






One prototype, first flown on 28 November 1934. No production.
Engine: 1 x 700hp Armstrong Siddeley Tiger IV
Wingspan: 14.02 m / 45 ft 12 in
Length: 10.80 m / 35 ft 5 in
Height: 3.89 m / 12 ft 9 in
Wing area: 774.63 sq.m / 8338.04 sq ft
Max. speed: 233 km/h / 145 mph
Ceiling: 3200 m / 10500 ft
Range: 765 km / 475 miles
Crew: 2-3
Armament: 2 x 7.7mm machine-guns, 1 x 450kg or 2 x 227kg bombs or a torpedo

The Shark was a carrier-borne torpedo biplane with a buoyant metal-skinned fuselage and a 750hp Armstrong Siddeley Tiger IV two-row radial engine. Production for the Fleet Air Arm was undertaken between 1934 and 1937, with 238 Shark I, II and III (Pegasus radial engines) being built, many as seaplanes. Accommodation was provided for a crew of two and armament comprised one 680kg torpedo or equivalent bomb load, plus one forward-firing Vickers and one rear-mounted Vickers or Lewis machine-gun. Deck take-offs and landings were aided by the large camber-changing flaps fitted to the aircraft. Sharks served with Nos 820 and 821 Squadrons on board HMS Courageous, No 822 Squadron on board HMS Furious and No 705 (Catapult) Flight on the battleships HMS Repulse and Warspite. The type was also used at Air Gunnery Schools in the UK and Trinidad.
Six Sharks were also delivered to the Portuguese Navy in March 1936 and were based at Bom Succeso on the River Tagus, near Lisbon, where they operated for several years. Four aircraft were built for the Royal Canadian Air Force and 17 IIIs were built under licence by Boeing Aircraft of Canada during 1939-40, mainly for the RCAF.

Blackburn B 6 Shark Mk.II
Engine: Armstrong Siddeley Tiger VI, 750 hp, 567kW
Length: 35 ft 3 in / 10.74 m
Height: 12 ft 1 in / 3.68 m
Wingspan: 45 ft 12 in / 14.02 m
Wing area: 489.009 sq.ft / 45.43 sq.m
Max take off weight: 8050.5 lb / 3651.0 kg
Weight empty: 4039.6 lb / 1832.0 kg
Max. speed: 130 kt / 241 km/h
Cruising speed: 103 kt / 190 km/h
Service ceiling: 15994 ft / 4875 m
Wing load: 16.4 lb/sq.ft / 80.0 kg/sq.m
Range: 543 nm / 1006 km
Crew: 2-3
Armament: 2x cal.303 MG (7,7mm), 680kg Torp.


The Blackburn R.B.3A Perth development of the Iris was to replace the earlier flying-boat in service with No. 209 Squadron at Plymouth. The Perth differed from the Iris V primarily in having an, enclosed cockpit, and a hull covered with corrosion-resistant material. An improvement in armament was the installation of a 37mm gun in the bow position for anti-shipping work, but there was also an alternative rail-mounted 7.7mm machine-gun, as on the Iris.
The Perth’s service introduction came in January 1934 when the second aircraft was delivered to Plymouth. At that time the first was still under test at Felixstowe, but by 31 May 1934 all three from the first contract had been delivered. A fourth Perth had been ordered subsequently and flew in April 1934, but this was retained at the MA&EE Felixstowe for experimental work.
Problems with the tail unit required the flying-boats to be modified at Brough, keeping them out of service for several months. The first Perth was lost in heavy seas during September 1935, and two of the remaining three were eventually struck off charge in 1936. The last aircraft survived a further two years at Felixstowe.
Engine: 3 x RR Buzzard IIMS, 615kW
Take-off weight: 14740 kg / 32496 lb
Empty weight: 9500 kg / 20944 lb
Wingspan: 29.6 m / 97 ft 1 in
Length: 21.3 m / 69 ft 11 in
Height: 8.1 m / 26 ft 7 in
Wing area: 233.3 sq.m / 2511.22 sq ft
Max. speed: 213 km/h / 132 mph
Cruise speed: 175 km/h / 109 mph
Ceiling: 3500 m / 11500 ft
Range w/max.fuel: 2780 km / 1727 miles
Range w/max.payload: 1600 km / 994 miles
Crew: 6


