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Armstrong Whitworth A.W.38 Whitley

Operation Biting: On the night of February 27, 1942, Whitleys of No. 51 Squadron RAF drop sticks of parachutists near the German radar site at Bruneval on the French coast. The Whitley did much to assist the early development of British airborne forces, taking part in a few notable actions before replacement by purpose-built transports.

Country of Origin:

Great Britain

Manufacturer:

Armstrong Whitworth Ltd.

Designer:

John Lloyd

Major Variants:

Mk.I, Mk.II, Mk.III, Mk.IV, Mk.IVA, Mk.V, Mk.VII

Role:

Medium bomber, troop transport, glider tug, maritime patrol aircraft, trainer.

Operated by:

Great Britain

First Flight:

March 17, 1936 at Whitley Aerodrome, Yorkshire.

In Service:

March 19, 1937 with No 10 Squadron RAF at Dishforth, Yorkshire.

Number Built:

Total: 1,814. Mk.I (34), Mk.II (46), Mk.III (80), Mk.IV (33), Mk.IVA (7), Mk.V (1,466), Mk.VII (146).

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Overview

When Britain began rearming in the mid thirties, a high priority was given to replacing the RAF’s fleet of obsolescent biplane bombers. In 1934, with the political situation in Europe worsening and the newly ordered Wellington and Hampden bombers still years away from production. Therefore it was decided to order lower performance night bomber as a stopgap. As with many previous RAF bombers the new aircraft was also required to be a transport, able to fly troops to trouble spots in the Empire and then support them from the air.

Armstrong Whitworth Ltd. was chosen to build the new aircraft to specification B.3 / 34. By adapting their existing A.W. 23 bomber / transport design, they were able to get their prototype A.W 38 flying in only 18 months. Named Whitley after the district in which it was built, the new bomber was an 84 ft (25.6 m) span monoplane with retracting undercarriage and powered by two 795 hp (593 kW) Armstrong Siddeley Tiger IX 14 cylinder radials driving three bladed variable pitch propellers. Hand traversed turrets, each with a single drum-fed Vickers .303 in (7.7 mm) machine gun were provided front and rear and 3,365 lb (1,526 kg) of bombs could be accommodated in two fuselage and fourteen small bomb bays in the wings.

The speed of the aircraft’s construction had led to some compromises in its design. Although the fuselage was a modern aluminum monocoque design, the wing wasn’t. It was built in three pieces around a huge box spar; with structures formed from aluminum sections attached front and rear, which were then clad in a mixture of non-structural aluminum sheets and fabric. This was a heavier arrangement than the more modern, but less understood stressed skin construction. The wing was also set at a huge incidence angle of 8.5 degrees to reduce the aircraft’s angle of attack while landing. The late addition of hydraulic landing flaps had made this unnecessary, but it was by then too late to change. In level flight this high wing incidence caused the fuselage to fly several degrees nose down, thereby increasing drag.

Other than excessive directional stability the Whitley was considered easy to fly, if a little vague on the controls. It was therefore rushed into service largely unchanged. No. 10 Squadron RAF received their first Mk.Is in March 1937, only a year after the prototype’s first flight and well over a year before the Wellington and Hampden became operational. Even in 1937 the Whitley’s slow top speed of only 192 mph (309 km / h) and poor defensive armament made it too vulnerable to operate by day. As a night bomber however it was considered adequate and its performance was far better than the aircraft it was replacing, the biplane Heyford.

Late production Mk.Is featured increased dihedral, while further development of the Whitley centered on improving its engines and defensive firepower. The Mk.II’s 845 hp (630 kW) Tiger engines incorporated two speed superchargers, boosting top speed to 215 mph (346 km / h). The Mk.III added hydraulically powered turrets to the nose and belly, the latter a retractable “dustbin” type with two .303 in (7.7 mm) belt-fed Browning machine guns.

The first major upgrade of the Whitley was the Mk.IV, which entered service in May 1939. New 1,030 hp (768 kW) Rolls Royce Merlin inline engines and constant speed propellers increased its top speed to 245 mph (394 km / h). The new engines also caused a vicious swing to port on takeoff and made the aircraft directionally unstable in some conditions. The ineffective dustbin turret was removed, but a new hydraulically powered rear turret armed with four Browning .303 in (7.7 mm) machine guns more than made up for this. These features were carried over to the Mk.IVA and then the Mk.V, which was to become the major production variant. The Mk.V featured an increased fuel capacity as well as de-icing equipment. Despite 1,075 hp (802 kW) Merlin X engines, increased weight reduced its top speed to 230 mph (370 km / h). These successive increases in power allowed the later marks of Whitley to carry ever-increasing bomb loads. The Mk.V could carry up to 7,373 lb (3,344 kg) of ordnance over short ranges, more than double the load of the Mk.I.

