Italian light bombers and reconnaissance aircrafts

Ad: This forum contains affiliate links to products on Amazon and eBay. More information in Terms and rules

In July 1935 there flew the prototype of a large wooden twin-float-seaplane, powered by three 840 hp (626 kW) Isotta-Fraschini Asso XI inline engines. This was the CRDA Cant Z.505 which had been designed as a mail-plane. On 19 August in the same year, Mario Stoppani conducted the first flight of the slightly smaller and lighter Z.506, a 12/14-passenger transport with three 610 hp (455 kW) Piaggio Stella IX radial engines. The type was put into production in 1936 as the Z.506A, and entered service with the Italian airline Ala Littoria during that year on routes around the Mediterranean. Powered by three 750 hp (559 kW) Alfa Romeo 126 RC.34 radial engines the Z.506A, flown mostly by Mario Stoppani, set several altitude, distance and speed records in 1936-8, including speeds of 191.539 mph (308.25 km/h), 198.7 mph (319.78 km/h) and 200.118 mph (322.06 km/h) over distances of 3,107 miles (5000 km), 1,243 miles (2000 km) and 621 miles (1000 km) respectively. It carried a payload of 4,409 lbs (2000 kg) to 25,623 ft (7810 m) and 11,023 lbs (5000 kg) to 22,693 ft (6917 m) and later flew 3,345.225 miles (5383.6 km) over a closed circuit.

A military version, designated Z.500B Airone (Heron), was shown at the Milan Aeronautical Exhibition in October 1937. This had a stepped, extensively glazed tandem two-seat cockpit and a ventral gondola which contained the bomb aimer's position and the bomb bay, immediately behind which was a gunner's position. The Z.506B was built at Cant's Monfalcone and Finale Ligure Factories, and by Piaggio under licence. In November 1937 a Z.506B with 750 hp (559 kW) Alfa Romeo 127 RC.55 engines set a load-to-height record of 33,318 ft (10155 m) with a 2,205 lbs (1000 kg) payload, and then flew 4,362 miles (7020 km) non-stop from Cadiz to Carevalas. Z.506 variants included an air-sea rescue Z.506S of which at least 20 were produced as conversions from Z.506Bs, and a single Z.506 landplane which was specially prepared with fixed, spatted landing gear for an endurance record attempt by Mario Stoppani; this was at first postponed, then finally cancelled, because of continuing bad weather. In 1936 a heavy bomber prototype, which was essentially a scaled-up version of the Z.506, was built under the designation Z.508. No production version resulted but this aircraft, powered by three 840 hp (627 kW) Isotta-Fraschini Asso XI RC.40 engines, was used to set a number of records, including a speed of 154.26 mph (248.25 km/h) over a 1,234 mile (2000 km) course with an 11,023 lbs (5000 kg) payload.

Last of this family was the Z.509, a larger and heavier version of the Z.506A of which three were built in 1937 for use on Ala Littoria's transatlantic postal service to South America. This model was powered by three Fiat A.80 RC.41 radial engines, and a new wing of 92 it 11 in (28.32 m) span and 1,076.43 sq it (100.00m2) area was introduced to compensate for increased empty and maximum take-off weights of 22,000 lbs (9980 kg) and 35,200 lbs (15965 kg) respectively. Production of the Z.506B totalled 324, including two prototypes which were supplied to the Regia Aeronautica and the Regia Marina; the latter service took over 29 aircraft, the balance of a Polish order for 30 which were not delivered as a result of the German invasion. Five were delivered to the Nationalist forces in the Spanish Civil War late in 1938. A number of the Z.506S air-sea rescue aircraft remained in service until 1959.

The Largest float seaplane to give wide spread operational service during World War II (although the Junkers Ju 52/3mW might also lay claim to this achievement), the Italian Cant Z.506B Airone (Heron) three engine twin-float reconnaissance bomber was developed from the commercial Z.506A in 1936, production of the military aircraft starting the following year with a batch of 32 aircraft (Serie I) and differing from the earlier aircraft in featuring a long ventral gondola accommodating bomb bay, bomb-aimer's station and a rear ventral gun position. A semi-retractable gun turret was also added.

