Breguet Br.890

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.

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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Br.890