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gptkbp:instanceOf
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gptkb:helicopter
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gptkbp:avionics
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basic navigation instruments
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gptkbp:barrelLength
|
2 degrees/second
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gptkbp:capacity
|
3
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gptkbp:climbRate
|
1,200 ft/min
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gptkbp:cockpit
|
two-seat tandem
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gptkbp:controls
|
cyclic and collective pitch control
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gptkbp:crew
|
1
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gptkbp:design
|
single main rotor and tail rotor
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gptkbp:engineType
|
Lycoming VO-540
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gptkbp:firstFlight
|
1956
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gptkbp:flag
|
4 degrees/second
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gptkbp:fuelCapacity
|
40 gallons
20 gallons/hour
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gptkbp:headlights
|
1
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gptkbp:height
|
10 ft 6 in
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gptkbp:historicalSignificance
|
one of the first light helicopters
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|
https://www.w3.org/2000/01/rdf-schema#label
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Hiller 12Q
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gptkbp:influenced
|
modern light helicopters
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gptkbp:influencedBy
|
gptkb:Hiller_12E
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gptkbp:introduced
|
1956
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gptkbp:landingGear
|
skids
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gptkbp:legacy
|
paved the way for future designs.
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gptkbp:length
|
32 ft 6 in
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|
gptkbp:manufacturer
|
gptkb:Hiller_Aircraft_Corporation
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|
gptkbp:market
|
commercial and military
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|
gptkbp:maxSpeed
|
120 mph
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|
gptkbp:maxTakeoffWeight
|
3,200 lb
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gptkbp:notableFeature
|
2
fenestron tail rotor
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|
gptkbp:numberBuilt
|
approximately 1,000
|
|
gptkbp:powerOutput
|
300 hp
|
|
gptkbp:productionLocation
|
gptkb:California
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|
gptkbp:productionYears
|
1956-1970
|
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gptkbp:range
|
300 miles
|
|
gptkbp:retired
|
1970s
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gptkbp:river
|
45 degrees
|
|
gptkbp:role
|
utility
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|
gptkbp:rotorDiameter
|
36 ft
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gptkbp:services
|
10,000 ft
|
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gptkbp:speed
|
50 mph
|
|
gptkbp:succeededBy
|
3 degrees/second
|
|
gptkbp:successor
|
gptkb:Hiller_12E
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gptkbp:type
|
light utility helicopter
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|
gptkbp:usedBy
|
military
civilian
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gptkbp:variant
|
gptkb:Hiller_12S
gptkb:Hiller_12R
|
|
gptkbp:weight
|
2,200 lb
|