The early Z.506B aircraft were evaluated with the Aviazione Legionaria in Spain during 1939, 30 other aircraft having also been ordered by the Polish naval wing (in the event only one of the latter had arrived in Poland when the Germans invaded in September, and the remaining aircraft were taken on charge by Italy's Regia Marina). By the date of Italy's entry into the war in June 1940 the Z.506B was in full production, 95 aircraft having been completed by the parent company. Most of these were serving with the 31° and 35° Stormi Bombardamento Marittimo at Elmas and Brindisi respectively were these units were fairly heavily engaged during the campaign in Greece, although they seldom operated when likely to be opposed by RAF fighters. They participated in the capture of Corfu, Cefalonia and Zante, and attempted to shadow British naval forces after the Battle of Cape Matapan but sheered away when faced by Fleet Air Arm Fairey Fulmar fighters. Thereafter the "Airone" was almost entirely withdrawn from use as a bomber and torpedo attack aircraft, the Italian navy calling for its greater use in maritime reconnaissance, air-sea rescue, convoy escort and anti-submarine patrol roles; such had been the shift in naval superiority in the Mediterranean following the debacle at Taranto and the Battle of Cape Matapan.

Development and production of the Airone continued, with small modifications being introduced with each new production batch (serie), of which Serie XII was the most important. A special air-sea rescue conversion was the Z.506S (Soccorso), this version being also used in small numbers by the Luftwaffe. After the Italian surrender 23 Z.506B and five Z.506S aircraft were flown to Allied ports and subsequently flew with the Co-Belligerent Air Force's Raggruppamento Idro, performing transport and other second-line tasks.
 

Attachments

  • Cant Z506 Airone 001.jpg
    Cant Z506 Airone 001.jpg
    153.9 KB · Views: 431
  • Cant Z506 Airone 002.jpg
    Cant Z506 Airone 002.jpg
    104.4 KB · Views: 548
  • Cant Z506 Airone 003.jpg
    Cant Z506 Airone 003.jpg
    79.1 KB · Views: 628
  • Cant Z506 Airone 005.jpg
    Cant Z506 Airone 005.jpg
    138.5 KB · Views: 427
  • Cant Z506 Airone 006.jpg
    Cant Z506 Airone 006.jpg
    109.9 KB · Views: 577
  • Cant Z506 Airone 007.jpg
    Cant Z506 Airone 007.jpg
    124.1 KB · Views: 415
  • Cant Z506 Airone 008.jpg
    Cant Z506 Airone 008.jpg
    105.8 KB · Views: 542
  • Cant Z506 Airone 009.jpg
    Cant Z506 Airone 009.jpg
    93 KB · Views: 1,285
  • Cant Z506 Airone 0010.jpg
    Cant Z506 Airone 0010.jpg
    59.7 KB · Views: 737
Cant Z.506B - This was a militarised version featuring a stepped, extensively glazed tandem two-seat cockpit and a ventral gondola which contained the bomb aimer's position and the bomb bay, immediately behind which was a gunner's position with a single 7.7 mm (0.303 in) Breda-SAFAT machine-gun. A 12.7-mm (0.50 in) gun was fitted in the Breda M.1 upper turret. The bomb bay could accommodate an 1,764 lbs (800 kg) torpedo or a combination of smaller weapons to a similar total weight, while later versions were able to carry a bomb load of 2,645 lbs (1200 kg) and were equipped with two 7.7 mm (0.303 in) Breda-SAFAT machine-guns in waist positions and a Caproni-Lanciani Delta E turret replacing the Breda turret. The Z.506B was built at CANT's Monfalcone and Finale Ligure factories, and by Piaggio under licence.

Cant Z.506S Soccorso - A dedicated air-sea rescue version, including 20 Z.506Bs converted by Savoia-Marchetti in 1948.

Cant Z.506 Landplane - One Z.506 was specially prepared for an endurance record attempt by Mario Stopparii, and was converted to a landplane configuration with fixed, spatted landing gear. The flight was at first postponed and then cancelled as a result of continuing bad weather.

Cant Z.508 - A 1936 heavy bomber prototype, essentially a scaled-up version of the Z.501. Data included a powerplant of three 840 hp (627 kW) Isotta-Fraschini Asso XI RC.40 engines, with a maximum speed of 196 mph (315 km/h), span 30 m (98 ft 5 in) and length 21.45 m (70 ft 5 in). This sole example of the type set several records, including the carriage of a 22,046 lbs (1000 kg) load to 6,560 ft (2000 m) and a speed of 154.26 mph (248.25 km/h) over a 1,243 mile (2000 km) course with a 11,023 lbs (5000 kg) load.

Cant Z.509 - Three aircraft of this larger and heavier version of the Z.506A were built in 1937 for Ala Littoria's transatlantic postal service to South America, powered by three Fiat A.80 RC.41 radial engines and with a new wing of 92 ft 11 in (28.32 m) span and 1,076.43 sq ft (100 sq m) area to compensate for increased empty and maximum take-off weights of 22,000 lbs (9980 kg) and 35,200 lbs (15965 kg) respectively.

