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C-20 Gulfstream III
The C-20 Gulfstream is the military designation of the commercial Gulfstream bizjets used by the US military forces. The C-20D Gulfstream III used for world-wide airlift of senior leadership and dignitaries. The C-20G is the Gulfstream IV used for long range, medium airlift logistics support for Fleet Battle Groups.
The C-20D Gulfstream III is an all-weather, long-range, high speed aircraft powered by two Rolls-Royce Spey turbofan engines with thrust reversers . The aircraft has an executive compartment with accommodations for five passengers, and a staff compartment with accommodations for eight passengers. C-20D aircraft are operated by Fleet Logistics Support Wing Detachment at Naval Air Facility, Andrews Air Force Base , Washington, D.C.
The C-20G Gulfstream IV is an upgraded and updated version powered by two Rolls-Royce Tay engines. The aircraft may be configured for cargo operations, passenger operations or combinations of the two. With passengers seats removed, it may be modified to the following configurations: three pallets/no passengers, two pallets/eight passengers, and one pallet/fourteen passengers. With a full complement of seats installed, the aircraft is capable of accommodating up to twenty-six passengers and a crew of four. A hydraulically-operated cargo door is installed on the starboard side of the aircraft, and a ball roller cargo floor is capable of accommodating palletized cargo . C-20G aircraft are operated Fleet Logistics Support Squadron Four Eight (VR-48 ) and Marine Air Support Detachment (MASD) at Naval Air Facility, Andrews Air Force Base, Washington, DC and at Fleet Logistics Support Wing Detachment , Marine Corps Base, Kaneohe Bay , Hawaii.
General Characteristics
- Contractor: Sustaining Engineering - Gulfstream, CLS - Sabreliner
- Unit Cost: New GIV - $37 Million
- Propulsion:
- GIII - (2) Rolls-Royce Spey MK511-8 turbofan engines equipped with thrust reversers.
- GIV - (2) Rolls-Royce Tay MK611-8 turbofan engines equipped with thrust reversers.
- Length: (Nose to Tail)
- GIII - 83.80 ft (25.54 m)
- IV - 88.40 ft (26.94 m)
- Height : (Tail Height)
- GIII - 24.37 ft (7.43 m)
- GIV - 24.51 ft (7.47 m)
- Wing Span:
- GIII - 77.83 ft (23.72 m)
- GIV - 77.83 ft (23.72 m)
- Weight: Max. gross, take-off:
- GIII - 69,700 lb (31.6 t)
- GIV - 73,200 lb (33.2 t)
- Airspeed: 0.75 Mach (919 km/h)
- Range:
- GIII - Max (varies with load) 3,700 nautical miles (6,850 km)
- GIV - Max 5,130 nautical miles (9,500 km)
- Crew: Pilot, Co-Pilot and Crew chief, flight attendant and/or loadmaster added as required. Crewed by USMC/USN Reserves
| Modern USAF Series | Miscellaneous | |
| C-5 Galaxy | Attack--OA/A-10,AC-130H/U | RC-135V/W |
| C-17 Globemaster III | Bomber--B-52,-2,-1B,F-117A | OC-135B |
| C-20 Gulfstream III | Fighter--F-15/E ,F-16 | KC-10,-135 |
| C-21 Learjet | Electronic--E-3,-4B,-8C EC-130E/J,H | HC-130P/N |
| C-32 C-22B | Transport--C-5,-17,-141B, -20,-21 | MC-130E/H/P |
| C-130 Hercules | C-22B, -32, -130, -37A, -40B/C | MH-53J/M |
| C-141B Starlifter | Trainers--T-1, -37, -38, -43, -6 | HH-60G |
| C-37A Gulfstream V | Weather--WC-130, -135 | UH-1N |
| C-40B/C Clipper | UAV--RQ-1/MQ-1 UAV, Global Hawk | U-2S/TU-2S |
| VC-25 |
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