The Development of Halifax Aircraft

The Halifax was initially intended as a twin-engined, medium range bomber (British Air Ministry P 13/36). Handley Page Ltd. designed the HP56 to be fitted with two Rolls Royce Vulture engines but, because the performance of the engines was unsatisfactory, the aircraft was not built. Modifications to the design resulted in a larger aircraft, the HP 57, powered by four Rolls Royce Merlin XX engines. The maiden flight of the Halifax prototype took place in 1939, soon after England declared war on Germany. Production began and the aircraft entered service with the Royal Air Force 35 Squadron at Linton-on-Ouse, Yorkshire, England in November 1940.

Technical Specs:
Type: Four engine long-range heavy bomber
Designed by: Handley Page Ltd. Cricklewood, London, England
Assembled by: Components manufactured by 45 sub-contractors: Handley Page Ltd., Rootes Securities Ltd., English Electric Company, Fairey Aviation, London Aircraft Production Group (all in England)
Production: 1939 through 1946, 6178 aircraft
Variants: Mark I, II and V: Wingspan 98 feet, length 70 feet Rolls Royce Merlin XX 1,100 HP liquid cooled engines All up weight 55,000 lbs (25,000 Kg) Max speed 280 mph (450 km/h) Range 1,900 miles (3000 km)
Mark III, IV and VII: Wingspan 104 feet, length 70 feet Bristol Hercules XVI 1650 HP sleeve valve air cooled engines All up weight 65,000 lbs (29,500 kg) Max speed 270 mph (430 km/h) Range 3,000 miles (4,800 km)
Mark VI and VIII : Wingspan 104 feet, length 70 feet Bristol Hercules 100 1,800 HP sleeve valve air cooled engines All up weight 65,000 lbs (29,500 kg) Max speed 270 mph (430 km/h) Range 3,000 miles (4,800 km)