gptkbp:instanceOf
|
gptkb:helicopter
|
gptkbp:capacity
|
3
|
gptkbp:crew
|
1
|
gptkbp:design
|
gptkb:Stanley_Hiller_Jr.
tandem_rotor_system
|
gptkbp:engineType
|
Lycoming VO-540
|
gptkbp:firstFlight
|
1956
|
gptkbp:fuelCapacity
|
50 US gallons
|
gptkbp:height
|
10 ft 6 in
|
https://www.w3.org/2000/01/rdf-schema#label
|
Hiller 12D
|
gptkbp:introduced
|
1956
|
gptkbp:length
|
32 ft 6 in
|
gptkbp:manufacturer
|
gptkb:Hiller_Aircraft_Corporation
|
gptkbp:maxSpeed
|
120 mph
|
gptkbp:maxTakeoffWeight
|
3,500 lb
|
gptkbp:notableFeature
|
high maneuverability
low noise levels
good visibility
used in law enforcement
used in search and rescue missions
simple maintenance
used in aerial photography
used in agricultural applications
|
gptkbp:numberBuilt
|
approximately 100
|
gptkbp:powerOutput
|
300 hp
|
gptkbp:primaryUser
|
gptkb:United_States_Army
gptkb:United_States_Navy
civilian operators
|
gptkbp:productionYears
|
1956-1970
|
gptkbp:range
|
300 miles
|
gptkbp:relatedAircraft
|
gptkb:Hiller_360
gptkb:Hiller_12C
gptkb:Hiller_12E
gptkb:Hiller_12B
|
gptkbp:retired
|
1970s
|
gptkbp:role
|
civil and military use
|
gptkbp:rotorDiameter
|
36 ft 0 in
|
gptkbp:services
|
10,000 ft
|
gptkbp:successor
|
gptkb:Hiller_12E
|
gptkbp:type
|
light utility helicopter
|
gptkbp:usedBy
|
gptkb:United_States_Army
gptkb:United_States_Navy
various civilian operators
|
gptkbp:variant
|
gptkb:Hiller_12C
gptkb:Hiller_12F
gptkb:Hiller_12E
gptkb:Hiller_12B
|
gptkbp:weight
|
2,200 lb
|
gptkbp:wingspan
|
not applicable
|