Douglas DC-8

Airplanes

Length

45.9334 m

Flat Wing Span

43.4035 m

Max Seating

177

Number of Engines

Aircraft Engine

First Flight

1958-05-30

Entry Into service

1959-09-18

Number Built

556

Maximum Take-Off Weight

123.8307 t (paragliders: kg)

Total Fuel Capacity

88552.14

Maximum Range

6963.52 km

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Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Douglas DC-8	123.8307	88552.14	6963.52

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Airbus A400M Atlas	Europrop TP400	45.1	42.4	116	Compare
Vickers VC10	Rolls-Royce Conway	48.1584	44.5008	151	Compare
Boeing CC-137	Pratt & Whitney JT3D	46.61	44.42	170	Compare
Boeing C-137 Stratoliner		46.61	44.42		Compare
Boeing 707	Pratt & Whitney JT3D	46.3296	44.196	194	Compare
Shanghai Y-10		42.93	42.24		Compare

All data (20 fields)

Name: Douglas DC-8
Manufacturer: Douglas Aircraft Corporation
Description: The Douglas DC-8 (sometimes McDonnell Douglas DC-8) is an early long-range narrow-body jetliner designed and produced by the American Douglas Aircraft Company.
First Flight: 1958-05-30
Entry Into service: 1959-09-18
Production End: 1972-01-01
Designer: Douglas Aircraft Corporation
Type: Narrow-body airliner
Length (m): 45.9334
Max Seating: 177
Capacity Description: 177
National Origin: United States of America
Number Built: 556
Powerplant Description: -10: P&W JT3C , -20/30: P&W JT4A
Primary Users: United Airlines (historical), UPS Airlines (historical) , Delta Air Lines (historical) , Trans Air Cargo Service
Status: In limited cargo service
Wikipedia Article (URL): en.wikipedia.org/wiki/Douglas_DC-8
Flat Wing Span (m): 43.4035
Aircraft Engine: Pratt & Whitney J57
Number of Engines: 4