SOCATA (Aerospatiale) - France
Manufacturer(s)
France; Portugal; Senegal; Togo
Operators
1983
Service Year
France
National Origin
Active
Project Status
2
Crew
56
Units
TRAINING
Developed ability to be used as a dedicated trainer for student pilots (typically under the supervision of an instructor).
24.9 ft
(7.60 meters)
Length
26.0 ft
(7.92 meters)
Width/Span
8.7 ft
(2.65 meters)
Height
2,061 lb
(935 kilograms)
Empty Weight
2,756 lb
(1,250 kilograms)
Maximum Take-Off Weight
+694 lb
(+315 kg)
Weight Difference
1 x Lycoming AEIO-540-L 1B5D 6-cylinder, air-cooled piston engine developing 300 horsepower driving two-bladed propeller unit at the nose.
Propulsion
236 mph
(380 kph | 205 knots)
Max Speed
22,999 ft
(7,010 m | 4 miles)
Ceiling
808 miles
(1,300 km | 702 nm)
Range
1,850 ft/min
(564 m/min)
Rate-of-Climb
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
