wings. The solution was to increase a part of the central section of the wings in order to accommodate these guns. Additional bomb racks were also to be added. One prototype, serial number MM 8595, was built and tested in October 1942. The whole concept proved to be problematic and the project was abandoned. The prototype would be used up to 1943 in testing new wing designs. In some sources, this model is designated as G.50 A/N.

G.50 bis “Tuffo” Dive Bomber

This was a dive bomber version designed in 1941 and 42, possibly inspired by the famous German Ju-87 “Stuka.” A bomb load of up to 990 lbs (450 kg) was planned, with two 200 lbs (100 kg) bombs placed under the wings and one 550 lbs (250 kg) under the main fuselage. For this modification, the addition of dive brakes were necessary. There is no information about prototype construction, but there is a great chance that it was never made.

G.50 B Naval Observer

One plane (MM 6548) was rebuilt for a naval observation role in 1943. It had a larger tail, different wing sections, a camera and an arrestor hook for use on an aircraft carrier. It was also equipped with a B 30T transmitter, B.G.42 direction finder and a A.R.18 receiver. Only one was built, possibly because of the impending Italian capitulation.

G.50 O/R

This version was based on the G.50 bis and the only difference was the installation of a arrestor hook for aircraft carrier use. Around 16 planes were modified for this role and were in use by the 155th Group Autonomo, mostly for training, in 1943.

Other Projects

Beside these, there were some minor projects that were proposed, but the majority if not all of them were not implemented. On the base of the G.50 B some project were proposed like the: night fighter, land reconnaissance or even a floatplane fighter (G.50 Idro).

Prototypes based on the G.50

During the war, in order to improve the flying performance of the G.50, many new designs and weapon loads and engines were tested.

G.50 ter

This was a further development of the canceled G.52 project. The new project, designated the ‘G.50 ter,’ was to be equipped with the same 1000 hp (746 kW) Fiat A 76 engine as the G.52. Even before production of a prototype, the new engine was found to have a number of flaws. The first prototype powered by the new engine was ready by late July 1941. First flying tests were carried out at the Aeritalia airfield, with the plane being piloted by Agostini. During these flight tests, the engine proved to be mechanically unreliable and it could not reach expected performance. More test were held in November 1941, but in the end the project was canceled and only one plane was built.

G.50 V

The G.50 V prototype, powered by a new German engine. Even though this design solved the aerodynamic problems, it was never put into production. [Pinterest]
In late 1939, the Italian Ministry of Aviation made a decision to begin negotiations with the German Daimler-Benz company for a production license of the newest liquid cooled DB 601A engine (1035 hp). It had a much lower frontal area and had much better aerodynamics than the larger Italian radial engines. The license was eventually obtained and Alfa Romeo was put in charge of the production of this engine, but it was never built in any great numbers.

In early 1940, the Italian Ministry of Aviation asked Fiat to build a modified version of the G.50 using this new engine. Two prototypes were to be built by CMASA, and these were marked as G.50 V (the ‘V’ stand for Veloce, which means fast). The first prototype, serial number MM 479, was built and tested in late August 1941 by the test pilot Ezio Guerra. Immediately, the new design proved to have some issues, such as an inefficient engine cooling system and the controls being difficult to operate. By the end of 1941, most these problems were solved and a new series of tests was scheduled.

In December 1941, more extensive flight tests were carried out by test pilot Valentino Cus in order to determine the precise flight performance, in particular the maximum speeds at various heights and the climbing rate. Maximum speed achieved was some 360 mph (580 km/h), and a maximum altitude of 16,400 ft (5,000 m) was reached in 5 minutes and 30 seconds. Mostly due to the introduction of the new FIAT G.55 and the lack of DB 601 engines, the G.50 V project abandoned.

G.51

In 1940, it was proposed to equip one G.50 with the new A 75 R engine. Nothing came of this project.

G.52

Information about this version differs significantly depending on the source.

