De Havilland Comet

· De Havilland
Airplanes
Length
28.3464 m
Flat Wing Span
35.052 m
Height
8.8392 m
Max Seating
36
First Flight
1949-07-27
Entry Into service
1952-05-02
Number Built
114
Maximum Take-Off Weight
49.8952 t (paragliders: kg)
Maximum Range
2414.016 km

Pictures

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Aircraft Weight Variants

Aircraft Maximum Take-Off Weight (t (paragliders: kg)) Maximum Range (km)
De Havilland Comet 49.8952 2414.016

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Gulfstream G650/G700/G800 30.1752 30.1752 19 Compare
Bombardier Global 7500 33.8328 31.6992 19 Compare
MPC 75 28.3464 29.5656 82 Compare
IPTN N2130 27.23 28.95 80 Compare
Airbus A320 family A320 CFM International CFM56 31.44 34.1 136 Compare
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All data (19 fields)
Name
De Havilland Comet
Manufacturer
De Havilland
Description
The de Havilland DH.106 Comet is a four-engine narrow body aircraft developed and manufactured by de Havilland in the United Kingdom.
First Flight
1949-07-27
Entry Into service
1952-05-02
Production End
1964-01-01
Service End
1997-03-14
Designer
De Havilland
Type
Narrow-body jet airliner
Length (m)
28.3464
Height (m)
8.8392
Max Seating
36
Capacity Description
36–44
National Origin
United Kingdom
Number Built
114
Primary Users
BOAC, British European Airways; Dan-Air; Royal Air Force
Status
Retired
Wikipedia Article (URL)
en.wikipedia.org/wiki/De_Havilland_Comet
Flat Wing Span (m)
35.052