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Capacity: 100 passengers, and 2.5 tonnes of
cargo.
Seating: 100 seats, two either side of the aisle, with a 37 ins
(94 cm) pitch. The front cabin has 40 seats, and the rear cabin 60
seats, both offering a single-class "R", or supersonic, brand of
service
Range: 4,300 miles (6,880 kms)
Engines: Four Rolls-Royce/SNECMA Olympus 593s, each producing
38,000 lbs thrust with reheat
Take-off speed: 220 knots (250 mph 400 kph)
Cruising speed: 1,350 mph (2,150 kph/Mach Two), at 60,000 ft
(18,181 m)
Landing speed: 187 mph (300 kph)
Autoland capability: Category 3 (Decision height 15 ft, landing
runway visual range 200
metres, and take-off runway visual range 150 metre)
Length: 203 ft 9 ins (62.1 m)
Wingspan: 83 ft 8 ins (25.5 m)
Height: 37 ft 1 ins (11.3 m)
Fuselage width: 9 ft 6 ins (2.9 m)
Fuel capacity: 26,286 Imperial gallons (119,500 litres/95,600 kgs)
Fuel consumption: 5,638 Imperial gallons (25,629 litres/20,500 kgs)
per hour
Maximum take-off weight: 408,000 lbs (185 tonnes)
Landing gear: Eight main wheel (tyre pressure 207 lbs sq ins), two
nose wheels (tyre pressure 181 lbs sq ins)
Flight crew: Two pilots, one flight engineer
Cabin crew: Six
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