According to Piero Vergnano, Fiat worked on improving the performance of the A 74 engine used on the G.50 for quite some time. This lead to the development of the new 1000 hp (746 kW) Fiat A 76 engine. In 1938, Fiat suggested the installation of this engine in the G.50 to the Air Ministry. At first, the request was accepted and an order for two prototypes was placed. By late 1939, the project was canceled due to the acquisition of new German DB 601A engines, and no prototypes were ever built. According to Gianni Cattaneo, the G.52 was in fact just a further development of the G.50 V. Due to the appearance of the new G.55 fighter, this project was abandoned.

G.53

This proposal was a combination of the G.50 B powered by the DB 601A engine. It was developed in 1941. It was intended to be used as a fast reconnaissance plane, but the Air Ministry never showed any interest in this proposal and nothing came of it.

First Operational Units

As CMASA began producing the first G.50 planes in late 1938, an experimental military fighter unit was formed for further testing and training. This unit was located at the Ciampino airfield near Rome. The unit was named Gruppo Sperimentale da Caccia (Experimental Fighter Unit/Group). Command of this new unit was given to Major Mario Bonzano, at that time a famous pilot ace from the Spanish Civil War (flying the CR.32 biplane). Pilot training on this new plane lasted until January 1939, when the Italian Air Force High Command decided to send a unit of 12 planes to Spain for real combat testing.

In Spain

A group of 12 new G.50 fighters arrived in January 1939 in Spain, having been transported by sea. This unit was based at Escalona Airport, some 43.5 mi (70 km) from the capital of Madrid. Starting in March, this unit carried out flight patrols and fighter cover missions for bombers at altitudes between 24,600 to 26,240 ft (7,500 to 8,000 m). By that time, the opposing air force had been almost destroyed and air to air combat was rare. The only combat action that was recorded happened when a lone Soviet-built I-16, possibly flown by a Canadian pilot by the name of Dickinson, was intercepted by a G.50. The Italian aircraft was damaged and the pilot was forced to land. None of the 12 G.50 that were sent were lost in combat during the Spanish Civil War. At the end of this war, 11 operational G.50 fighters were given to the new Spanish fascist regime. These planes were used by the 27 Gruppo Caza (Fighter Group). After 1943, they were sent to Spanish Morocco, to be used by the 2. Regimento Mixto (mixed regiment) together with several German supplied He-112B.

A small number of G.50 fighters were used in the Spanish Civil War. Their combat operations were minimal and all were gifted to the new Spanish state. [Wiki]
After his return to Italy, Major Bonzano made his report of the effectiveness of the G.50. According to him, the G.50 had good maneuverability, effective armament and was easy to operate at altitude. On the other hand, he pointed out that the visibility was poor and the landing gear construction was weak and prone to malfunctioning. His conclusion about the effectiveness of the main armament would prove to have a great negative impact for the G.50 in the future.

In Finnish Service

Finnish G.50 on the airfield. [ww2aircraft.net]
Because of the likelihood of a Soviet attack in 1939, the Finnish government and Army wanted to equip their forces with modern equipment and weapons. As a result, a Finnish military delegation visited Turin in 1939, where the new G.50 fighters were being tested. The delegation was impressed with the aircraft’s performance, so they placed an order for 35 brand new G.50. Most of the planes sold were of the first series produced by CMASA, with serial numbers 3599 to 3614. These were supplemented by planes from the second productions series (serial numbers 4722 to 4750).

A very interesting fact is the maximum speed achieved by Finnish pilot Tapani Harmaja. As he was testing the flying performance of the G.50 at an airfield near Latina, he managed to reach a speed of 515 mph (830 km/h). He achieved this by diving from a high altitude of 11,480 ft (3,500 m) down to 1,310 ft (400 m). This was the fastest speed reached by any aircraft in Italy at that time.

