Bleriot XLIII

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In March 1913, Louis Bleriot constructed the Bleriot XLIII, a dedicated reconnaissance and observation aircraft. This new model was a further development of the Bleriot XXXVI, featuring a two-seater mid-wing monoplane design with a monocoque fuselage. It was powered by an 80 hp Gnome 7A engine.

Table of Contents

Innovative Design and Crew Layout

The crew was accommodated in the cockpit in a tandem configuration. A special porthole was added to the floor for the observer, providing an excellent downward field of view. This feature was intended to enhance its reconnaissance capabilities significantly.

Operational Potential and Limitations

The Bleriot XLIII was designed for long-range reconnaissance missions. However, its mediocre flight characteristics ultimately prevented Louis Bleriot from securing a contract for its serial production. Despite its innovative features, the aircraft did not achieve widespread success.

Technical Specifications

Modification	Bleriot XLIII
Wingspan, m	10.10
Length, m	6.12
Height, m	3.10
Wing area, m2	19.30
Empty weight	350
Maximum takeoff weight	625
Engine type	1 Piston engine Gnome 7A
Power, hp	1 x 80
Maximum speed, km/h	120
Cruising speed, km/h	100
Crew, crew members	2

Image and diagram gallery of the Bleriot XLIII

French

ArchivoAéreo Editorial Team

A group of aviation researchers and enthusiasts dedicated to documenting and preserving global aeronautical history. All articles are reviewed to ensure historical accuracy.

Sources & Accuracy

The information presented in this technical sheet has been compiled from declassified flight manuals, historical archives, and specialized literature. While we strive for maximum accuracy, some performance data may vary depending on the specific variant or operational conditions.