|
gptkbp:instanceOf
|
piston engine
|
|
gptkbp:category
|
gptkb:helicopter
business aircraft
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:crew
|
1 or 2
|
|
gptkbp:cruiseSpeed
|
270 mph (435 km/h, 235 kn)
|
|
gptkbp:engineType
|
gptkb:Pratt_&_Whitney_Canada_PT6A-28
|
|
gptkbp:firstFlight
|
March 17, 1969
|
|
gptkbp:height
|
15 ft 0 in (4.57 m)
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Beechcraft 100 King Air
|
|
gptkbp:introduced
|
1970
|
|
gptkbp:length
|
43 ft 9 in (13.34 m)
|
|
gptkbp:manufacturer
|
gptkb:Beechcraft
|
|
gptkbp:maxTakeoffWeight
|
11,500 lb (5,216 kg)
|
|
gptkbp:militaryDesignation
|
C-12 Huron (for some variants)
|
|
gptkbp:numberBuilt
|
over 350
|
|
gptkbp:numberOfEngines
|
2
|
|
gptkbp:primaryUser
|
civil aviation
military operators
|
|
gptkbp:produced
|
1969–1983
|
|
gptkbp:range
|
1,565 mi (2,519 km, 1,360 nmi)
|
|
gptkbp:seatingCapacity
|
7 to 13
|
|
gptkbp:serviceCeiling
|
25,000 ft (7,620 m)
|
|
gptkbp:successor
|
gptkb:Beechcraft_Super_King_Air
|
|
gptkbp:variant
|
gptkb:Beechcraft_King_Air_family
|
|
gptkbp:wingspan
|
45 ft 10 in (13.97 m)
|
|
gptkbp:bfsParent
|
gptkb:Pratt_&_Whitney_Canada_PT6
gptkb:Aviación_Militar_Bolivariana_de_Venezuela
|
|
gptkbp:bfsLayer
|
7
|