Due to the outbreak of the Second World War in Europe, the transportation of the purchased aircraft was slow and complicated. The planes were disassembled and then transported by train through Italy to the north of Germany and then by ship to Sweden, and from there to Finland. As they were transported in parts, the assembly was done at Gothenburg. When they were completed, the pilots were instructed to fly them to their new stations. The first 14 G.50’s were received in February 1940 and the last in June 1940. While flying en route to their designated airfields, two planes were lost in accidents in February 1940.

The G.50 arrived too late to have any large impact on the Winter War (30 Nov. 1939 to 13 Mar. 1940) but they saw some combat during this period. The first G.50 planes were equipped with the 26th Fighter Wing (Lentolaivue 26 or just simply LeLv or HLeLv) located at Haukkajarvi. They were used to replace the older Gloster Gladiators used by this unit. By 13 March, the Finnish pilots flying the G.50 claimed to have shot down 11 Soviet planes. There is some disagreement between the sources, authors Gianni C. and David M. states that this unit did not participate in the Winter War.

Finland operated 35 G.50s during the war. Most saw extensive service during the Continuation War when, despite their obsolescence, they proved to be effective in the hands of Finnish pilots. [Wiki]
Until the German and Finnish attack on the Soviet Union in June 1941, known in Finland as The Continuation War, Finnish technicians and engineers tried to improve the performance of the G.50 fighters. Most Finnish G.50s were from the first series, equipped with the enclosed cockpit. This design was not popular with the Finnish pilots and was replaced with an open cockpit. The vertical stabilizer and rudders were replaced with improved ones. Also, the Finnish tested snow skis taken from Fokker D.XXI’s, for the G.50 allowing them to better land on on frozen airstrips.

At the start of the German invasion of the Soviet Union in 1941, Finland joined the war with a much larger air force than it had in the previous conflict. LeLv 26 was stationed at an airfield near Utti, and was charged with the protection of the area around Lake Ladoga where they saw most of the action they were involved in. The G.50 proved to be an effective fighter in the hands of Finnish pilots. On 25th June 1941, six Finnish G.50 fighters managed to shoot down 10 Soviet bombers with no losses. Later in August, pilots from LeLv 26 managed to shoot down nine Soviet fighters. The most famous Finnish pilot was Oiva Tuominen, who had a total of 23 (33 or 43 according to different sources) air victories, with around 15 while flying the G.50. For his service, he was awarded the Mannerheim Cross, the highest Finnish military medal at the time. By the war’s end, LeLv 26 had around 88 air victories with the loss of 11 G.50s. Only two were shot down by Soviet planes, one was lost to AA fire, and eight more were lost either to accidents or mechanical failures. The Finnish G.50s remained in use up to June 1944, when they were moved to the rear for second-line duties. By the end of the war, there were still some 22 (the exact numbers are not known) operational G.50 fighters and they were used up to 1947.

In Italian Service

Fiat G-50 “1-3” of the 1 Experimental Group in Escalona, in March 1939

According to the Italian military program codenamed “R” (Programme R), the Italian Air Force was to be heavily reinforced with many new units and more modern aircraft designs. With the existing G.50 fighter, it was planned to form and equip one Stormo (Stormo-regiment) and one Fighter Wing/Group (Gruppo).

The first unit to receive the new G.50s was 51° Stormo located at the Ciampino airport near Rome, in November 1939. This regiment consisted of the 20th Group, with 351st, 352nd and 353rd Squadrons, and the 21st Group, with 354th, 355th and 356th Squadrons. Almost all of the squadrons were equipped with the newer G.50 with the open cockpit, and only the 351st Squadron was equipped with the first series with the enclosed cockpits. To more effectively train both experienced and new pilots, military war game exercises were often held by the Italian Army. During one of these games the 51° Stormo would earn its military emblem, a black cat with a green mouse. During one exercises, a group of different fighter planes were tasked with intercepting a group of S.M.79 bombers, marked with the green mouse emblem. The older CR.32 biplane could not fulfill this task, but the new G.50 from the 352nd Squadron accomplished this without any problem. From that point on, the pilots from 51° Stormo began painting the emblem on their planes.

