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gptkbp:instanceOf
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gptkb:helicopter
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gptkbp:aircraft
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rotorcraft
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gptkbp:airlines
|
2 pilots
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gptkbp:armament
|
none
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gptkbp:avionics
|
modernized
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
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gptkbp:crewCapacity
|
2
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|
gptkbp:design
|
gptkb:Boeing_Vertol
high capacity
|
|
gptkbp:emergencyServices
|
floatation gear
|
|
gptkbp:engineType
|
turboshaft
|
|
gptkbp:firstFlight
|
1980
|
|
gptkbp:fuelCapacity
|
1,500 liters
|
|
gptkbp:height
|
5.79 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Boeing Vertol 234LR
|
|
gptkbp:introduced
|
1980
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gptkbp:landingGear
|
tricycle type
|
|
gptkbp:legacy
|
influenced future designs
|
|
gptkbp:length
|
22.86 m
|
|
gptkbp:maintenance
|
moderate
|
|
gptkbp:manufacturer
|
gptkb:Boeing
|
|
gptkbp:maxSpeed
|
150 knots
|
|
gptkbp:notableFeature
|
none reported
tandem_rotor_system
|
|
gptkbp:operationalHistory
|
varied missions
|
|
gptkbp:operationalRange
|
1,000 km
|
|
gptkbp:operationalRole
|
transport and logistics
|
|
gptkbp:passengerCapacity
|
30
4,500 kg
large rear ramp
|
|
gptkbp:performance
|
highly capable
|
|
gptkbp:powerOutput
|
2,500 shp
|
|
gptkbp:primaryUser
|
gptkb:U.S._Army
|
|
gptkbp:produces
|
limited
|
|
gptkbp:productionYears
|
1980-1990
|
|
gptkbp:range
|
400 nautical miles
|
|
gptkbp:relatedAircraft
|
gptkb:Boeing_Vertol_107
|
|
gptkbp:retired
|
2000s
|
|
gptkbp:role
|
transport helicopter
|
|
gptkbp:rotorDiameter
|
18.29 m
|
|
gptkbp:safetyFeatures
|
dual control systems
|
|
gptkbp:services
|
1980s
2000s
15,000 ft
|
|
gptkbp:setting
|
gptkb:tandem_rotor
|
|
gptkbp:successor
|
gptkb:Boeing_CH-47_Chinook
|
|
gptkbp:type
|
utility helicopter
|
|
gptkbp:usedBy
|
military
civilian
|
|
gptkbp:variant
|
gptkb:Boeing_Vertol_234
|
|
gptkbp:weight
|
10,000 kg
|
|
gptkbp:wingspan
|
not applicable
|