Second World War

Avro Manchester

A. V. Roe and Company

Bomber Aircraft

The Avro Manchester was introduced in 1940 as the Royal Air Force’s new twin-engined heavy bomber, intended to form the backbone of Bomber Command’s expansion. Powered by Rolls-Royce Vulture engines, it suffered persistent reliability problems that limited operational effectiveness. Withdrawn from frontline service in 1942, its airframe nevertheless provided the foundation for the four-engined Avro Lancaster, which emerged as one of the principal heavy bombers of the Second World War.

Entered service November 1940
Retired June 1942
Max speed 265 mph (426 km/h)
Service ceiling 19,200 ft (5,852 m)
Range 1,200 mi (1,931 km)
Crew 7

The Avro Manchester was conceived as part of the expansion of RAF Bomber Command and entered service in late 1940. Designed to meet Air Ministry Specification P.13/36 as a twin-engined medium bomber powered by Rolls-Royce Vulture engines, it was intended to combine high speed, long range and a substantial bomb load within a relatively compact airframe. In operational use between February 1941 and June 1942, however, these objectives proved difficult to achieve.

During 16 months of operations, the Manchester flew 1,269 sorties with Bomber Command, and 202 examples were built. The expected performance was not realised, largely because the Vulture engine remained unreliable and insufficiently developed. Frequent engine failures contributed to losses and led to the aircraft’s withdrawal once more dependable four-engined heavy bombers entered service. Although judged unsuccessful as a bomber, the Manchester airframe formed the structural basis for the Avro Lancaster. Its development illustrates the transition within Bomber Command from twin-engined types to four-engined heavy bombers from 1942 onward. It highlights the risks associated with introducing new technology before it has fully matured.

Origins And Development Of The Manchester

The origins of the Avro Manchester lay in Air Ministry Specification P.13/36, issued in September 1936. This specification called for a new twin-engined medium bomber intended to exceed the performance of existing types such as the Vickers Wellington and Handley Page Hampden. Designers were expected to use the new 24-cylinder Rolls-Royce Vulture engine, then still at an early stage of development.

A.V. Roe & Co. responded with the Avro 679 design. Handley Page initially proposed the H.P.56 but later redirected its efforts towards a four-engined design that became the Halifax, leaving Avro as the sole manufacturer for the P.13/36 requirement. Reflecting the urgency of pre-war rearmament, the Air Ministry ordered two prototypes and an initial production batch of 200 aircraft on 1 July 1937, before the first prototype had flown.

The first prototype, L7246, flew on 25 July 1939. Early trials revealed instability in flight, leading to a 10-foot increase in wingspan to improve handling. The second prototype, L7247, incorporating the extended wing, flew on 26 May 1940. Production was centred at Avro’s factory at Chadderton near Oldham. The first production Manchester Mk I reached the Aeroplane and Armament Experimental Establishment on 5 August 1940.

Early aircraft featured a central tail fin flanked by two smaller fins. Directional stability remained unsatisfactory, and the Manchester Mk IA deleted the central fin and enlarged the twin endplate fins and rudders, a configuration later associated with the Lancaster.

Technical Specifications And The Vulture Engine Problem

The Avro Manchester was a mid-wing, twin-engined bomber with an all-metal stressed-skin structure. The standard crew of six comprised two pilots seated side by side, a navigator who also acted as bomb aimer, a wireless operator who could serve as a gunner, and two additional gunners. The fuselage contained a bomb bay and three power-operated turrets, while the wings housed fuel tanks supplying the two Vulture engines.

Defensive armament consisted of eight 0.303-inch Browning machine guns mounted in nose, dorsal and tail turrets. For its size, the Manchester could carry a substantial bomb load, and the airframe itself proved structurally sound.

The principal weakness lay in the Rolls-Royce Vulture engine, an X-24 configuration combining two Peregrine V-12 cylinder blocks on a common crankcase. Although designed to deliver high power from a compact installation, it encountered persistent technical difficulties in service. Squadrons reported chronic lubrication problems leading to bearing failures, cooling issues and overheating during prolonged high-power operation, and repeated in-flight stoppages alongside a consistent failure to achieve the intended power output.

For a fully loaded Manchester, the loss of one engine significantly reduced performance, particularly during climb or at low altitude. In adverse weather or when damaged by enemy fire, the aircraft could struggle to maintain height on a single engine. These issues led to the termination of the Vulture programme and prompted reconsideration of how the Manchester airframe might be re-engined.

Operational Service And Squadron Experience

The Avro Manchester entered front-line service with RAF Bomber Command in late 1940. No. 207 Squadron received the type at RAF Waddington on 8 November 1940. After conversion training, the squadron flew the first operational Manchester mission on the night of 24 February 1941 against the German cruiser Admiral Hipper at Brest.

