To install click the Add extension button. That's it.

The source code for the WIKI 2 extension is being checked by specialists of the Mozilla Foundation, Google, and Apple. You could also do it yourself at any point in time.

4,5
Kelly Slayton
Congratulations on this excellent venture… what a great idea!
Alexander Grigorievskiy
I use WIKI 2 every day and almost forgot how the original Wikipedia looks like.
Live Statistics
English Articles
Improved in 24 Hours
Added in 24 Hours
What we do. Every page goes through several hundred of perfecting techniques; in live mode. Quite the same Wikipedia. Just better.
.
Leo
Newton
Brights
Milds

Caproni Ca.308 Borea

From Wikipedia, the free encyclopedia

Ca.308 Borea
Role Airliner
Manufacturer Caproni
First flight 1935
Primary user Ala Littoria
Number built 8

The Caproni Ca.308 Borea ("North Wind") was a small airliner built in Italy in the mid-1930s.

Development

The Ca.308 was a streamlined, low-wing cantilevered monoplane design of conventional configuration. Its undercarriage was not retractable. The mainwheels were fitted with spats.

The prototype, designated Ca.306, was exhibited at the Milan Exhibition of 1935.

The basic design of the Ca.308 subsequently served as the basis for a large family of military aircraft, beginning with the Caproni Ca.309.

Operational history

The Italian airline Ala Littoria ordered five examples.

The Italian government ordered two aircraft for general-purpose use by its colonial administration in Libya.

All these aircraft received the Ca.308 designation.

Variants

Ca 306
The prototype, exhibited at the Milan Exhibition of 1935.
Ca 308 Borea
Production aircraft, Seven built.

Operators

 Kingdom of Italy
 Italy

Specifications (Ca.308)

Caproni Ca. 308 Borea (Letectví, November 1935)

Data from European Transport Aircraft since 1910[1]

General characteristics

  • Crew: 3
  • Capacity: 7 passengers
  • Length: 12.87 m (42 ft 3 in)
  • Wingspan: 16.20 m (53 ft 2 in)
  • Height: 3.25 m (10 ft 8 in) [3]
  • Wing area: 38.4 m2 (413 sq ft)
  • Empty weight: 1,700 kg (3,748 lb)
  • Gross weight: 2,600–2,700 kg (5,732–5,952 lb)
  • Powerplant: 2 × de Havilland Gipsy Six six-cylinder inline engine, 150 kW (200 hp) each

Performance

  • Maximum speed: 246 km/h (153 mph, 133 kn)
  • Cruise speed: 210 km/h (130 mph, 110 kn)
  • Range: 1,200 km (750 mi, 650 nmi)
  • Service ceiling: 5,000 m (16,000 ft)
  • Rate of climb: 4.30 m/s (846 ft/min) [3]

See also

References

  1. ^ a b Stroud 1966, p. 411
  2. ^ aeroflight
  3. ^ a b Thompson 1963, p. 106
  • Stroud, John (1966). European Transport Aircraft since 1910. London: Putnam. OCLC 895249324.
  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 236.
  • Thompson, Jonathon (1963). Italian Civil and Military Aircraft 1930–1945. Aero Publishers, Inc. ISBN 0-8168-6500-0.
  • World Aircraft Information Files. London: Bright Star Publishing. pp. File 891 Sheet 11.
  • Уголок неба
This page was last edited on 16 August 2023, at 07:38
Basis of this page is in Wikipedia. Text is available under the CC BY-SA 3.0 Unported License. Non-text media are available under their specified licenses. Wikipedia® is a registered trademark of the Wikimedia Foundation, Inc. WIKI 2 is an independent company and has no affiliation with Wikimedia Foundation.