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Bleriot 165

Posted on September 22, 2026 By

Intended to replace the Farman Goliath airliner, the Bleriot 165 was a two-bay biplane featuring wings of equal span and a rectangular cross-section fuselage. Its powerplant included two air-cooled Gnome-Rhone Jupiter engines, installed in nacelles between the upper and lower wings. The two pilots were seated side-by-side in an open cockpit located in the nose of the fuselage.

The passenger cabin, designed for 16 people, was enclosed. The first Bleriot 165 took to the air on October 27, 1926. It was followed by a second aircraft, initially designated Bleriot 175, which featured Renault engines and equipment for night flights. Later, Jupiter engines were installed on this second aircraft, converting it into a second Bleriot 165.

Table of Contents

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    • Design and Features
    • Operational History
    • Variants and Unfulfilled Projects
    • Technical Specifications
  • Image and diagram gallery of the Bleriot 165
    • How to cite this article:

Design and Features

The Bleriot 165 was conceived as a robust and efficient biplane, marking an evolution in air transport of its era. Its two-bay structure and the placement of engines in nacelles optimized aerodynamics and maintenance. The capacity for 16 passengers in an enclosed cabin offered an advanced level of comfort for the standards of the 1920s.

Operational History

Both machines were utilized by the “Air-Union” airline on the prestigious “Golden Ray” line, connecting Paris and London. This route symbolized the link between two major European capitals, and the Bleriot 165 played a crucial role in the development of commercial air travel between them. Its reliability and capacity made it a valuable asset for interwar aviation.

Variants and Unfulfilled Projects

Plans for a military variant, a three-seat bomber designated Bleriot 123, were abandoned. The idea for a second Bleriot 175, intended for a transcontinental flight to Tokyo, was also scrapped. These decisions reflect the economic and strategic challenges of the era, which often limited the development of ambitious projects.

Technical Specifications

Modification Bl-165
Wingspan, m 23.00
Length, m 14.85
Height, m 4.85
Wing area, m2 119.10
Empty weight 2919
Normal takeoff weight 5600
Engine type 2 Piston engine Gnome & Rhône 9Ab
Power, hp 2 x 420
Maximum speed, km/h 185
Cruising speed, km/h 158
Practical range, km 525
Service ceiling, m 4000
Crew, crew members 3
Payload maximum – up to 16 passengers

Image and diagram gallery of the Bleriot 165

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How to cite this article:

APA: Bleriot 165 (). Bleriot 165. wp.archivoaereo.com. https://wp.archivoaereo.com/en/bleriot-165-3/
VANCOUVER: Bleriot 165 [online]. wp.archivoaereo.com; [cited 2026-09-22]. Available at: https://wp.archivoaereo.com/en/bleriot-165-3/
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