No. 97 Squadron at RAF Coningsby followed, conducting its first Manchester sortie on 8 April 1941 against targets at Kiel. Additional units, including No. 61 Squadron and No. 50 Squadron, subsequently re-equipped with the type. The aircraft was employed on bombing operations against targets in Germany and occupied Europe, frequently at long range and under night conditions.

Across Bomber Command, the Manchester completed 1,269 operational sorties. Its final operational appearance occurred during a raid on Bremen on 25 June 1942. By that stage, four-engined bombers such as the Halifax and the Lancaster were entering service in increasing numbers. Their greater reliability and improved performance made continued use of the Manchester difficult to justify.

Accounts from squadrons indicate the operational strain imposed by engine unreliability. Ground crews devoted considerable effort to maintaining serviceability, while aircrew undertook missions aware of the possibility of mechanical failure. These factors influenced morale and contributed to the type’s reputation.

Courage Under Adversity: Notable Incidents

The operational record of the Avro Manchester includes several incidents that illustrate the risks its crews face. On the night of 2 September 1941, a Manchester of No. 61 Squadron was lost during a raid on Berlin. On board were the station commander of RAF North Luffenham and the commanding officer of No. 61 Squadron. The aircraft was hit by anti-aircraft fire and crashed near Berlin, resulting in the loss of all crew members. Following this event, RAF policy was amended to restrict senior officers from flying together on operations without specific authorisation.

On the night of 9/10 January 1942, a Manchester of No. 61 Squadron experienced an engine fire shortly after take-off. Although the fire was extinguished, the aircraft continued to lose height. The captain maintained control, allowing the majority of the crew to abandon the aircraft before attempting a forced landing. The two pilots were killed in the subsequent crash. The incident demonstrated the limited margin available when an engine failure occurred with a full bomb load.

The most notable award associated with the type was the posthumous Victoria Cross granted to Flying Officer Leslie Thomas Manser of No. 50 Squadron. During a raid on 30 May 1942, his aircraft sustained severe damage from anti-aircraft fire. He retained control long enough for his crew to escape before the aircraft crashed, at the cost of his own life.

These incidents form part of the broader operational history of the type and reflect the hazards of night bombing operations during this period.

From Failure To Legend: The Lancaster Evolution

Despite the shortcomings of the Avro Manchester, confidence remained in the underlying airframe. Consideration was given to a Manchester Mk II powered by alternative engines, such as the Bristol Centaurus or Napier Sabre, though these versions did not proceed to flight.

The decisive development was the Manchester Mk III project, which replaced the two Vulture engines with four Rolls-Royce Merlin engines mounted on a new, larger wing. The prototype, converted from a Manchester airframe, flew in January 1941 and demonstrated clear improvements in performance, reliability and bomb-carrying capacity.

This aircraft entered production under a new designation as the Avro Lancaster. The Vulture programme was abandoned, and manufacturing effort was redirected to Merlin production and Lancaster assembly. A total of 7,377 Lancasters were built, while Manchester production concluded at 202 aircraft, including the two prototypes.

No complete examples of the Avro Manchester are known to survive. Its significance lies primarily in its role as the immediate predecessor of the Lancaster and as part of Bomber Command’s transition to four-engined heavy bombers.

Avro Manchester — Technical Specification
Dimensions
Wingspan90 ft 1 in (27.46 m)
Length70 ft 4 in (21.44 m)
Height19 ft 9 in (6.02 m)
Wing area840 sq ft (78.0 m²)
Weights
Empty weight33,200 lb (15,059 kg)
Max takeoff weight51,000 lb (23,133 kg)
Max bomb load10,350 lb (4,695 kg)
Performance
Maximum speed265 mph (426 km/h)
Cruise speed200 mph (322 km/h)
Service ceiling19,200 ft (5,852 m)
Range1,200 mi (1,931 km)
Powerplant
Engines2 × Rolls-Royce Vulture X liquid-cooled X-24
Power1,760 hp (1,312 kW) each
Armament
Guns8 × .303 in Browning machine guns in nose, dorsal, and tail turrets
Bombs / weapons10,350 lb (4,695 kg)
1939
First flight - prototype L7246, 25 July
1940
Entered service - No. 207 Squadron begins operational conversion
1941
Operational deployment - night bombing raids over Germany and occupied Europe
1942
Production curtailed following engine reliability issues; transition to four-engined development
1942
Withdrawn from frontline RAF service
Mk.I
Principal production variant powered by two Rolls-Royce Vulture X engines; formed the basis of operational RAF service between 1940 and 1942.
Mk.IA
Improved production standard with structural refinements and minor equipment changes during early service.