Blackburn Type E

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Following the success of its initial batch of wooden monoplanes, Blackburn shifted its focus to steel constructions, as demanded by the military. In November 1911, the War Office published requirements for a two-seater reconnaissance aircraft. One key demand was the ability to disassemble the aircraft for transport in crates from one operational area to another.

Table of Contents

Military Development and Requirements

Nine months before the competitive trials on Salisbury Plain, Blackburn built two monoplanes designated “Type E.” The first, assembled in April 1912, was a single-seater aircraft powered by a 60 hp Green inline engine. This particular aircraft was specifically created for Lieutenant W. Lawrence, who intended to use it in India.

Blackburn Type E Variants

The two-seater Type E, intended for the War Office tender trials, was constructed in June 1912 and fitted with a 70 hp Renault V-type engine. However, this second Type E proved too heavy to fly, significantly hindering its military application.

Technical Specifications

Modification	Blackburn Type E
Wingspan, m	11.68
Length, m	9.50
Wing area, m2	27.00
Normal takeoff weight, kg	431
Engine type	1 Piston engine Renault
Power, hp	1 x 70
Maximum speed, km/h	130
Cruising speed, km/h	105
Flight endurance, h	5
Crew	2 crew

Image and diagram gallery of the Blackburn Type E

British

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.

Blackburn Type E	Blackburn Type E
Blackburn Type E	Blackburn Type E
Blackburn Type E