Source: Cant Z.506B Airone
 

Attachments

  • Cant Z506 Airone 0011.jpg
    Cant Z506 Airone 0011.jpg
    67.9 KB · Views: 427
  • Cant Z506 Airone 0012.jpg
    Cant Z506 Airone 0012.jpg
    91.7 KB · Views: 342
  • Cant Z506 Airone 0013.jpg
    Cant Z506 Airone 0013.jpg
    105.4 KB · Views: 1,086
  • Cant Z506 Airone 0014.jpg
    Cant Z506 Airone 0014.jpg
    84.8 KB · Views: 403
  • Cant Z506 Airone 0015.jpg
    Cant Z506 Airone 0015.jpg
    119.6 KB · Views: 715
  • Cant Z506 Airone 0016.jpg
    Cant Z506 Airone 0016.jpg
    104.8 KB · Views: 418
  • Cant Z506 Airone Floatplane-01.jpg
    Cant Z506 Airone Floatplane-01.jpg
    74.6 KB · Views: 245
Last edited:
The SM.85 was part of a programme by the Regia Aeronautica to produce a twin-engine monoplane dive bomber based on the theories developed over the previous 20 years by the American General Billy Mitchell, which were enthusiastically adopted by Colonel Amedeo Mecozzi (who also developed the Breda Ba.64 and its derivatives) for attack aircraft. The resulting aircraft, constructed of wood, had a wing set in an upper-middle configuration, a rectangular cross-section fuselage, retractable undercarriage and a fixed tailwheel, and was powered by two Piaggio P.VII C.35 engines. The wings, made totally of wood, had three longerons, with fabric covering. The aircraft was designed to give the pilot the best possible forward view, with a transparent panel built into the cockpit floor. The SM.85's useful payload was 1,150 kg (2,540 lb), including the possibility of fitting a 12.7 mm (0.5 in) machine gun with 300-500 rounds. The aircraft was capable of also using its flaps as airbrakes for diving attacks, a notable characteristic of this aircraft. The bombload was carried in a parallelogram-shaped section mounted under the fuselage. The SM.85 was capable of carrying a 500 kg/1,100 lb bomb (or an 800 kg/1,760 lb bomb, the heaviest weapon in the Italian aviation arsenal, but only on very short range missions).

At maximum payload, with a 4,000 kg (8,820 lb) takeoff weight, the climb rate was 20 min to 5,000 m (16,400 ft), but freshly started engines did not produce their theoretical maximum power and the aircraft was usually much slower than this. The takeoff needed 433 m (1,421 ft), and the landing 415 m (1,362 ft). Ceiling was 6,000-6,500 m (19,690-21,330 ft) and 756–827 km (470-514 mi) range. Maximum speed was 367 km/h ( mph) at 4,000 m (13,123 ft). The fuel capacity was 1,078 L (285 US gal), contained in four self-sealing fuel tanks. At the maximum payload with a 500 kg (1,100 lb) bomb, it was incapable of taking off with a full fuel load (around 730 kg/1,610 lb), so this was used only on ferrying missions. The first prototype was tested in December 1936, and in spite of its insufficient speed and the disappointing rates of climb, the Regia Aeronautica felt there was sufficient room for development and ordered the SM.85 into production. Despite some improvements, critical deficiencies continued to be experienced during test flights by the Reparto Sperimentale Volo a Tuffo. These revised aircraft were disappointing as dive bombers in almost every aspect, with the most serious problems encountered being frequent uncontrollable spins, extremely slow climb rate after a dive, and instability during the dive. Production of the aircraft was halted, and the 34 produced up to that time were organised as 96° Gruppo Tuffatori (96th Independent Dive-Bomber Group).

In June 1940, 96° Gruppo Tuffatori was relocated to Pantelleria, a small island off Sicily, in anticipation of attacks on Malta and the British Mediterranean fleet. The commander of the group, Maggiore Ercolano Ercolani, made it clear to the General Staff that in combat the performance of the aircraft was such that it would result in 100% losses. In order to prove his assertion, Ercolani volunteered to fly the aircraft himself. These aircraft still didn't suffer any losses until the transfer to Pantelleria, when one of them crashed to a wall, killing the pilot. The others carried out a few missions over the Mediterranean until the end of July, but were never involved in real combat. The aircraft was soon withdrawn from service and scrapped, and the Regia Aeronautica was obliged to acquire Junkers Ju 87s from Germany which were rapidly introduced into service by the end of summer 1940. The differences in speed and other characteristics between the two aircraft was not great, apart from the availability of a rear gunner, but the Ju 87 was much more effective as a combat aircraft.

