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About: dbkwik:resource/sb30v4Zv8mqvGdQYq9VlOA==

PropertyValue
rdf:type
rdfs:label
  • Technoavia SM92 Finist
rdfs:comment
  • The Technoavia SM92 Finist is a utility aircraft with a STOL capability, designed by the Russian company Technoavia. The maiden flight was on December 28, 1993. It is built by the Smolensk Aviation Plant.
owl:sameAs
dcterms:subject
dbkwik:military/property/wikiPageUsesTemplate
max takeoff weight alt
  • 5181.0
loaded weight main
  • 2350.0
airfoil
  • P-301M
climb rate main
  • 5.0
number of props
  • 1
length alt
  • 29
span main
  • 14.60 m
Status
  • Production
cruise speed main
  • 200.0
cruise speed alt
  • 108
height alt
  • 307.34000000000003
Type
  • Light utility transport
type of prop
  • nine-cylinder radial engine
range alt
  • 744
range more
  • 2400.0
length main
  • 9.13 m
power alt
  • 360.0
area main
  • 20.44
power main
  • 269.0
stall speed alt
  • 54
height main
  • 3.08 m
span alt
  • 1460.5
range main
  • 1380.0
Manufacturer
max speed main
  • 230.0
engine (prop)
Capacity
  • **6 passengers or **2 stretchers plus attendant **600 kg cargo
stall speed more
  • flaps down
climb rate alt
  • 984.0
ceiling main
  • 3,000 m
National Origin
empty weight main
  • 1430.0
aspect ratio
  • 10.430000
stall speed main
  • 100.0
loaded weight alt
  • 5181.0
area alt
  • 220.0
First Flight
  • 1993-12-28
max speed alt
  • 124
jet or prop?
  • prop
never exceed speed alt
  • 156
empty weight alt
  • 3153.0
plane or copter?
  • plane
ceiling alt
  • 9840.0
max takeoff weight main
  • 2350.0
never exceed speed main
  • 290.0
Crew
  • 1
Number Built
  • about 30
ref
  • Brassey's World Aircraft & Systems Directory 1999/2000
abstract
  • The Technoavia SM92 Finist is a utility aircraft with a STOL capability, designed by the Russian company Technoavia. The maiden flight was on December 28, 1993. It is built by the Smolensk Aviation Plant.