About: Bell 206   Sponge Permalink

An Entity of Type : dbkwik:resource/AGhloO_nVTaFp7GvOmHv5Q==, within Data Space : 134.155.108.49:8890 associated with source dataset(s)

The Bell 206 is a family of two-bladed, single- or twin-engine helicopters, manufactured by Bell Helicopter at its Mirabel, Quebec plant. Originally developed as the Bell YOH-4 for the United States Army's Light Observation Helicopter program, the 206 failed to be selected. Bell redesigned the airframe and successfully marketed the aircraft commercially as the five-place Bell 206A JetRanger. The new design was eventually selected by the Army as the OH-58 Kiowa. Bell also developed a seven-place LongRanger, which was later offered with a twin-engine option as the TwinRanger, while Tridair Helicopters offers a similar conversion of the LongRanger called the Gemini ST. The ICAO-assigned model designation "B06" is used on flight plans for the JetRanger and LongRanger, and the designation "B06T

AttributesValues
rdf:type
rdfs:label
  • Bell 206
rdfs:comment
  • The Bell 206 is a family of two-bladed, single- or twin-engine helicopters, manufactured by Bell Helicopter at its Mirabel, Quebec plant. Originally developed as the Bell YOH-4 for the United States Army's Light Observation Helicopter program, the 206 failed to be selected. Bell redesigned the airframe and successfully marketed the aircraft commercially as the five-place Bell 206A JetRanger. The new design was eventually selected by the Army as the OH-58 Kiowa. Bell also developed a seven-place LongRanger, which was later offered with a twin-engine option as the TwinRanger, while Tridair Helicopters offers a similar conversion of the LongRanger called the Gemini ST. The ICAO-assigned model designation "B06" is used on flight plans for the JetRanger and LongRanger, and the designation "B06T
sameAs
Developed Into
dcterms:subject
dbkwik:military/pr...iPageUsesTemplate
max takeoff weight alt
  • 1451.0
climb rate main
  • 1350.0
number of props
  • 1(xsd:integer)
length alt
  • 12.11 m
span main
  • 1016.0
power/mass alt
  • 420(xsd:integer)
Produced
  • 1962(xsd:integer)
Status
  • In service
height alt
  • 2.83 m
Introduced
  • 1967(xsd:integer)
Type
  • Multipurpose Utility helicopter
type of prop
  • turboshaft
loading main
  • 4(xsd:integer)
range alt
  • 430(xsd:integer)
length main
  • 1209.04
power alt
  • 310.0
Unit Cost
  • US$900K to $1.2M
area main
  • 872.0
power main
  • 450(xsd:integer)
height main
  • 284.48
span alt
  • 10.16 m
range main
  • 374.0
Manufacturer
max speed main
  • 120(xsd:integer)
engine (prop)
  • Allison 250-C20B
power/mass main
  • 0(xsd:double)
Capacity
  • 4(xsd:integer)
climb rate alt
  • 6.9
ceiling main
  • 13500.0
National Origin
  • Canada
empty weight main
  • 1713.0
Developed From
area alt
  • 81.1
First Flight
  • 1962-12-08(xsd:date)
  • 1966-01-10(xsd:date)
max speed alt
  • 222(xsd:integer)
jet or prop?
  • prop
never exceed speed alt
  • 241(xsd:integer)
loading alt
  • 177(xsd:integer)
empty weight alt
  • 777.0
plane or copter?
  • copter
ceiling alt
  • 4,115 m
max takeoff weight main
  • 3200.0
variants with their own articles
never exceed speed main
  • 130(xsd:integer)
Crew
  • 1(xsd:integer)
Number Built
  • 7300(xsd:integer)
ref
  • Bell 206B-L4 specifications
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