Source: Savoia-Marchetti SM.85 - Wikipedia, the free encyclopedia
 

Attachments

  • Savoia Marchetti SM-85 001.jpg
    Savoia Marchetti SM-85 001.jpg
    133.1 KB · Views: 350
  • Savoia Marchetti SM-85 002.jpg
    Savoia Marchetti SM-85 002.jpg
    118.6 KB · Views: 284
  • Savoia Marchetti SM-85 0021 (1).jpg
    Savoia Marchetti SM-85 0021 (1).jpg
    116.1 KB · Views: 284
Gran trabajo Gekho, sorry that I wasnt able to help you with the argentinian thread, I been with little spare time lately.

No te preocupes, ya encontre un par de fotos de los Ju-52 argentinos, con eso voy tirando. Felices fiestas.
 
A propaganda triumph when its appearance was trumpeted by Mussolini's Fascist regime in 1936, the Breda Ba.88 Lince (lynx), designed by Antonio Parano and Giuseppe Panzeri, was a sleek all-metal shoulder wing monoplane with twin engine powerplant. The prototype (MM 302) , which had a single vertical tail assembly, made its maiden flight during October 1936 flown by Furio Niclot, Breda's chief test pilot. In April 1937 Niclot established two world speed-over-distance records, averaging 321.25 mph (517 km/h) over a 62 mile (l00 km) distance and 295.15 mph (475 km/h) over a 621 mile (1000 km) circuit. In December of that year he raised these speeds to 344.24 mph (554 km/h) and 325.6 mph (524 km/h) respectively. The prototype, which had retractable tailwheel landing gear, and powerplant comprising two 900 hp (671 kW) Gnome-Rhône K-14 radials, was then given a modified tail unit with twin fins and rudders. Regarded as an aeroplano di combattimento, suitable for attack, long-range reconnaissance or bombing operations. The Ba.88 then had its military equipment and weapons installed. Immediately, performance and flight characteristics fell off dramatically, but by then production orders were already being executed. The first batch of 80, plus eight dual-control trainers, was built by Breda between May and October 1939. Problems with the prototype led to a number of weight-saving modifications, and more power was provided by the installation of 1,000-hp (746 kW) Piaggio P.XI RC.40 radials. On 16 June 1940, just after Italy's declaration of war on France and her allies, the Ba.88 had its first taste of action.

Twelve aircraft from the Regia Aeronautica's 19° Gruppo Autonomo made bombing and machine-gun attacks on the principal airfields of Corsica and three days later nine Ba.88s made a repeat attack. Analysis of these operations showed that the Ba.88 had only limited value, and any remaining doubts were settled when Ba.88s of the 7° Gruppo Autonomo joined action in Libya against the British. Fitted with sand filters, the engines overheated and failed to deliver their designed power. Attacks on targets at Sidi Barrani had to be aborted in September 1940, the aircraft failing to gain sufficient altitude or maintain formation, and reaching a speed less than half that claimed by the manufacturers. By mid-November 1940 most surviving Ba.88s had been stripped of useful equipment and were scattered around operational airfields as decoys for attacking British aircraft. During this time, however, further batches of Ba.88s were being delivered, comprising 19 built by Breda and 48 by IMAM (Meridionali). Most went straight to the scrap yard.

Three Ba.88s were modified by the Agusta plant in 1942 to serve as ground-attack aircraft. Wingspan was increased by 6 ft 6% in (2.00 m) to alleviate wing loading problems, their engines were replaced by Fiat A.74s, nose armament was increased to four 12.7 mm (0.50 in) Breda-SAFAT machine-guns, and dive brakes were installed. These Breda Ba.88Ms were delivered to the 103° Gruppo Autonomo Tuffatori (independent dive-bombing group) at Lonate Pozzolo on 7 September 1943. They were flight-tested by Luftwaffe pilots, but that was the last heard of the Breda Ba.88 which represented, perhaps, the most remarkable failure of any operational aircraft to see service in World War II.

Source: Breda Ba.88 RC.40 Lince
 

Attachments

  • Breda Ba-88 Lince 001.jpg
    Breda Ba-88 Lince 001.jpg
    90.6 KB · Views: 392
  • Breda Ba-88 Lince 002.jpg
    Breda Ba-88 Lince 002.jpg
    110.5 KB · Views: 224
  • Breda Ba-88 Lince 003.jpg
    Breda Ba-88 Lince 003.jpg
    91.5 KB · Views: 271

Users who are viewing this thread

Back