Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:aircraft
|
| gptkbp:aircraftType |
twin-turboprop
|
| gptkbp:crew |
1 or 2
|
| gptkbp:engineType |
gptkb:Pratt_&_Whitney_Canada_PT6A-28
|
| gptkbp:family |
gptkb:Beechcraft_King_Air
|
| gptkbp:firstFlight |
1972
|
| gptkbp:height |
15 ft 0 in (4.57 m)
|
| gptkbp:introduced |
1972
|
| gptkbp:length |
43 ft 9 in (13.34 m)
|
| gptkbp:manufacturer |
gptkb:Beechcraft
|
| gptkbp:maximumSpeed |
270 knots (310 mph, 500 km/h)
|
| gptkbp:maxTakeoffWeight |
12,500 lb (5,670 kg)
|
| gptkbp:numberBuilt |
157
|
| gptkbp:primaryUser |
civil aviation
|
| gptkbp:range |
1,800 nmi (2,100 mi, 3,300 km)
|
| gptkbp:seatingCapacity |
13
|
| gptkbp:serviceCeiling |
31,000 ft (9,450 m)
|
| gptkbp:status |
out of production
|
| gptkbp:wingspan |
50 ft 3 in (15.32 m)
|
| gptkbp:bfsParent |
gptkb:PT-6
|
| gptkbp:bfsLayer |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
Beechcraft King Air C100
|