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Explore the Avro Manchester, the RAF bomber whose unreliable Vulture engines cut short its service but led directly to the Lancaster.
The Avro Manchester was an ambitious twin-engined bomber developed for RAF Bomber Command under Air Ministry Specification P.13/36. It entered operational service in February 1941, but persistent difficulties with its Rolls-Royce Vulture engines shortened its career. The Manchester nevertheless undertook demanding raids against targets in Germany and occupied Europe, and its airframe provided the foundation for the four-engined Avro Lancaster.
Its history deserves to be understood on its own terms. Manchester crews flew in dangerous conditions while engineers and ground staff struggled to improve reliability. The aircraft was withdrawn from front-line bombing in June 1942, but the lessons of its development helped shape one of the RAF’s most important wartime aircraft.
In September 1936, the Air Ministry sought a new twin-engined bomber capable of carrying a substantial load over long distances. Avro proposed the Type 679, powered by two Rolls-Royce Vulture engines. Handley Page initially pursued a competing twin-engined design before developing the four-engined Halifax. The urgency of RAF rearmament led to orders for Manchester aircraft before the prototype had flown.
The first prototype, L7246, flew on 25 July 1939. Trials identified handling and stability problems, prompting an increase in wingspan and revisions to the tail. The second prototype, L7247, flew in May 1940. Early Manchester Mk I aircraft had three vertical fins, including a central fin, while the Mk IA adopted enlarged twin fins and rudders. The latter arrangement became familiar on the Lancaster.
The Manchester was an all-metal mid-wing monoplane with a retractable undercarriage, an internal bomb bay and powered gun turrets. The normal operational crew is generally given as seven, although the complement varied with duties and particular flights. The crew worked from separate flying, navigation, wireless, bombing and defensive positions rather than a simple conventional side-by-side two-pilot cockpit arrangement.
The developed aircraft had a wingspan of approximately 90 ft and a length of about 69 ft 6 in. Its two Vulture engines were intended to provide substantial power, and published maximum speeds are commonly around 265 mph. The Manchester could carry a large bomb load, although actual loads depended on fuel, range and operating conditions. Defensive armament typically involved .303-inch Browning machine guns in nose, upper and tail positions, with variations between production aircraft and modifications.
The Vulture was a 24-cylinder X-configuration engine derived from Rolls-Royce Peregrine technology. It promised high power from a relatively compact installation, but its development was troubled by lubrication and bearing failures. Cooling and overheating problems also affected serviceability. Repeated engine stoppages undermined confidence and placed heavy demands on maintenance crews.
For a loaded twin-engined bomber, the failure of one engine removed half its installed power. The Manchester could struggle to maintain height after an engine failure, particularly during take-off or when carrying a substantial fuel and bomb load. Jettisoning bombs or attempting an emergency landing could become necessary. The Vulture’s problems were therefore operational hazards, not merely inconveniences for engineers.
No. 207 Squadron received Manchesters at RAF Waddington in November 1940 and mounted the type’s first operational mission on the night of 24–25 February 1941 against the German cruiser Admiral Hipper at Brest. No. 97 Squadron followed, with Nos. 61 and 50 Squadrons also operating the type. Manchester crews attacked ports, industrial centres and other targets during the expanding night offensive.
The Manchester is commonly credited with 1,269 operational aircraft sorties, a total that should not be confused with the number of separate raids. Its final front-line operation is generally associated with the Bremen raid of 25–26 June 1942. By then the Lancaster and other four-engined aircraft were entering service in increasing numbers, offering Bomber Command a more promising combination of load, range and reliability.
During an operation against Berlin on the night of 2–3 September 1941, Manchester L7388 of No. 61 Squadron was lost. Among those aboard were senior officers associated with RAF North Luffenham and the squadron. All seven men died. The loss demonstrated the risks faced by senior personnel who continued to participate in operational flying.
Some accounts associate the incident with later restrictions on senior officers flying together. Without a verified contemporary order, however, that claimed RAF-wide policy change should be treated cautiously rather than stated as an established direct consequence.
On 9 January 1942, Manchester R5789 of No. 61 Squadron suffered a serious engine emergency shortly after take-off. The aircraft lost height, and most of those aboard escaped by parachute. The two pilots, Pilot Officer Douglas Spencer Matthews and Pilot Officer Thomas Ivor Ravenhill Wilson, were killed when the aircraft crashed near Tidworth.
The flight carried more people than the normal crew establishment, illustrating why a particular accident’s occupancy should not be used to define the standard Manchester crew. The incident also revealed the narrow margin available to a heavily laden bomber when one of its two engines failed.
One of the Manchester’s most significant operational stories concerns Flying Officer Leslie Thomas Manser of No. 50 Squadron. On the night of 30–31 May 1942, he captained Manchester L7301 during Operation Millennium, the first Thousand Bomber Raid, against Cologne. His aircraft suffered severe damage from searchlights and anti-aircraft fire during the mission.
Manser continued the operation, but the damaged aircraft encountered worsening engine trouble on the return flight. He ordered his crew to abandon the Manchester and remained at the controls while they escaped. The aircraft crashed in Belgium and Manser was killed. His posthumous Victoria Cross recognised his exceptional courage and determination to give his crew a chance of survival. The episode remains an important part of the Manchester’s history, independently of the later fame of the Lancaster.
Avro investigated alternative engines and configurations as the Vulture’s limitations became clear. The decisive development was the Manchester Mk III project, with four Rolls-Royce Merlin engines mounted on a redesigned, larger wing. Prototype BT308 flew on 9 January 1941. The new arrangement offered substantially improved reliability and performance, and the aircraft entered production as the Avro Lancaster.
The Lancaster retained elements of the Manchester’s fuselage, bomb-bay concept and general design, but its wing and powerplant arrangement represented a major change. It was therefore both a direct descendant and a substantially improved aircraft. Its rapid development was made possible in part by work already completed on the Manchester structure.
Manchester production is usually given as 202 aircraft including prototypes, although published counts can differ according to which completed airframes are included. No complete Manchester is known to survive. Its operational career lasted approximately sixteen months, and the type disappeared from front-line bombing as Lancaster production accelerated in 1942.
The Manchester should be remembered neither simply as a failed aircraft nor only as the Lancaster’s predecessor. It was an operational bomber whose crews endured the hazards of night warfare and serious mechanical uncertainty. At the same time, the experience of its development showed the danger of depending on an immature engine programme. The redesign that produced the Lancaster became one of the most consequential engineering decisions in Bomber Command’s history.
| Dimensions | |
| Wingspan | 90 ft 1 in (27.46 m) |
| Length | 70 ft 4 in (21.44 m) |
| Height | 19 ft 9 in (6.02 m) |
| Wing area | 840 sq ft (78.0 m²) |
| Weights | |
| Empty weight | 33,200 lb (15,059 kg) |
| Max takeoff weight | 51,000 lb (23,133 kg) |
| Max bomb load | 10,350 lb (4,695 kg) |
| Performance | |
| Maximum speed | 265 mph (426 km/h) |
| Cruise speed | 200 mph (322 km/h) |
| Service ceiling | 19,200 ft (5,852 m) |
| Range | 1,200 mi (1,931 km) |
| Powerplant | |
| Engines | 2 × Rolls-Royce Vulture X liquid-cooled X-24 |
| Power | 1,760 hp (1,312 kW) each |
| Armament | |
| Guns | 8 × .303 in Browning machine guns in nose, dorsal, and tail turrets |
| Bombs / weapons | 10,350 lb (4,695 kg) |
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