Country of Origin Date of First Flight Date of First Delivery:	France May 27th, 1955 April, 1959 (to SAS and Air France)
Engine Type Engine Data	2 Rolls Royce Avon RA.29 Mk 527B 5.17 kN each at 8100 rpm (Total 10.34 kN)
Length / Wingspan / Height Wing Area / Asp Ratio / Sweep Ang Wheel Base / Track Cabin Width	32.01 m / 34.30 m / 8.72 m 146.7 sqm / 8.021 / 20 deg 11.79 m / 5.21 m 3.0 m
Empty weight Max Zero Fuel Max Takeoff Weight Max Landing Weight Max Payload	24185 kg 37000 kg 46000 kg 43800 kg 8290 kg
Typical Cruise Speed Max Speed Approach Speed (flaps 20-35) BFL Takeoff BFL Landning Cruising Altitude Max Altitude Design Range Fuel Capacity Fuel Flow in Cruise Max Passenger Total Built	Mach 0.77 / 300 kt Mach 0.81 / 325 kt 190 kt 1830 m 1800 m 35000 ft 39300 ft 3200 km 19000 litres ca 4000 litres/hr 90 pax 282 (incl 2 prototypes), 85 Type III
References	"Caravelle - The complete story" by John Wegg and other various sources