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Blériot 111

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Blériot 111
Bleriot 111/3
Role Executive transport monoplane
Manufacturer Blériot Aéronautique
Designer André Herbemont
First flight 24 January 1929
Number built 2+

The Blériot 111 was a French four-seat executive transport monoplane designed by André Herbemont.[1] The first French aircraft to be fitted with a retractable landing gear, after six years development it was not ordered into production.[1]

Design and development

Bleriot 111 photo from Annuaire de L'Aéronautique 1931

The Bleriot 111 was a low-wing single-engined monoplane with an enclosed passenger cabin and an open cockpit for the pilot forward of the cabin.[1] The first variant was the Bleriot 111/1 which first flew on 24 January 1929 powered by a 280 hp (209 kW) Hispano-Suiza 6Mbr 6-cyl. water-cooled in-line engine.[1] In October 1929 a second variant flew (known as the 111bis or 111/2) which had a modified landing gear.[1] The 111/2 was re-engined with a 420 hp (313 kW) Gnome & Rhône 9Ady radial engine and re-designated 111/3.[1] The 111/3 was flown as part of the Patrouille Blériot which gave exhibitions and demonstrations around France and Spain in the 1930s.[1]

The 111/1 was modified as the 111/4 with a revised wing bracing, a 400 hp (298 kW) Hispano-Suiza 12Jb engine and retractable landing gear,a first for a French aircraft.[1] The 111/4 flew on 27 October 1930.[1] The next variant was the 111/5 which moved the pilot's cockpit to the rear of the passenger cabin and was fitted with a 500 hp (373 kW) Hispano-Suiza 12Mbr engine.[1] A re-engined variant of the 111/5 was fitted with a 500 hp (373 kW) Gnome-Rhône K-14(sic) radial engine and was named Sagittaire (Template:Lang-en).[1]

Sagittaire later fitted with a new wing and 840 hp (626 kW) Gnome & Rhône 14Kbrs, was re-designated 111/6.[1] The 111/6 was entered into the 1934 London to Melbourne air race but it was withdrawn when the landing gear was damaged two days before the race start.[1] With no commercial interest in the design no more Bleriot 111s were built.[1]

Variants

Bleriot 111/5 photo from L'Aerophile Salon 1932
Blériot Sagittaire photo from L'Aerophile November 1934
Bleriot 111/1
Powered by a 280 hp (209 kW) Hispano-Suiza 6Mbr 6-cyl. water-cooled in-line engine.[1]
Bleriot 111/2 / bis
Modified landing gear.
Bleriot 111/3
The 111/2 re-engined with a 420 hp (313 kW) Gnome & Rhône 9Ady radial engine. This aircraft ended up in the Spanish Republican Air Force during the Spanish Civil War.[2]
Bleriot 111/4
The 111/1 was modified as the 111/4 with a revised wing bracing, a 400 hp (298 kW) Hispano-Suiza 12Jb engine and retractable landing gear,a first for a French aircraft.[1]
Bleriot 111/5
The pilot's cockpit moved to the rear of the passenger cabin and fitted with a 500 hp (373 kW) Hispano-Suiza 12Mbr engine.[1]
Sagittaire
A re-engined variant of the 111/5 was fitted with a 500 hp (373 kW) Gnome-Rhône K-14(sic) radial engine and was named Sagittaire (Template:Lang-en).[1]
Bleriot 111/6
Sagittaire later fitted with a new wing and 840 hp (626 kW) Gnome & Rhône 14Kbrs

Operators

 France
 Spain

Specifications (111/6)

Data from [3]The Illustrated Encyclopedia of Aircraft

General characteristics

  • Crew: 1
  • Capacity: four passengers

Performance

See also

Related lists

References

Notes
  1. ^ a b c d e f g h i j k l m n o p q r Orbis 1985, p. 712
  2. ^ Aircraft that took part in the Spanish Civil War
  3. ^ Orbis 1985, p. 713
Sources
  • The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing. {{cite book}}: Cite has empty unknown parameter: |coauthors= (help)