SNCAC NC.211 Cormoran

· SNCAC · 4 × SNECMA 14R

Airplanes

Length

30.5 m

Flat Wing Span

44 m

Height

10.7 m

Flat Wing Area

200 m²

Max Seating

Cruise Speed

288 km/h

Max Speed

390 km/h

Max Ceiling

8000 m

Number of Engines

Aircraft Engine

First Flight

1948-07-20

Number Built

Maximum Range

1000 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Range (km)
SNCAC NC.211 Cormoran	1000

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Boeing XB-39 Superfortress	Allison V-3420	30.18	43.05		Compare
Tupolev Tu-4	Shvetsov ASh-73	30.18	43.05		Compare
Boeing B-29 Superfortress		30.1752	42.9768		Compare
Boeing B-50 Superfortress		30.1752	42.9768		Compare
Nakajima G5N Shinzan	Mitsubishi Kasei	31.02	42.12		Compare
Douglas DC-4E	Pratt & Whitney R-2180-A Twin Hornet	29.74	42.14	42	Compare

All data (21 fields)

Name: SNCAC NC.211 Cormoran
Manufacturer: SNCAC
Description: The SNCAC NC.211 Cormoran was a large four-engined military transport aircraft for passengers and cargo designed and built by SNCAC from 1945.
First Flight: 1948-07-20
Designer: SNCAC
Length (m): 30.5
Height (m): 10.7
Cockpit Crew: 5
Max Seating: 76
Max Speed (km/h): 390
Cruise Speed (km/h): 288
Max Ceiling (m): 8000
Capacity Description: 12,000 kg payload, 76 paratroops, 60 stretchers or 100-150 passengers (civil)
National Origin: France
Number Built: 2
Powerplant Description: 4 × SNECMA 14R 14-cyl. two-row air-cooled radial piston engines, 1193 kW (1600 hp) each
Wikipedia Article (URL): en.wikipedia.org/wiki/SNCAC_NC.211_Cormoran
Flat Wing Span (m): 44
Flat Wing Area (m²): 200
Aircraft Engine: SNECMA 14R
Number of Engines: 4