The Baffin was an improved version of the Ripon with a 421kW Bristol Pegasus radial engine in place of the water-cooled Napier Lion. Two prototypes and 33 production Baffins served with a single flight at Gosport for dummy deck-landing and torpedo practice and with Nos 810, 811 and 812 Squadrons on board the aircraft carriers HMS Courageous, Furious and Glorious respectively from 1934 until replaced by Sharks in 1936. One batch of 14 Baffins were shipped to Malta as reserve aircraft when the carriers exercised their squadrons in the Mediterranean.
More than 60 Ripons were re-worked and re-engined as Baffins during 1934-35. Twenty-nine surplus Fleet Air Arm aircraft were sold to the RNZAF during 1937-38 for the Wellington, Christchurch and Auckland Territorial GR Squadrons, which combined for wartime coastal patrols.

The Baffin was taken out of RAF service in 1937.
Engine: 1 x Bristol Pegasus IM-3, 405kW
Take-off weight: 3450 kg / 7606 lb
Empty weight: 1900 kg / 4189 lb
Wingspan: 13.9 m / 45 ft 7 in
Length: 11.6 m / 38 ft 1 in
Height: 4.1 m / 13 ft 5 in
Wing area: 63.4 sq.m / 682.43 sq ft
Max. speed: 218 km/h / 135 mph
Cruise speed: 160 km/h / 99 mph
Ceiling: 4500 m / 14750 ft
Range w/max.payload: 725 km / 451 miles
Engine: Bristol Pegasus II M-3, 580-660 hp.
Max speed: 136 mph.
Service ceiling: 15,000 ft.
Range: 450 miles.
Crew: 2
Armament: 2 mg + 2000 lb bombs.


1932


A single-engine, two-seat biplane naval torpedo bomber. Two prototypes, first flown on 8 March 1932. No production.
M.1/30
Serial: S1640
Cn: 3380/1
1 aircraft ordered from The Blackburn Aeroplane and Motor Co. Ltd, Brough, Yorkshire, to contract 55826/30. First flew 8 March 1932.
M.1/30A
Serial: K3591
Cn: 3900/1
1 aircraft built by The Blackburn Aeroplane and Motor Co. Ltd, Brough, Yorkshire, as a Private Venture. First flew 24 February 1933; to the Air Ministry under contract 244326/33 on 18 May 1933. Originally flew under Class B conditions as B-3
M.1/30A
Engine: 1 x 825hp Rolls-Royce Buzzard IIIMS
Take-Off Weight: 4718 kg / 10401 lb
Empty Weight: 2787 kg / 6144 lb
Wingspan: 15.09 m / 49 ft 6 in
Length: 12.14 m / 39 ft 10 in
Height: 4.45 m / 14 ft 7 in
Wing Area: 60.48 sq.m / 651.00 sq ft
Max. Speed: 229 km/h / 142 mph
Ceiling: 2789 m / 9150 ft
Crew: 2
Armament: 2 x 7.7mm machine-guns, 4 x 250kg bombs or a torpedo


A two-seat (side-by-side) all-metal biplane trainer with a semi-monocoque Alclad fuselage and fabric-covered wings first produced in 1932.
The entire output of 42 aircraft was produced for pilot training at civilian Elementary and Reserve Flying Schools under the RAF expansion scheme. Blind-flying hood, camera-gun or vertical camera were fitted for advanced instruction. All were transferred to Air Training Corps squadrons as instructional airframes in 1942.

B-2
Engine: 1 x De Havilland Gipsy III, 97kW
Take-Off Weight: 839 kg / 1850 lb
Loaded Weight: 533 kg / 1175 lb
Wingspan: 9.19 m / 30 ft 2 in
Length: 7.39 m / 24 ft 3 in
Height: 2.74 m / 8 ft 12 in
Wing Area: 22.85 sq.m / 245.96 sq ft
Max. Speed: 180 km/h / 112 mph
Cruise Speed: 153 km/h / 95 mph
Range W/Max.Fuel: 515 km / 320 miles
Crew: 2

A batch of 32 were ordered by the Fleet Air Arm in August 1924.

1930

