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The prototype of this airliner flew for the first time on 29 June 1962. The VC10 entered service on BOAC's route to West Africa on 29 April 1964. Four production variants and a modification of the prototype were produced: the Model 1101, of which 12 went to BOAC accommodated 16 first-class and 93 economy passengers; the Model 1102, of which two went to Ghana Airways, one with a large hydraulically operated cargo door between the standard passenger doors and both with 4% chord leading-edge extension from wing root to fence; the Model 1103, of which three went to British United Airways with cargo door and extended leading edge; Model 1106, of which 14 went to RAF Air Support Command with cargo door, folding hatracks, machined cargo floor, extended leading edge, 97kN Conway RCo.43 Mk 301 turbofans and fin fuel tank; and the Model 1109, the prototype brought up to airline standard for Laker Airways, with the Model 1106 wing. Standard engines for the VC10 were four 90.6kN Rolls-Royce Conway RCo. 42 turbofans in lateral pairs on each side of the rear fuselage. RAF basic transport version designated VC10 C.1. C.2 is the unconfirmed designation of flight refuelling tanker conversions of five VC10 and four Super VC10.
 | A three-view drawing (1000 x 726) |
| CREW | 4-6 |
| PASSENGERS | 108-151 |
| ENGINE | 4 x turbo-jet RR "Conway RCo-42", 93.4kN |
| WEIGHTS |
| Take-off weight | 141521 kg | 312002 lb |
| Empty weight | 67094 kg | 147918 lb |
| DIMENSIONS |
| Wingspan | 44.6 m | 146 ft 4 in |
| Length | 48.4 m | 158 ft 10 in |
| Height | 12.0 m | 39 ft 4 in |
| Wing area | 264.3 m2 | 2844.90 sq ft |
| PERFORMANCE |
| Cruise speed | 915 km/h | 569 mph |
| Range w/max.fuel | 8328 km | 5175 miles |
| Range w/max.payload | 6680 km | 4151 miles |
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