Societe Nationale de Constructions Aeronatiques du Centre (SNCAC) - France
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Width/Span
69.9 ft
(21.30 m)
Empty Wgt
8,818 lb
(4,000 kg)
MTOW
12,644 lb
(5,735 kg)
Wgt Diff
+3,825 lb
(+1,735 kg)
(Showcased structural values pertain to the SNCAC NC.701 production variant)
Installed:
2 x Renault (Argus As 411) 12S-00 engines developing 590 horsepower each.
Max Speed
217 mph
(350 kph | 189 kts)
Ceiling
24,606 ft
(7,500 m | 5 mi)
Range
1,056 mi
(1,700 km | 3,148 nm)
♦ MACH Regime (Sonic)
Sub
Trans
Super
Hyper
HiHyper
ReEntry
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030
Values are derrived from a variety of categories related to the design, overall function, and historical influence of this aircraft in aviation history.
The overall rating takes into account over 60 individual factors related to this aircraft entry.
Rating is out of a possible 100 points.
This entry's maximum listed speed (217mph).
Graph average of 225 miles-per-hour.
SNCAC NC.701 operational range when compared to distances between major cities (in KM).
Max Altitude Visualization
The three qualities reflected above are altitude, speed, and range.
Showcasing era cross-over of this aircraft design.
Compared against Ilyushin IL-2 (military) and Cessna 172 (civilian).
Ribbon graphics not necessarily indicative of actual historical campaign ribbons. Ribbons are clickable to their respective aerial campaigns / operations / aviation periods.