Quite soon, the order was given to form a second unit, 52° Stormo. It consisted of the 22nd Group (357th, 358th and 359th Squadrons) and the 24th Group (360th, 361st and 362nd Squadrons). The 24th Group was equipped with older FIAT CR.32 planes that were soon to be replaced with G.50’s. 52° Stormo operated from two airports, Pontendera and Sarzana. Both of these groups had around 100 brand new G.50s.

Western Front

By the time Italy entered the War in the West, there were some 118 G.50 planes on hand, with 97 operational, and some 21 were ready for delivery to designated units. In an attempt to profit from the fast Allied defeat in Western Europe, Italy declared war on France on the 10th of June 1940. Most G.50s saw some limited action, mostly covering SM.79 bombers during their attack on Corsica on 15th and 16th June. Subsequent attacks followed on 17th and 19th June. The center of operations then moved to the north, in the French Alps on 21st June. Due to a lack of proper training, the G.50 pilots had problems adapting to this type of aircraft, as most of them had flown only on the older biplanes. The G.50 proved to have good flying performance at low speeds, but was hard to control at high altitudes and higher speeds.

Battle for Britain

In order to support the German air raids on Great Britain, a special unit (Corpo Aereo Italiano C.A.I) was formed in late 1940 and was sent to Belgium. For this operation, the 20th Group, with 45-48 G.50’s, was selected under the command of Col. Bonzano. Despite the original planes being planned to reach their base of operations in Belgium by September 1940, this was delayed until October 1940. This delay occurred mostly due to bad weather. During the transfer from Italy to Belgium, two G.50’s were lost to accidents. The first combat actions were carried out in late October 1940, and were mostly bomber support missions. Similar missions were planned for 11th November against Great Yarmount, but they were canceled due to bad weather. From November 1940 to January 1941, the G.50 flew on many surveillance missions but there was no contact with enemy planes. By the end of January 1941, most Italian Air Force units returned home, with the exception of the 20th Group.

The C.A.I had great technical problems during this operation. The G.50 was designed for the Mediterranean rather than the cold climate of the North, and there were problems with freezing and defective instruments, unreliable batteries and fuel problems.

By April 1941, the remaining units were ordered to return to Italy. Missions conducted against Britain were unsuccessful and they did not go well for the Italian pilots, as they did not win any air victories. Italy had lost more than six aircraft with two dead pilots. This operation was a strategic failure for the Italian Air Force, mostly due to poor planning, adverse weather conditions and inefficiency of the planes used.

In the Balkans

Mussolini ordered an invasion of Greece in October 1940. For that purpose, fewer than 80 G.50 fighters based in Southern Italy (33) and occupied Albania (43) were used. Initially, because of the lack Greek air resistance, the G.50 were used as ground attack planes. But, after the arrival of the British forces in November, the first air battles started. Due to the fact that the Italian pilots had some experience during the Spanish Civil War, they managed to achieve some successes against the British. The G.50’s main opponent was the Gloster Gladiator, which had poorer flying performance in comparison. Later, however, more modern Hurricanes appeared, which were much more advanced than the G.50.

During the war in Greece, there were a number of engagements between the British and the Italian Air Forces. During one dogfight on 20th February 1941, some 10, possibly even 12, British planes were shot down in a single engagement by a group of 22 G.50s. The Italians only lost one plane. However, during the same day, British Hurricanes managed to shoot down four G.50s in a different engagement. On the 28th of February 1941, some 12 British planes were shot down at the loss of 27 Italian aircraft. In one unusual case, a collision took place between a G.50 and a Gladiator. Because of the heavy damage, the Gladiator crashed to the ground, while the pilot of the G.50, despite the damage received, managed to fly about 123 mi (200 km) back to his home base and safely land. Due to significant disagreements among sources, there is no accurate data on the losses of both sides. As the G.50 proved to be inferior to the Hurricane, they were gradually replaced with the more advanced Macchi C.200 planes.

