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gptkbp:instanceOf
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gptkb:helicopter
|
|
gptkbp:armament
|
none
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gptkbp:capacity
|
up to 6 passengers
|
|
gptkbp:cockpit
|
two-seat cockpit
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|
gptkbp:crew
|
1
|
|
gptkbp:design
|
gptkb:Igor_Sikorsky
gptkb:Sikorsky_S-300_series
|
|
gptkbp:engine
|
gptkb:Lycoming_T53
|
|
gptkbp:enginePower
|
1,000 shp
|
|
gptkbp:engineType
|
turboshaft
|
|
gptkbp:firstFlight
|
1974
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|
gptkbp:fuelCapacity
|
400 liters
|
|
gptkbp:headlights
|
two-bladed tail rotor
|
|
gptkbp:height
|
3.8 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Sikorsky S-300S
|
|
gptkbp:introduced
|
1974
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|
gptkbp:landingGear
|
skid landing gear
|
|
gptkbp:length
|
12.5 m
|
|
gptkbp:manufacturer
|
gptkb:Sikorsky_Aircraft_Corporation
|
|
gptkbp:maxSpeed
|
250 km/h
|
|
gptkbp:maxTakeoffWeight
|
2,500 kg
|
|
gptkbp:notableFeature
|
advanced avionics
high maneuverability
low noise levels
easy maintenance
good visibility
two-bladed main rotor
|
|
gptkbp:numberBuilt
|
50
|
|
gptkbp:primaryUser
|
gptkb:United_States_Army
gptkb:United_States_Coast_Guard
gptkb:United_States_Navy
|
|
gptkbp:produces
|
1974-1980
|
|
gptkbp:propulsion
|
single-engine
|
|
gptkbp:range
|
600 km
|
|
gptkbp:relatedAircraft
|
gptkb:Sikorsky_S-300C
Sikorsky S-300D
Sikorsky S-300E
Sikorsky S-300F
Sikorsky S-300H
|
|
gptkbp:role
|
utility helicopter
training helicopter
|
|
gptkbp:rotorDiameter
|
10.7 m
|
|
gptkbp:services
|
3,000 m
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
gptkb:Sikorsky_S-300C
|
|
gptkbp:type
|
civil helicopter
|
|
gptkbp:usedBy
|
various flight schools
|
|
gptkbp:variant
|
gptkb:Sikorsky_S-300C
|
|
gptkbp:weight
|
1,500 kg
|