Convair 880

· Convair

Airplanes

Length

39.3192 m

Flat Wing Span

36.576 m

Height

10.9728 m

Max Seating

110

Cruise Speed

-989.8931 km/h

Max Ceiling

12496.8 m

First Flight

1959-01-27

Entry Into service

1960-05-01

Number Built

Maximum Take-Off Weight

83.6878 t (paragliders: kg)

Total Fuel Capacity

40064.8

Maximum Range

4578.144 km

Pictures

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Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Convair 880	83.6878	40064.8	4578.144

Name	Family	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Yakovlev MC-21			36.8	35.9	132	Compare
Airbus A320neo family	A320	CFM International LEAP	33.84	35.8	140	Compare
Bombardier Global 7500			33.8328	31.6992	19	Compare
Sud Aviation Caravelle		Rolls-Royce Avon	32.01	34.3	80	Compare

All data (21 fields)

Name: Convair 880
Manufacturer: Convair
Description: The Convair 880 is a retired American narrow-body jet airliner produced by the Convair division of General Dynamics.
First Flight: 1959-01-27
Entry Into service: 1960-05-01
Production End: 1962-01-01
Service End: 1998-01-01
Designer: Convair
Type: Narrow-body jet airliner
Length (m): 39.3192
Height (m): 10.9728
Max Seating: 110
Cruise Speed (km/h): -989.8931
Max Ceiling (m): 12496.8
Capacity Description: 110 passengers / 24000 lb
National Origin: United States of America
Number Built: 65
Primary Users: Trans World Airlines, Delta Air Lines , Japan Airlines , Swissair
Status: Retired
Wikipedia Article (URL): en.wikipedia.org/wiki/Convair_880
Flat Wing Span (m): 36.576