During the attack on Yugoslavia, the so-called “April War” in April 1941, the G.50 were used in escort missions. There were very few air battles and, by 17th April, the war was over.

In the Mediterranean and North Africa

During the North African campaign, the first G.50s were stationed near Tripoli by the end of 1940 and early 1941. The first units to operate in Africa were the 151st, 152nd and 358th Squadrons with around 76 to 80 planes. Even before these units saw any action, there were great problems with the maintenance of these planes due to sand. Taking into account that North Africa is dominated by the Sahara desert, it is very strange that the Italian military leaders did not take into account the fact that the desert sand could affect the plane’s engine. Since a certain number of planes were taken out of action by this, the demand for special sand filters was high. There were also problems with the sand getting into the landing gear which caused issues. To solve these problems, the Air Ministry urged CMASA and Aeritalia to provide adequate sand filters and modify the landing gear. The G.50 planes modified in such a way were marked as G.50 A.S (A.S standing for Africa Sahariana).

The G.50 saw heavy fighting in North Africa. Depending on the combat situation, it was used in a standard fighter role, for ground attack, defence missions, or for bomber escort. As the war progressed, the G.50 was mostly used in a ground attack role by equipping them with a 220 lbs (100 kg) bomb load to increase its offensive armament. For this purpose, 50° Stormo was formed. 50° Stormo mostly operated around the Sidi Barrani sector, where it attained some success against the British P-40 and Hurricanes. The pilot Bovoli (from 50° Stormo) shot down six British Blenheim bombers in July 1941.

During 1941 and early 1942, despite reinforcements, G.50 losses were increasing. At the beginning of 1941 there were only 20 planes operational, but with reinforcements the number increased to 80 in October and then fell down to 35 in December 1941. Most planes were lost not in air combat but instead during enemy ground and air attacks on airfields, as well as accidents. For example, the 20th group suffered heavy losses when 18 G.50 were destroyed as British armored forces attacked the airfield at Martubi on 19th November 1941. By the end of 1941, the only unit operating the G.50 was the 12th Group stationed at Tripoli. By 1942, most G.50 fighters were either lost or replaced with more modern Macchi C.200 and C.202. The surviving G.50s were relocated to second line airfields in Sardinia (24th Group), Greece (151 Group) and in the Aegean (154th Group). By the time of the Axis defeat in Africa (1943), only the 358th Squadron was still using the G.50.

Despite having poorer flying performance than its main opponents, the P-40 and the Hurricane, the G.50 proved to be a formidable plane in the right hands. The G.50 also proved capable in its new role as a ground attack plane, in which it destroyed a large number of enemy planes on the ground.

The Last Stand

The 20th Group’s emblem, a black cat hunting green mice. [ea51.org]
After late 1942, the remaining G.50 fighters that were stationed in Italy serving as trainers and for second line operations. After the defeat in Northern Africa, the Italian army was in disarray and the rapid Allied landing in Sicily in July of 1943 worsened the situation. Many surviving G.50s were used to equip the 158th and 159th Groups. These two groups suffered heavy losses attacking strong Allied positions in Sicily. In a period of only a few days, the two groups ceased to exist.

After Sicily, the Allies landed on the Italian mainland and, on 8th September 1943, Italy capitulated. By that time, there were only around 40 to 48 G.50 airplanes still in service, of which only 17 were operational. A small number of G.50 were used by the new National Republican Air Force (Aeronautica Nazionale Repubblicana/ANR) in Northern Italy until the end of WW2 as second line and training planes. A few were even used by the Italian Co-Belligerent Air Force (Aviazione Cobelligerante Italiana, or ACI) in the southern part of Italy, which had switched over to the Allied side.

