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Fairchild C-123 Provider ✕ Douglas DC-8 (piston airliner) ✕
Manufacturer Chase Aircraft Company Douglas Aircraft Corporation
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. The Douglas DC-8 was an American piston-engined airliner project by Douglas Aircraft.
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 Douglas Aircraft Corporation
Type Military transport aircraft
Length (m) 23.1648 23.4696
Height (m) 10.3632 7.9248
Cockpit Crew 4
Max Seating 60 48
Max Speed (km/h) 366.9304 450.6163
Cruise Speed (km/h) 278.4165 381.4145
Min Speed (km/h) 152.8877
Max Ceiling (m) 6431.28 9296.4
Rate of Climb (m/s) 6.1976 4.7752
Capacity Description 60 passengers, 50 litters, or 24000 lb of cargo 40-48 passengers
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 2 × Allison V-1710-G4L/R liquid-cooled V12 engine, 1193 kW (1600 hp) each
Primary Users United States Air Force (historical), United States Coast Guard (historical), South Vietnam Air Force (historical)
Status Project canceled
Wikipedia Article (URL) en.wikipedia.org/wiki/Fairchild_C-123_Provider en.wikipedia.org/wiki/Douglas_DC-8_%28piston_airliner%29
Flat Wing Span (m) 33.528 33.528
Flat Wing Area (m²) 113.6204 102.565
Flat Wing Aspect Ratio 11
Wake Category M
Aircraft Engine Allison V-1710
Number of Engines 2 2