Fairchild XC-120 Packplane

Airplanes

Length

24.9936 m

Flat Wing Span

32.3088 m

Height

7.62 m

Flat Wing Area

134.4307 m²

Cruise Speed

281.6352 km/h

Max Speed

402.336 km/h

Max Ceiling

7284.72 m

Number of Engines

Aircraft Engine

First Flight

1950-08-11

Number Built

Maximum Take-Off Weight

29.0299 t (paragliders: kg)

Maximum Range

3685.398 km

Pictures

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Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Fairchild XC-120 Packplane	29.0299	3685.398

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Beriev Be-6		23.5	33		Compare
Fairchild AC-119		26.2128	33.2232		Compare
Antonov/Taqnia An-132	Pratt & Whitney Canada PW100	24.53	29.2	75	Compare
Fairchild C-123 Provider		23.1648	33.528	60	Compare
Antonov An-71		23.5	31.89		Compare
Stroukoff YC-134		24.9936	33.528		Compare

All data (19 fields)

Name: Fairchild XC-120 Packplane
Manufacturer: Fairchild
Description: The Fairchild XC-120 Packplane was an American experimental modular aircraft first flown in 1950.
First Flight: 1950-08-11
Designer: Fairchild
Type: Military transport aircraft
Length (m): 24.9936
Height (m): 7.62
Max Speed (km/h): 402.336
Cruise Speed (km/h): 281.6352
Max Ceiling (m): 7284.72
Capacity Description: 20,000 lb (9,090 kg) (2,700 cu.ft)
Number Built: 1
Powerplant Description: 2 × Pratt & Whitney R-4360 Wasp Major radial engines, 2424 kW (3250 hp) each
Wikipedia Article (URL): en.wikipedia.org/wiki/Fairchild_XC-120_Packplane
Flat Wing Span (m): 32.3088
Flat Wing Area (m²): 134.4307
Aircraft Engine: Pratt & Whitney R-4360 Wasp Major
Number of Engines: 2