gptkbp:instanceOf
|
gptkb:helicopter
|
gptkbp:aircraft
|
rotorcraft
tandem_rotor_configuration
|
gptkbp:airlines
|
2 pilots
|
gptkbp:armament
|
none
|
gptkbp:avionics
|
modern avionics suite
|
gptkbp:basedOn
|
18.29 m
not applicable
|
gptkbp:cockpit
|
two-pilot cockpit
|
gptkbp:constructionMaterial
|
aluminum fuselage
|
gptkbp:crewCapacity
|
2
|
gptkbp:decommissioned
|
1980s
|
gptkbp:design
|
military transport
Boeing_Vertol_engineers
tandem_rotor_design
|
gptkbp:enginePower
|
1,500 hp
|
gptkbp:engineType
|
turbine engine
|
gptkbp:firstFlight
|
1963
|
gptkbp:fuelCapacity
|
1,500 liters
|
gptkbp:headlights
|
integrated tail boom
no_tail_rotor
|
gptkbp:height
|
4.57 m
|
gptkbp:helicopterCapacity
|
pressurized flight deck
|
gptkbp:historicalSignificance
|
first tandem rotor helicopter in service
|
https://www.w3.org/2000/01/rdf-schema#label
|
Boeing Vertol 619-1
|
gptkbp:influenced
|
modern tandem rotor helicopters
|
gptkbp:landingGear
|
skid
|
gptkbp:legacy
|
influenced future helicopter designs
|
gptkbp:length
|
15.24 m
|
gptkbp:manufacturer
|
gptkb:Boeing_Vertol
|
gptkbp:maximumDepth
|
2,000 kg
|
gptkbp:maxSpeed
|
150 knots
|
gptkbp:maxTakeoffWeight
|
5,000 kg
|
gptkbp:notableUsers
|
gptkb:U.S._Army
|
gptkbp:numberOfEpisodes
|
2
|
gptkbp:operationalHistory
|
used in various military operations
|
gptkbp:operationalRange
|
300 nautical miles
|
gptkbp:passengerCapacity
|
24
1,500 kg
|
gptkbp:produces
|
1963-1970
|
gptkbp:productionLocation
|
gptkb:Pennsylvania,_USA
|
gptkbp:propulsion
|
twin_rotor_system
|
gptkbp:range
|
300 nautical miles
|
gptkbp:relatedModel
|
gptkb:Boeing_Vertol_107
|
gptkbp:retirementYear
|
1970s
|
gptkbp:role
|
transport
utility helicopter
|
gptkbp:service_ceiling
|
3,000 m
|
gptkbp:services
|
1964
approximately 10 years
|
gptkbp:successor
|
gptkb:Boeing_Vertol_107-II
Boeing_CH-46_Sea_Knight
|
gptkbp:type
|
multi-role helicopter
|
gptkbp:usedBy
|
military
|
gptkbp:variant
|
gptkb:Boeing_Vertol_107
|
gptkbp:weight
|
3,000 kg
|
gptkbp:wingspan
|
12.19 m
|