Chase XC-123A

Airplanes

Length

23.4696 m

Flat Wing Span

33.528 m

Height

10.0584 m

Flat Wing Area

113.6 m²

Cruise Speed

643.7376 km/h

Max Speed

804.672 km/h

Number of Engines

Aircraft Engine

First Flight

1951-04-21

Number Built

Maximum Take-Off Weight

27.2155 t (paragliders: kg)

Pictures

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Aircraft	Maximum Take-Off Weight (t (paragliders: kg))
Chase XC-123A	27.2155

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Consolidated PB4Y-2 Privateer	Pratt & Whitney R-1830 Twin Wasp	22.73	33.53		Compare
Boeing XB-38 Flying Fortress	Allison V-1710	22.56	31.67		Compare
Consolidated PB2Y Coronado		24.2	35		Compare
Boeing B-17 Flying Fortress		22.66	31.62		Compare
Junkers Ju 89		26.2128	35.052		Compare
Focke-Wulf Fw 200 Condor		23.45	32.85	30	Compare

All data (19 fields)

Name: Chase XC-123A
Manufacturer: Chase Aircraft Company
Description: The Chase XC-123A was an experimental transport aircraft developed by Chase Aircraft.
First Flight: 1951-04-21
Designer: Michael Stroukoff
Type: Military transport aircraft
Length (m): 23.4696
Height (m): 10.0584
Cockpit Crew: 3
Max Speed (km/h): 804.672
Cruise Speed (km/h): 643.7376
Number Built: 1
Powerplant Description: 4 × General Electric J47-GE-11 turbojets
Primary Users: United States Air Force
Wikipedia Article (URL): en.wikipedia.org/wiki/Chase_XC-123A
Flat Wing Span (m): 33.528
Flat Wing Area (m²): 113.6
Aircraft Engine: General Electric J47
Number of Engines: 4