The tailplane’s length was feet, which was hydraulically operated, and covered a total area of 638 square feet. Its two-section, electro-hydraulically actuated elevators featured a 146-square-foot place themselves. Its vertical fin, which had its square-foot room, was equipped with a three-section independently controlled rudder. It provided them with the height of in height overall Vessel Cargo Hold Cleaning. The power was supplied by four Rolls Royce thrust pounds of capacity with a thrust reverser with low bypass rate turbofans housed in drag-reducing nacelles placed in pairs on the forward fuselage. The clean high-flapped wing and its engine capabilities allowed Vickers to design a plane that performed superior to the currently in use.

Fuel was stored in tanks and pumped to engines via four integral wing tanks, whose total capacity was Imperial gallons. An aft inside section on each wing introduced fuel. The oil capacity of the branch was 19.5 Imperial gallons. The VC10 rests on a traditional tricycle, which was hydraulically operated undercarriage. The dual-wheel nose gear featured a tire size and was retracted to the rear of its fuselage. Its two main gear units with quad-wheels with tire size extended laterally into the fuselage bays. All of them were fitted with Dunlop wheels with tubeless tires, Minaret anti-skids, and hydraulic disc brakes.

The entry was through two forward and port doors for passengers. Both were in front of the wing. Meanwhile, galley service access was via two 5.62 feet starboard doors, one of which was located forward of the wing, while the other was behind it Vessel Blasting and Painting. The aircraft was typically operated by a crew of three, comprising Captain, a pilot officer, and the chief engineer; however, there was also the option of observers and a navigator should the pilot choose to use one. The cabin was long, 1 foot wide, and feet high. The house, which has an area of 1,000 square feet, was typically equipped with a galley that was two units and two toilets in the forward section, 135 six-abreast seating in a three-three configuration, and a second galley with two teams and three lavatories at the rear. While its maximum individual-class capacities were 151, the cabin could accommodate a variety of classes, seating angles, and abreast configurations, precisely four across first class and five across the business class in three-two or two-three configurations and six-abreast coach configurations.

The two lower cargo and baggage storage areas, located in front of the wing’s wing, were equipped with a large 4-by-5-foot forward hatch on the starboard side and had a 615 cubic-foot volume. The second one, located behind the wing, was a foot hatch in the direction of the starboard side and was cubic feet in size. The plane was not equipped with an auxiliary power unit that powered the cabin air conditioning and engine start-ups. With pounds of payload and gross weights, the Standard VC10 required a runway to take off from. The sea-level climb rate was fpm, and its ceiling of service is Vessel Blasting and Painting. The maximum speed of its cruising was 568 mph. However, its economy-oriented cruising speed, which was decreased per hour. The range varied with the payload and fuel ratios, reaching the former’s highest and when using the maximum in the other. The type needed a runway of feet to land. Piloted by Chief Test Pilot Bryce, Co-pilot Brian Trishaw, and Flight Engineer Bill Cairns, aircraft from Brookland’s took the brief flight to Wisely to conduct further tests.

It was, however, equipped with several modifications, which included a narrower wingspan which was 140.2 feet, the removal from the leading edge of slats, and a gross weight of pounds. The slats and wing fences that provide the upper airfoil with airflow guidance were then put into place after early test flights identified stall and drag problems. The first version of the production was manufactured in a new assembly facility in Weighbridge and registered as G-ARVA first flew five months after on however, it was fitted with Kuchean wings that increased the airfoil size to square feet and increased payload capacity and weight to pounds.