Designed to contest with narrow body airliners such as Boeing 707 and Douglas DC-8, the Convair 880 is an American single-aisle jetliner manufactured by Convair. It is compact in size but flies faster compared to other competing aircraft of its kind. With a speed of 615 miles per hour, the Convair 880 has been recorded as the fastest jet transport in the whole world.

United States
1959 to: 1962
4x General Electric CJ-805-3
11,650 pound-force
Max Cruise Speed:
535 knots
991 Km/h
Approach Speed (Vref):
139 knots
Travel range:
2,472 Nautical Miles
4,578 Kilometers
Fuel Economy:
Service Ceiling:
41,000 feet
Rate of Climb:
3000 feet / minute
15.24metre / second
Take Off Distance:
2670 metre - 8,759.74 feet
Landing Distance:
1900 metre - 6,233.52 feet
Max Take Off Weight:
83,688 Kg
184,499 lbs
Max Landing Weight:
62,000 Kg
136,685 lbs
Max Payload:
30,688 Kg
67,655 lbs
Fuel Tank Capacity:
10,584 gallon
40,065 litre
Baggage Volume:
24.43 m3 / 863 ft3
Seats - Economy / General:
110 seats
Seats - Business Class:
Seats - First Class:
Cabin Height:
1.8 metre - 5.91 feet
Cabin Width:
3.27 metre - 10.73 feet
Cabin Length:
26 metre - 85.30 feet
Exterior Length:
39.42 metre - 129.33 feet
Tail height:
11.06 metre - 36.29 feet
Fuselage Diameter:
3.5 metre - 11.48 feet
Wing Span / Rotor Diameter:
36.58 metre - 120.01 feet
Wing Tips:
No Winglets

Blog Mentions

Blog posts that mention the Convair 880:

Convair 880 Production and Development

In April 1956, the aircraft manufacturing company Convair started to develop a medium range aircraft for commercial transport. The aircraft went through several renaming such as Skylark, Golden Arrow, and Convair 600 before it was renamed as the Convair 880.

On January 57 1959, the Model 22 initial production type took its first flight.

The finishing assembly of the aircraft occurred in San Diego, California at the Convair headquarters.

On May 15 1960, the aircraft entered into commercial service with Delta Air Lines flying between Houston, Texas and New York. Some of the operators of the Convair 880 were Delta Air Lines, Cathay Pacific, Japan Airlines, Northeast Airlines, Swissair, Trans World Airlines and Venezuelan International Airways.

The Convair 880 was produced for only three years, from 1959 to 1962. There were 65 aircraft produced during its production run.

Convair 880 Design

The Convair 880 was built with a short and slim fuselage that has an exterior length of 39.42 meters, height of 11.06 meters and a fuselage diameter of 3.5 meters. Its wings has a wingspan of 36.58 meters and a wing area of 190 square meters. It has a wheelbase of 16.18 meters.

The Convair 880 22-M model is a modified class which is designed with four leading edge slats each wing, Krueger flaps attached to the leading edge, increased engine thrust, power-enhanced rudder, added fuel capacity, restrengthened landing gear, seating pitch alterations, and an uncomplicated overhead compartment.

With a cabin length of 26 meters, the aircraft can seat up to 110 passengers on board in a five abreast seating. It has a cabin width of 3.27 meters and height of 1.8 meters.

Convair 880 Engine and Performance

Powered by four CJ805 turbofan engines from General Electric, the Convair 880 has a maximum thrust of 11,650 lbf each engine. The engine has a length of 4.79 meters with thrust reverser and a fan diameter of 80.3 centimeters.

Built for speed, the Convair 880 has a maximum cruise speed of 534.5 knots at 22,000 feet with maximum take off weight of 83,688 kg. It has a stall speed of 105 knots at 55,600 kg and an approach speed of 139 knots. It has a maximum cruising altitude of 41,000 feet and a rate of climb of 3,000 feet per minute.

The aircraft has a travel range of 2,4723 nautical miles with 10,200 kg of payload and 6,400 kg fuel reserve. The Convair 880 has a maximum landing weight of 62,000 kg and a maximum payload of 30,688 kg.

Convair 880 Notable Accidents

On May 23 1960, a Delta Air Lines flight 1903 from Atlanta Municipal Airport crashed upon takeoff because of the aircraft’s nose that pitched up and banked steeply to the left before it crashed the ground and burst into flames. Four people on board were killed on the accident.

On August 26 1966, a Japan Air Lines flight from Haneda International Airport crashed due to uncontrollable left yaw while in a training flight. All of the four engines were separated, along with the aircraft’s nose and left main gear. The aircraft burst into flames killing all five people on board.

On November 20 1967, a Trans World Airlines flight 128 from Los Angeles International Airport fall short of the runway in an attempt to land in bad weather conditions. The aircraft crashed into several trees before it disintegrated and burst into flames. There were 82 occupants on board; 70 of them were killed on the accident.

On June 24 1969, a Japan Airlines flight 90 from Grant County International Airport crashed due to a simulated critical engine-out takeoff. The aircraft kept on yawing to the right until the engine number four hit the runway, following the aircraft’s crash before it burst into flames. Among five crew members, three were killed on the accident.

On June 15 1972, a Cathay Pacific flight 700Z from a stopover in Don Mueang International Airport crashed due to a bomb explosion in-flight. The bomb was concealed inside a passenger suitcase and exploded in the cabin that caused some seats to be ejected through a hole in the fuselage. There were 81 occupants on board; none of them survived the accident.

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