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Boulton and Paul Overstrand

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Top speed  238 km/h
Length  14 m
Retired  1941
Manufacturer  Boulton Paul Aircraft
Wingspan  22 m
Introduced  1934
First flight  1933
Boulton & Paul Overstrand The last Biplane bomber of the RAF the Boulton Paul Overstrand

The Boulton Paul P.75 Overstrand was the last of the twin-engine biplane medium bombers of the Royal Air Force, a series that had begun during the First World War with the likes of the Vickers Vimy and Handley Page Type O. The Overstrand saw brief service in the late 1930s and by the Second World War, only a few surviving aircraft remained in operation with training units.

Contents

Boulton & Paul Overstrand BoultonPaul P75 Overstrand bomber

Design and development

Boulton & Paul Overstrand The last Biplane bomber of the RAF the Boulton Paul Overstrand

The Overstrand was a development of the Boulton Paul Sidestrand, which had first flown in 1928 and like the Sidestrand was named for a village in Norfolk, home also of Boulton Paul's Norwich factory. The Sidestrand was similar to its First World War predecessors, in that it had open cockpits and hand-operated machine-guns. Unlike its predecessors, the Sidestrand could fly at 140 mph (225 km/h) making operating the guns in exposed positions difficult, particularly in the nose. The Overstrand was fitted with an enclosed and powered nose turret with a Lewis gun, the first RAF aircraft to have a power-operated turret. Rotation was by pneumatic motors, elevation and depression of the gun by hydraulic rams. The cockpit was also enclosed but the dorsal and ventral gun positions remained open, though shielded.

Operational history

Boulton & Paul Overstrand Boulton Paul Overstrand

The first Overstrand flew in 1933 as the Sidestrand Mk IV, powered by two 580 hp (430 kW) Bristol Pegasus IM.3 engines, instead of the 460 hp (340 kW) Bristol Jupiters in the Sidestrand and was capable of 153 mph (246 km/h). The bomb load was also increased to 1,500 pounds (680 kg). The conversion was a success and three more Sidestrands were modified using the 580 hp (430 kW) Bristol Pegasus II.M3. 24 Overstrands were produced and in 1936 began replacing the Sidestrand in No. 101 Squadron RAF, the only Sidestrand squadron) and briefly in No. 144 Squadron RAF, being replaced by Bristol Blenheims in 1938. At the outbreak of the Second World War, eleven Overstrands remained in service and six were used for gunnery training. They remained in operation until May 1941, though flying was limited following the mid-air breakup of Overstrand K8173 on 22 April 1940. Plans were made to develop a version with retractable undercarriage as the P.80 "Superstrand" but the project was abandoned.

Operators

 United Kingdom
Boulton & Paul Overstrand httpsuploadwikimediaorgwikipediacommonsthu
  • Royal Air Force
  • No. 101 Squadron RAF
  • No. 144 Squadron RAF
  • RAF Second line units
  • No. 2 Air Observer School RAF
  • No. 10 Bombing and Gunnery School RAF
  • Balloon Development Unit RAF
  • Army Co-operation Development Unit RAF
  • Accidents and incidents

    A number of Overstrands were destroyed or beyond economic repair in accidents, the type had only two fatal accidents:

  • 11 January 1937 K4564 of 101 Squadron flew into ground in fog at Swanbourne, Buckinghamshire, three crew killed.
  • 22 April 1940 K8173 of 101 Squadron crashed off Chesil Beach, Dorset following an engine fire, three crew killed.
  • Specifications

    Data from the British Bomber since 1914

    General characteristics

  • Crew: three or four; pilot and two–three gunners
  • Length: 46 ft 0 in (14.02 m)
  • Wingspan: 72 ft 0 in (21.95 m)
  • Height: 15 ft 6 in (4.73 m)
  • Wing area: 980 ft² (91.1 m²)
  • Empty weight: 7,936 lb (3,607 kg)
  • Max. takeoff weight: 11,923 lb (5,420 kg)
  • Powerplant: 2 × Bristol Pegasus II.M3 9 cylinder radial engine, 580 hp (433 kW) each
  • Performance

  • Maximum speed: 148 mph (129 knots, 238 km/h) at 6,500 ft (1,980 m)
  • Range: 545 mi (474 nmi, 872 km)
  • Service ceiling: 21,300 ft (6,490 m)
  • Wing loading: 12.2 lb/ft² (59.4 kg/m²)
  • Power/mass: 0.097 hp/lb (0.16 kW/kg)
  • Climb to 6,500 ft (1,980 m): 5 min 24 sec
  • Armament

  • Guns: 3 × .303 in (7.7 mm) Lewis guns in nose turret, dorsal and ventral gun positions
  • Bombs: 1,500 lb (680 kg) bombs (2 × 500 lb/227 kg and 2 × 250 lb/113 kg) and 4 × 20 lb (9 kg) bombs could be carried on fuselage racks by the cockpit and dorsal gun position
  • References

    Boulton & Paul Overstrand Wikipedia


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