Breguet Br.890

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After the end of the Second World War, designers at Breguet Aviation developed a project for a multi-purpose transport aircraft capable of carrying up to 30 passengers. This project envisioned the construction of three modifications: the multi-purpose transport-passenger Br.890, the military transport Br.891, and the passenger Br.892.

Table of Contents

Initial Design and Engine Choices

Initially, the first variant of the aircraft, designated Br.890J, was planned to be equipped with 1200 hp Junkers Jumo 211 engines, produced at the Arsenal factory. However, during the construction phase of the first prototype, it was decided to replace these engines with English Bristol Hercules 739 units, delivering 2030 hp.

Maiden Flight and Trials

This version of the aircraft, the Br.890H (tail number F-WFRF), first flew on April 5, 1950. The aircraft successfully completed its tests, but despite its success, it did not proceed to serial production.

Technical Specifications

Modification	Br. 89 0H
Wingspan, m	30.62
Aircraft length, m	21.60
Aircraft height, m	7.20
Wing area, m2	101.00
Empty weight	12040
Maximum takeoff weight	20000
Engine type	2 Piston engine Bristol Hercules 739
Power, hp	2 x 2030
Maximum speed, km/h	380
Cruising speed, km/h	350
Range with max. payload, km	1000
Service ceiling, m	7800
Crew, crew	4
Payload:	34-40 passengers or 6210 kg of commercial cargo

Image and diagram gallery of the Breguet Br.890

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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.

Br.890	Br.890
Br.890	Br.890
Br.890	Br.890
Br.890