When war was declared on 3rd September 1939 the RAF initially employed their Whitleys dropping propaganda leaflets over Germany by night. Terrified of Luftwaffe reprisals, Allied governments had forbidden bombing the German mainland. These restrictions weren’t lifted until March 1940, when two squadrons of Whitleys opened the bombing campaign against Germany, targeting a seaplane base at Hornum. The Whitley was also the first aircraft to bomb Italy on June 11 / 12, the night after they entered the war. Over the next two years the Whitley saw extensive use in the night offensive against German cities, although the lack of any sort of electronic bombing aids meant the bombing was often highly inaccurate. As Germany introduced radar guided nightfighters and searchlights, losses on these missions mounted. So in May 1942 as the new better performing four engine “heavies” arrived, the RAF withdrew the Whitley from bombing operations.

Since 1939 Whitley squadrons had been transferred both temporarily and permanently to Coastal Command to help in the fight against the U Boat. Like most of Coastal Command, they initially had little success in this role. Even when they could find a U Boat, their anti-submarine bombs were inaccurate and ineffective. Modified naval depth charges replaced these from late 1940 and proved a far more effective weapon. Then in late 1941 the Mk.VII Whitley was introduced specifically for the maritime patrol role, equipped with long-range internal tanks and A.S.V. Mk.II radar. It was a Mk.VII Whitley that scored the first radar assisted kill of a U Boat on November 30, 1941, U 206 being the victim. Although the Whitley served in Coastal Command until early 1943, this was to be its only U Boat kill.

The Whitley also saw extensive use in the paratrooper schools from 1940, training the newly formed parachute brigades. The ten paratroopers would each sit on the edge of a hole under the rear fuselage originally used for the underside turret and drop through, five from ahead of the hole and five from behind. Dropping from a Whitley could be hazardous though. The five men dropping from the rear tended to tumble, since they hit the slipstream facing forward. This tumbling could cause a chute not to deploy properly, with fatal results for the paratrooper.

Nevertheless Whitleys were employed on two of Britain’s first paratrooper raids. On Feb. 10, 1941 eight Whitleys of 78 Squadron took off from Malta on Operation Colossus. They were carrying 38 men from No. 11 SAS Battalion, who were successfully dropped by night near their target, the Tragino Aqueduct in Italy. All the SAS men were later captured, but not before they had blown up the aqueduct with explosives.

The second raid, Operation Biting, took place on the night of February 27, 1942. Twelve Whitleys of No 51 Squadron dropped 120 men from the 2nd Battalion, The Parachute Regiment onto the Bruneval radar site near the French city of Le Havre. After a brief but heavy firefight that left three raiders dead, the station was captured and the Wurzburg radar stripped of top-secret equipment. The raiders and their plunder were then picked up by Royal Navy landing craft and returned safely to Britain.

Production of the Whitley ended in July 1943 by which time 1,814 had been made. They served on for a while as crew trainers, transport aircraft and glider tugs, until replaced by more modern aircraft such as the C47 Dakota.

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Variants

Type

Number Built

Remarks

A.W.38

2

A prototype twin-engine, five-man medium bomber / transport derived from the unsuccessful A.W.23 transport. Its fuselage was built using a double skin made of aluminum alloy sections. The wing was formed from a large box section spar, with its remaining pressed alloy structure clad in alloy sheet and fabric. Power was from two 795 hp (593 kW) Armstrong Siddeley Tiger IX 14 cylinder radial engines driving three bladed two-pitch propellers. Manually rotated turrets, each with a single drum-fed .303 in (7.7 mm) Vickers gun were fitted front and rear. Its maximum bomb load of 3,365 lb (1,526 kg) was split between two fuselage bays and fourteen small wing bays.

Mk.I

34

Similar to the A.W. 38 prototypes, except for some increased dihedral added to improve stability.

Mk.II

46

Similar to the Mk.I except for new two speed supercharged A.S. Tiger VIII engines of 845 hp (630 kW) and increased all up weight.

Mk.III

80

To improve the Whitley’s defenses, a Nash and Thompson hydraulically powered turret was fitted at the front. A “dustbin” retractable under turret with two .303 in (7.7 mm) Browning guns was also fitted, while the rear turret was unchanged. Dihedral was again increased, protruding bomb aimer glazing and improved bomb racks fitted.

Mk.IV

33

Liquid cooled 1,030 hp (768 kW) Rolls Royce Merlin IV engines driving Rotol constant speed propellers gave much improved performance to this variant, at the cost of some directional instability. A new Nash and Thompson hydraulically powered rear turret was fitted to most Mk.IVs, housing four .303 in (7.7 mm) belt-fed Browning guns. The “dustbin” turret was deleted from this and all subsequent Whitley marks.

