Societe Nationale de Constructions Aeronatiques du Centre (SNCAC) - France
Manufacturer(s)
France; Morocco; Nazi Germany; Poland; Sweden
Operators
1945
Service Year
France
National Origin
Retired
Project Status
2
Crew
168
Units
TRANSPORT
General transport functionality to move supplies/cargo or personnel (including wounded and VIP) over range.
TRAINING
Developed ability to be used as a dedicated trainer for student pilots (typically under the supervision of an instructor).
41.2 ft
(12.57 meters)
Length
69.9 ft
(21.30 meters)
Width/Span
10.8 ft
(3.30 meters)
Height
8,818 lb
(4,000 kilograms)
Empty Weight
12,644 lb
(5,735 kilograms)
Maximum Take-Off Weight
+3,825 lb
(+1,735 kg)
Weight Difference
2 x Renault (Argus As 411) 12S-00 engines developing 590 horsepower each.
Propulsion
217 mph
(350 kph | 189 knots)
Max Speed
24,606 ft
(7,500 m | 5 miles)
Ceiling
1,056 miles
(1,700 km | 918 nm)
Range
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.
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).
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