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Blackburn B.20


The Blackburn B-20 was an experimental aircraft, first flying in 1940, that attempted to drastically increase the performance of flying boat designs. 

Blackburn Aircraft undertook an independent design study based on a patent filed by their chief designer, John Douglas Rennie for a retractable pontoon float that formed the planning hull.

The B-20 was an attempt to combine the best features of both the flying boat and the floatplane.

While on the water, the B-20 was essentially a floatplane, using a large float under the fuselage for buoyancy, and two smaller floats near the wingtips for stability.

In flight, the main float retracted upwards towards the fuselage, fitting into a “notch” to become streamlined as a part of the fuselage.

The wing floats folded outwards, somewhat like those on the American Consolidated PBY flying boat design, to become the wingtips.

This configuration gave the correct wing incidence for take-off and for flight and in the latter a much-reduced drag compared to the deep hulls of flying boats.

Blackburn, along with Supermarine, Shorts and Saunders-Roe tendered designs against Air Ministry Specification R1/36.

The Supermarine was chosen initially but Supermarine could not start work soon enough (due to their work on the Spitfire) and what would enter service as the Saunders Roe Lerwick became the chosen aircraft.

However, the Ministry was interested enough to authorise and contract for the construction of a prototype of the B-20, serial number V8914, to test the concept.

The prototype, built at Dumbarton, flew for the first time on 26 March 1940.

On 7 April, during a test run, the aircraft experienced extreme vibration due to aileron flutter and the crew bailed out.

Three were lost, the other two were picked up by HMS Transylvania, a converted merchantman. Development ceased when the first prototype crashed, as Blackburn’s resources were dedicated to the war effort.

The Ministry felt the concept had been proven and the crash was not due to the pontoon design.



The B-40 was an improved variant of the B-20 with Bristol Centaurus engines to meet a requirement for a small general purpose flying boat and specification R.13/40 was raised for it.





69 ft 8 in (21.23 m)


82 ft 0 in (24.99 m) floats retracted


25 ft 2 in (7.67 m) hull extended

Wing area

1,066 sq ft (99.0 m2)

Max take-off weight

35,000 lb (15,876 kg)


2 × Rolls Royce Vulture X-24 liquid-cooled piston engines,

1,720 hp (1,280 kW) each


3 bladed Rotol constant speed feathering propellers


Maximum speed

306 mph (492 km/h, 266 kn) at 15,000 ft (4,572 m)


1,500 mi (2,400 km, 1,300 nmi)



Provision for two turrets and other defensive positions


Bomb cells in centre section.






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