Flat Wing Area
113.6204 m²
Cruise Speed
278.4165 km/h
Entry Into service
1956-01-01
Maximum Take-Off Weight
27.2155 t (paragliders: kg)
Total Fuel Capacity
5534.272
Maximum Range
1665.671 km
Pictures
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Aircraft Weight Variants
| Aircraft |
Maximum Take-Off Weight (t (paragliders: kg)) |
Total Fuel Capacity |
Maximum Range (km) |
|
Fairchild C-123 Provider |
27.2155 |
5534.272 |
1665.671 |
Similar airplanes
All data (29 fields)
- Name
- Fairchild C-123 Provider
- Manufacturer
- Chase Aircraft Company
- Description
- The Fairchild C-123 Provider is an American military transport aircraft designed by Chase Aircraft and built by Fairchild Aircraft for the U.S.
- ICAO Code
- C123
- First Flight
- 1949-10-14
- Entry Into service
- 1956-01-01
- Production End
- 1970-01-01
- Service End
- 1995-01-01
- Designer
- Chase Aircraft Company
- Type
- Military transport aircraft
- Length (m)
- 23.1648
- Height (m)
- 10.3632
- Cockpit Crew
- 4
- Max Seating
- 60
- Max Speed (km/h)
- 366.9304
- Cruise Speed (km/h)
- 278.4165
- Min Speed (km/h)
- 152.8877
- Max Ceiling (m)
- 6431.28
- Rate of Climb (m/s)
- 6.1976
- Capacity Description
- 60 passengers, 50 litters, or 24000 lb of cargo
- National Origin
- United States of America
- Number Built
- 307
- Powerplant Description
- 2 × Pratt & Whitney R-2800-99W Double Wasp 18-cylinder air-cooled radial piston engines, 1864 kW (2500 hp) each
- Primary Users
- United States Air Force (historical), United States Coast Guard (historical), South Vietnam Air Force (historical)
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Fairchild_C-123_Provider
- Flat Wing Span (m)
- 33.528
- Flat Wing Area (m²)
- 113.6204
- Wake Category
- M
- Number of Engines
- 2