TRAINING
Developed ability to be used as a dedicated trainer for student pilots (typically under the supervision of an instructor).
22.0 ft
(6.70 meters)
Length
35.1 ft
(10.70 meters)
Width/Span
9.2 ft
(2.80 meters)
Height
1,830 lb
(830 kilograms)
Empty Weight
2,535 lb
(1,150 kilograms)
Maximum Take-Off Weight
+705 lb
(+320 kg)
Weight Difference
1 x Salmson 9AB 9-cylinder air-cooled radial piston engine developing 230 horsepower driving a two-bladed propeller at the nose.
Propulsion
162 mph
(260 kph | 140 knots)
Max Speed
16,404 ft
(5,000 m | 3 miles)
Ceiling
360 mi
(580 km | 313 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 (162mph).
Graph average of 150 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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