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[edit] Old infobox
This article was tagged by WikiProject Aircraft as needing to be brought up to snuff. If the old spec sheet should need to be replaced, it is below. thadius856talk 05:26, 20 October 2006 (UTC)
C-20 Gulfstream III |
|
C-20 Gulfstream III |
Description |
Role |
Corporate Jet |
Crew |
Two |
First Flight |
02-12-1979 |
Entered Service |
1983 |
Manufacturer |
Gulfstream Aerospace Corp |
Dimensions |
Length C-20B |
83 ft 2 in |
25.35 m |
Length C-20H |
88 ft 4 in |
26.92 m |
Wingspan |
77 ft 10 in |
23.72 m |
Height |
24 ft 6 in |
7.47 m |
Wing area |
ft² |
m² |
Weights |
Empty |
lb |
kg |
Loaded |
lb |
kg |
Maximum takeoff C-20B |
69,700 lb |
31,620 kg |
Maximum takeoff C-20H |
74,600 lb |
33,840 kg |
Capacity |
|
Powerplant |
Engines |
|
Thrust |
lb |
kN |
Performance |
Maximum speed |
mph |
km/h |
Combat range |
miles |
km |
Ferry range |
miles |
km |
Service ceiling |
ft |
m |
Rate of climb |
ft/min |
m/min |
Wing loading |
lb/ft² |
kg/m² |
Thrust/Weight |
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Avionics |
Avionics |
|
Armament |
Guns |
|
Bombs |
|
Missiles |
|
Rockets |
|
Other |
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