In NDH Service

In the middle of 1942, in exchange for raw resources and materials, Italy delivered 10 G.50 (9 single seat and one two-seat trainer) airplanes to the NDH, the independent state of Croatia Air Force (reg. number 3501-3510). These were not newly produced planes, but instead G.50s that returned from the front and were repaired. The planes that were supplied were used alongside French-built MS.406 fighters supplied by the Germans. In 1944, six more airplanes were obtained from Italy, now under German control (reg. number 5686, 5965 and 06186, the rest are unknown) bringing the total number used to around 16 planes, possibly more as the exact numbers are not known. According to Tihomir T. and Darko Č. NDH forces acquired three G.50, after the withdrawal of Italian forces in 1943.

Their participation in the war was negligible and they saw little if any action. On 15th September 1944, only 7 were reported, with none fully operational for service. There were several cases of desertion among Croatian pilots while flying the G.50. On 2nd September 1944, pilot Andrija Arapović escaped to the island of Vis, under the control of the Yugoslav communist Partisans. A second pilot flying a G.50 fled to the Allies stationed in Italy.

Partisan forces put the captured G.50 to use during the war and it would remain in service up to 1946. An interesting fact about Andrija Arapović’s G.50 aircraft (reg. number 3505) is that it still exists today and can be seen in the Belgrade Military Aviation museum near the airport “Nikola Tesla” in Serbia. This is the only surviving example of a G.50 in the whole world, but it is in very bad condition and has been under restoration for years. By the end of the war, the Yugoslav Partisans had captured almost all of the surviving G.50s in Croatian service, but their use was limited due to a lack of spare parts.

G.50 production attempts in China

Italians were for some time trying to negotiate with Chinese authorities about opening an aviation production factory in China. After initial negotiations in June 1934, the Chinese signed a contract with the Aeronautico Italiano per la China (Aerocina). This company was owned by the Italian Government in conjunction with Caproni, Breda, Fiat and SIAI. According to this contract, the Italians were to build the SINAW (Sino-Italian National Aircraft Works) factory in Nanchang. With this agreement, the Italians were to provide tools and machines necessary for the factory to work. The head of the soon-to-be factory was the Italian Luigi Acampora and the Director was General Chu Lin. The production of the first operational aircraft was to begin from July 1937 on and all Italian personnel were to return to Italy after five years of cooperation.

The SINAW officially started production in November 1936 with six Savoia-Marchetti SM.81B bombers. Future plans included production of 30 Breda Ba.65s and 50 Fiat G.50s. The factory was slightly damaged during the Japanese bombing of Nanchang on the 20th October 1937. By November the Italian Government made a decision to discontinue any further cooperation and stopped all future deliveries of equipment and materials. This was done mostly due to Japanese military actions and the poor cooperation of the Chinese. By early December 1937, all Italian personnel returned home, and the deal with the Chinese was abandoned without a single G.50 being built.

Production and Variants

Besides the few prototype planes, a total of 791 (source Piero V.) G.50 and its variants were built during the war. Other authors give different numbers, according to Chris B. some 774 were produced and author Gianni C. quotes the figure of 778 planes. Author Duško N. give a figure of 788 planes.

The production of the G.50 fighter began in 1937 and ended in 1940, with a total 244 planes. The production totals by years were: two prototypes in 1937, 14 planes in 1938, 75 in 1939 and 153 in 1940. The improved G.50 bis was produced from 1940 to 1943 with a total of 439 planes built (421 according to some sources). 71 planes were built in 1940, some 253 in 1941, 113 in 1942 and the last 2 were built in 1943. If we compare these production numbers with other modern fighters of the time, the G.50 was built in relatively small numbers. The G.50 and its modifications and prototypes were produced by CMASA and Fiat during the war.

Conclusion

The Fiat G.50 was the first Italian all-metal fighter plane to enter operational service in significant numbers. In the early stages of the war, it proved to be an effective fighter, but as the war progressed, it became obvious that it was outdated in comparison with other modern fighters like the Hurricane. The G.50 was easy to control at lower speeds and had good maneuverability. The negative side was the lack of engine power and the overall design of the radial engine which affected the aerodynamics of the G.50. There were problems with cockpit visibility, but the most notorious issue was the lack of effective offensive armament, which consisted of only two heavy machine guns. Despite all this, with a good pilot the G.50 proved that it could be an effective fighter and it was responsible of downing of a significant number of Allied planes during the war.

