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Farman F.160

The Farman F.160 was a heavy bomber aircraft developed in France in the late 1920s. It was essentially an attempt by Farman Aviation Works to modernise its tremendously successful F.60 Goliath design of the immediately postwar years. The most noticeable external difference was the larger tailfin of the new aircraft. Like its predecessor, it was a large three-bay biplane of conventional configuration with unstaggered wings of equal span. Initially conceived as a heavy night bomber, most examples built were float-equipped torpedo bombers for the Aéronautique Maritime, which operated some 40 of the F.165 variant and 200 of the F.168. One of the original F.160 night bombers was exported to Italy, and one to Japan. Plans to develop airliner versions did not progress past the prototype stage.

F.160 Goliath
Farman F.160
Role Bomber
Manufacturer Farman
First flight 1928
Primary user Aéronautique Maritime
Number built c. 250

Variants edit

F.160
Four-seat night bomber with two 370 kW (500 hp) Farman 12We engines, designated F.160 BN.4 by Aviation Militaire.
F.161
One airliner with 2x 360 kW (480 hp) Gnome-Rhône 9Akx engines and one bomber similar to the F.160, powered by 2x 370 kW (500 hp) Farman 12Wers engines.
F.162
One prototype airliner with 2x 360 kW (480 hp) Gnome-Rhône 9Akx engines.
F.163
Airliner with 2x 280 kW (380 hp) Gnome-Rhône 9Aa engines.
F.165
Seaplane torpedo bomber with 2x Gnome-Rhône 9A or 9Aa engines.
F.166
2x 170 kW (230 hp) Salmson 9Ab engines.
F.167
Seaplane torpedo bomber with 2x 310 kW (420 hp) Gnome-Rhône 9Aa engines.
F.168
Seaplane torpedo bomber with Gnome-Rhône 9Akx engines; main production version, 200 built.
F.169
Improved airliner version with Gnome-Rhône 9Akx engines.
F.268
One F.168 fitted with 2x supercharged 370 kW (500 hp) Salmson 18 Abs engines.
F.269
One F.169 fitted with floats and modified wings as a sesquiplane seaplane.
F.368
One F.168 re-engined with 2x 400 kW (530 hp) Gnome-Rhône 9Kbrs engines.

Operators edit

  France
  Italy
  • one aircraft only.
  Japan
  • One aircraft only.
  Romania

Specifications (F.168) edit

 
Farman F.160 3-view drawing from L'Aérophile-Salon1926

General characteristics

  • Crew: Five
  • Length: 15.18 m (49 ft 10 in)
  • Wingspan: 26.25 m (86 ft 2 in)
  • Height: 6.10 m (20 ft 0 in)
  • Wing area: 159.6 m2 (11,718 sq ft)
  • Empty weight: 4,600 kg (10,140 lb)
  • Gross weight: 6,800 kg (14,990 lb)
  • Powerplant: 2 × Gnome-Rhône 9Akx , 360 kW (480 hp) each

Performance

  • Maximum speed: 174 km/h (108 mph, 94 kn)
  • Range: 800 km (500 mi, 430 nmi)
  • Service ceiling: 5,000 m (16,400 ft)
  • Rate of climb: 2.1 m/s (410 ft/min)

Related lists

References edit

  • Liron, Jean (1984). Les avions Farman. Collection Docavia. Vol. 21. Paris: Éditions Larivière. OCLC 37146471.
  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 379. ISBN 0-7106-0710-5.
  • World Aircraft Information Files. London: Bright Star Publishing. pp. File 894 Sheet 15. ISBN 1-156-94382-5.

External links edit

  • "The Paris Aero Show 1926". Flight: 779. 2 December 1926. Retrieved 2008-03-11.

farman, this, article, includes, list, references, related, reading, external, links, sources, remain, unclear, because, lacks, inline, citations, please, help, improve, this, article, introducing, more, precise, citations, january, 2024, learn, when, remove, . This article includes a list of references related reading or external links but its sources remain unclear because it lacks inline citations Please help improve this article by introducing more precise citations January 2024 Learn how and when to remove this message The Farman F 160 was a heavy bomber aircraft developed in France in the late 1920s It was essentially an attempt by Farman Aviation Works to modernise its tremendously successful F 60 Goliath design of the immediately postwar years The most noticeable external difference was the larger tailfin of the new aircraft Like its predecessor it was a large three bay biplane of conventional configuration with unstaggered wings of equal span Initially conceived as a heavy night bomber most examples built were float equipped torpedo bombers for the Aeronautique Maritime which operated some 40 of the F 165 variant and 200 of the F 168 One of the original F 160 night bombers was exported to Italy and one to Japan Plans to develop airliner versions did not progress past the prototype stage F 160 Goliath Farman F 160 Role Bomber Manufacturer Farman First flight 1928 Primary user Aeronautique Maritime Number built c 250Variants editF 160 Four seat night bomber with two 370 kW 500 hp Farman 12We engines designated F 160 BN 4 by Aviation Militaire F 161 One airliner with 2x 360 kW 480 hp Gnome Rhone 9Akx engines and one bomber similar to the F 160 powered by 2x 370 kW 500 hp Farman 12Wers engines F 162 One prototype airliner with 2x 360 kW 480 hp Gnome Rhone 9Akx engines F 163 Airliner with 2x 280 kW 380 hp Gnome Rhone 9Aa engines F 165 Seaplane torpedo bomber with 2x Gnome Rhone 9A or 9Aa engines F 166 2x 170 kW 230 hp Salmson 9Ab engines F 167 Seaplane torpedo bomber with 2x 310 kW 420 hp Gnome Rhone 9Aa engines F 168 Seaplane torpedo bomber with Gnome Rhone 9Akx engines main production version 200 built F 169 Improved airliner version with Gnome Rhone 9Akx engines F 268 One F 168 fitted with 2x supercharged 370 kW 500 hp Salmson 18 Abs engines F 269 One F 169 fitted with floats and modified wings as a sesquiplane seaplane F 368 One F 168 re engined with 2x 400 kW 530 hp Gnome Rhone 9Kbrs engines Operators edit nbsp France French Navy nbsp Italy one aircraft only nbsp Japan One aircraft only nbsp Romania Royal Romanian Air ForceSpecifications F 168 edit nbsp Farman F 160 3 view drawing from L Aerophile Salon1926 General characteristics Crew Five Length 15 18 m 49 ft 10 in Wingspan 26 25 m 86 ft 2 in Height 6 10 m 20 ft 0 in Wing area 159 6 m2 11 718 sq ft Empty weight 4 600 kg 10 140 lb Gross weight 6 800 kg 14 990 lb Powerplant 2 Gnome Rhone 9Akx 360 kW 480 hp each Performance Maximum speed 174 km h 108 mph 94 kn Range 800 km 500 mi 430 nmi Service ceiling 5 000 m 16 400 ft Rate of climb 2 1 m s 410 ft min Related lists List of Interwar military aircraftReferences editLiron Jean 1984 Les avions Farman Collection Docavia Vol 21 Paris Editions Lariviere OCLC 37146471 Taylor Michael J H 1989 Jane s Encyclopedia of Aviation London Studio Editions p 379 ISBN 0 7106 0710 5 World Aircraft Information Files London Bright Star Publishing pp File 894 Sheet 15 ISBN 1 156 94382 5 External links edit nbsp Wikimedia Commons has media related to Farman F 160 The Paris Aero Show 1926 Flight 779 2 December 1926 Retrieved 2008 03 11 Retrieved from https en wikipedia org w index php title Farman F 160 amp oldid 1198989424, wikipedia, wiki, book, books, library,

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