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line. The new aircraft, designated CANT 23, appeared to possess a conventional appearance and presented a new, for the company, fuselage made of duralumin characterized by the closed passenger compartment and an open cockpit for the pilot. The veiling and the three- engine propulsion in the tractor configuration were substantially similar to the previous CANT 22.
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in demand from the air transport market with the possibility of making new connections to
Central and Eastern Europe and in particular the opening of a route capable of connecting Trieste airport - Ronchi dei Legionari or, alternatively, the new Noghere airport, then under construction near the village of Zaule, in Vienna to continue to Budapest.
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The project, the first of the CRDA-CANT that was not a seaplane, was supervised by the engineer
Raffaele Conflenti, who at that time held the position of chief designer and director of the technical office of the company of Monfalcone, which took experience gained in the creation of the CANT 22 hydro
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In 1927 the airline company Società Italiana
Servizi Aerei (SISA), a company owned by the brothers Callisto and Alberto Cosulich as well as the CRDA, had begun to operate on the route that joined the Italian Trieste with Budapest, capital of the then Kingdom of Hungary. In anticipation of an increase
158:) only on 11 July 1932. Although the design of CANT 23 benefited from all-metal construction, the constant development of the aeronautic industry determined the early technical ageing of the type and definitively undermined any further development. The program was suspended on 1 May 1933
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and was characterized by a closed passenger compartment equipped with 10 single armchairs that overlooked a series of five rectangular windows on each side. The cockpit was open, placed on the upper part in front of the wings and protected by a windshield. The wing configuration was
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The construction of the aircraft began as early as 1927, but its progress was slow, continuing until the beginning of the 1930s . In 1929 a cell was created for static tests but the prototype, serial number NC.136, managed to be registered
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configuration. Both were made with a structure of side members in profile and ribs in square section tube covered in painted canvas.
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biplane-sesquiplane with the upper wing, more open, connected to the lower, considerably smaller, thanks to a
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The CANT 23 was an entirely metallic aircraft with a conventional look, a three-engine,
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6-cylinder water-cooled in-line piston engines, 260 hp (190 kW) each
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was an
Italian trimotor airliner built by CANT in the late 1920s.
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V-12 water-cooled piston engine, 500 hp (370 kW)
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Aircraft of comparable role, configuration, and era
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378:Cantieri Aeronautici e Navali Triestini (CANT)
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474:Cantieri Riuniti dell'Adriatico (C.R.D.A.)
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324:: CS1 maint: location missing publisher (
310:Garello, Giancarlo; Zorini, Decio (2009).
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258:214 mph (344 km/h, 186 kn)
169:and the project was therefore abandoned.
312:Le Officine aeronautiche CANT 1923-1945
264:590 mi (950 km, 510 nmi)
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124:with a fixed trolley. The
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243:3-bladed metal propellers
235:Isotta Fraschini Asso 200
225:Isotta Fraschini Asso 500
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670:1920s Italian airliners
184:General characteristics
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16:1920s Italian aircraft
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86:Number built
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141:Development
659:Categories
294:References
165:1933-05-01
77:1932-07-11
675:Trimotors
637:Companies
320:cite book
209:Wingspan:
197:Capacity:
178:Data from
680:Biplanes
649:Aviation
589:Gabbiano
372:aircraft
314:. Italy.
275:See also
126:fuselage
39:Airliner
22:CANT 23
611:Portals
584:Alcione
203:Length:
163: (
122:biplane
110:CANT 23
101:CANT 22
75: (
579:Airone
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538:Z.1007
262:Range:
116:Design
52:Italy
625:Italy
594:Leone
572:Names
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523:Z.514
518:Z.511
513:Z.509
508:Z.508
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370:CANT)
191:Crew:
36:Role
326:link
233:2 ×
223:1 ×
108:The
61:CANT
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