Mk.IVA

7

Similar to the Mk.IV except for the more powerful 1,075 hp (802 kW) Rolls Royce Merlin X engines.

Mk.V

1,466

Similar to the Mk.IVA except for a lengthened rear fuselage, designed to improve the rear gunner’s field of fire. The tailfins and rudders were revised; de-icing gear was fitted and extra fuel tanks fitted.

Mk.VII

146

Essentially this was a Mk.V modified as a maritime patrol aircraft. Mk.II ASV radar was fitted, its dipole aerials protruding from above and to the sides of the rear fuselage, as well as below the wings. Bomb bay fuel tanks were fitted as standard, increasing total capacity to 969 gallons (4,393 L). It proved to be a dangerously unstable aircraft when flying at its maximum permitted weight.

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Specifications

Model

Mk.I

Mk.V

Mk.VII

First Flight

Unknown

Unknown

Unknown

In Service

March 1937

August 1939

Late 1941

Crew

Five: Pilot; Navigator / Bomb Aimer; Radio Operator; Rear Gunner; Front Gunner.

Five: Pilot; Navigator / Bomb Aimer; Radio Operator; Rear Gunner; Front Gunner.

Six: Pilot; Navigator / Bomb Aimer; Radio Operator; Radar Operator; Rear Gunner; Front Gunner.

Dimensions

Span

84 ft (25.6 m)

84 ft (25.6 m)

84 ft (25.6 m)

Length

69 ft 3 in (21.2 m)

72 ft (21.95 m)

72 ft (21.95 m)

Height

15 ft (4.58 m)

15 ft (4.58 m)

15 ft (4.58 m)

Wing area

1,138 sq ft (122.5 sq m)

1,138 sq ft (122.5 sq m)

1,138 sq ft (122.5 sq m)

Powerplant

Type

Armstrong Siddeley Tiger IX

Rolls Royce Merlin Mk.X

Rolls Royce Merlin Mk.X

Cubic Capacity

1995 cu in (32.7 l)

1649 cu in (27 l)

1649 cu in (27 l)

Cylinders

14

12

12

Horsepower

795 hp (593 kW)

1,075 hp (802 kW)

1,075 hp (802 kW)

Weights and Loads (note - these figures vary for individual aircraft, and are often not directly comparable)

Weight (empty)

14,275 lb (6,475 kg)

19,350 lb (8,777 kg)

19,605 lb (8,893 kg)

Weight (maximum loaded)

23,500 lb (10,660 kg)

33,500 lb (15,196 kg)

33,950 lb (15,400 kg)

Performance (note - these figures vary for individual aircraft, and are often not directly comparable)

Maximum speed at [height]

192 mph at 7,000 ft (309 km / h at 2,134 m)

230 mph at 16,400 ft (370 km / h at 4,999 m)

 215 mph at 16,400 ft (346 km / h at 4,999 m)

Stalling speed

Unknown

65 mph (105 km / h)

65 mph (105 km / h)

Climb to [height]

27 min 24 sec to 15,000 ft (4,572 m)

16 min to 15,000 ft (4,572 m)

12 min to 12,000 ft (3,658 m)

Service ceiling

19,200 ft (5,852 m)

26,000 ft (7,925 m)

20,000 ft (6,096 m)

Range

1,250 miles (2,012 km)

1,500 miles (2,414 km)

2,300 miles (3,701 km)

Armament and Equipment

Radio

Unknown

Unknown

Unknown

Bombsight

Mk.VIIc

Mk.VIIc or Mk.IXc

Low Level Mk.II or Mk.III

Defensive Armament

Manually traversed nose and tail turrets each mounted a single .303 in (7.7 mm) Vickers K gun with 300 rpg.

A single .303 in drum fed Vickers gun with 300 rpg in the nose turret. Four .303 in (7.7 mm) Browning machine guns with 1,000 rpg in the rear turret.

A single .303 in drum fed Vickers gun with 300 rpg in the nose turret. Four .303 in (7.7 mm) Browning machine guns with 1,000 rpg in the rear turret.

Offensive armament

Up to 3,365 lb (1,526 kg) of ordnance.

Up to 7,373 lb (3,344 kg) of ordnance. Each fuselage bay could hold 2,000 lb (907 kg), with a single 250 lb (113 kg) bomb in each of fourteen wing bays.

Up to 5,993 lb (2,718 kg) of ordnance. Usual load two or four 420 lb (191 kg) depth charges plus extra fuel in bomb bay tanks.

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