  • G.50 prototype – Two prototypes built, the second was lost in an accident.
  • G.50 – Production aircraft.
  • G.50 bis – Improved version.
  • G.50 A.S – A number of G.50 planes that were used in North Africa were modified with sand filters and improved landing gear.
  • G.50 A – One plane was modified with an increased offensive armament of four 12.7 mm machine guns in October 1942. Only one was constructed and used up to 1943 for testing different wing designs.
  • G.50 B – Two-seat trainer version, around 100 to 108 built.
  • G.50 bis “Tuffo”– Dive bomber version, none built.
  • G.50 B naval observation – One G.50 was modified to be used by the Italian Navy in 1943.
  • G.50 O/R – Based on the G.50 bis, some 16 were built and used for training in 1943.

Prototypes:

  • G.50 ter – Equipped with a stronger 1000 hp (746 kW) FIAT A.76 engine, only one built.
  • G.51– In 1940, it was proposed to equip one G.50 with the new A 75 R.C.53 engine, none built.
  • G.52 – Proposed project, none built.
  • G.50 V– Equipped with a German Daimler-Benz DB 601 engine, one built.
  • G.53 – Proposed project based on the G.50 B and powered by the DB 601, none built.

Operators

  • Kingdom of Italy – Operated around 720 G.50 aircraft, starting from the Spanish Civil War until the Italian Armistice.
  • Croatia (NDH) – Used at least 16 G.50 aircraft during the war (supplied by the Italians and Germans).
  • Finland – Operated 35 G.50’s during the Winter War and the Continuation War.
  • Fascist Spain – Used some aircraft given to them by the Italians at the end of the Spanish Civil War and after.
  • SFR Yugoslavia – Captured some G.50 fighters from NDH during the war. Their use was very limited.
  • National Republican Air Force (Aeronautica Nazionale Repubblicana/ANR) – Operated a small number of G.50s, mostly as trainers.
  • Co-Belligerent Air Force (Aviazione Cobelligerante Italiana, or ACI) – Operated limited numbers.
  • Nazi Germany – A few were captured and saw limited use with the Luftwaffe.
  • China – There were plans to produce 50 G.50 aircraft in China but nothing came of this.
G.50 Freccia Specifications
Wingspan 35 ft 11 in / 10.9 m
Length 26 ft 3 in / 8 m
Height 10 ft 7 in / 3.28 m
Wing Area 196.5 ft² / 18.25 m²
Engine One 840 hp (626 kW) Fiat A.74 RC.38, 14 cylinder radial piston
Empty Weight 4,353 lbs / 1,975 kg
Maximum Takeoff Weight 5,324 lbs / 2,415 kg
Fuel Capacity 316 l
Maximum Speed 292 mph / 470 km/h
Range 267 mi / 445 km
Maximum Service Ceiling 35,100 ft (10,700 m)
Climb speed Climb to 19,700 ft (6,000 m) in 7 minutes and 30 seconds
Crew One pilot
Armament
  • Two 12.7 mm Breda-SAFAT heavy machine guns

Gallery

Illustrations by Haryo Panji https://www.deviantart.com/haryopanji

Fiat G.50 Prototype
Fiat G.50 “1-1” belonging to Mario Bonzano in Spain
G.50 MM4743 in Finnish Service
G.50 bis in Croatian Service circa 1941
G.50 B MM6137 in Luftwaffe Service

A G.50 from the 351st squadron in flight somewhere in Italy in January of 1941. [alieuomini.it]
Freccia in Italian service [monochrome-watches.com]
Side view of two G.50s, probably in Africa. [warbirdphotographs]

The Germans managed to capture a small numbers of surviving G.50s, but their use was limited. [warbirdphotographs]
The NDH received around 16 G.50 (with one G.50 B) planes during the war, but their use was very limited. [Asisbiz]

Credits