The Gulfstream III, a business jet produced by Gulfstream Aerospace, is an all-weather, long-range, high speed aircraft powered by two Rolls-Royce Spey turbofan engines with thrust reversers.There are two types of GIIIs in service. Earlier model GIIIs have a DC based electrical system, these are referred to as Non-VSCF (Variable Speed, Constant Frequency). Alternately newer GIIIs have an AC based electrical system, and are referred to as VSCF GIIIs.
Military variants[]
- C-20A - USAF variant configured for 14 passengers and 5 crew[1]
- C-20B - C-20A with upgraded electronics used for Presidential and VIP missions[1]
- C-20C - C-20B with upgraded secure communications, backup for VC-25A Air Force One[1]
- C-20D - C-20B with modified communications equipment for use by the U.S. Navy[1]
- C-20E - C-20B with modified avionics and interior furnishings for use by the U.S. Navy[1]
Military operators[]
Military operators of the Gulfstream III, IV, and C-20 include:
- Template:DZA
- Template:CIV
- Template:DEN
- Template:GAB
- Template:IRL
- Template:ITA
- Template:IND
- Template:MEX
- Template:MAR
- Template:OMA
- Template:SWE
- Template:UGA
- Template:USA
- United States Air Force
- United States Army
- United States Navy
- United States Coast Guard
Specifications (Gulfstream III)[]
Template:Aero-specs
| X | This page is a candidate for deletion because this is only about the C-123, but is used in all sorts of articles that are not about the C-123.
If you disagree with this page's deletion, please explain why at Candidates for deletion or the page's talk page, or improve this page and remove the Admins: remember to check what links here and the page history before deleting. |
|---|
C-123 Provider
Transport Aircraft
The Fairchild C-123 Provider is a twin-engined military transport aircraft produced by the US American manufacturer Fairchild Aircraft, developed by Chase Aircraft.
Crew 4
Propulsion 2 Radial Engines Engine Model Pratt & Whitney R-2800-99W Double Wasp Engine Power (each) 1715 kW 2300 hp
Speed 367 km/h 198 kts
228 mph
Service Ceiling 8.839 m 29.000 ft Range 2.367 km 1.278 NM 1.471 mi.
Empty Weight 13.562 kg 30.000 lbs max. Takeoff Weight 27.216 kg 60.000 lbs
Wing Span 33,53 m 110,0 ft Wing Area 113,6 m² 1223 ft² Length 23,09 m 75,8 ft Height 10,39 m 34,1 ft
gatherd from http://www.flugzeuginfo.net/acdata_php/acdata_c123_en.php
References[]
See also[]
Related development
- Grumman Gulfstream II
- Gulfstream IV/G400/G450
Related lists
- List of active United States military aircraft
Template:Aviation lists
Template:US transport aircraft Template:Gulfstream