Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:aircraft
|
| gptkbp:aircraftType |
twin-turboprop
|
| gptkbp:crew |
1
|
| gptkbp:developedBy |
gptkb:Beechcraft_King_Air_C90
Beechcraft F90-1 |
| gptkbp:emptyWeight |
3,356 kg
|
| gptkbp:engineType |
gptkb:Pratt_&_Whitney_Canada_PT6A-135
|
| gptkbp:firstFlight |
1978
|
| gptkbp:height |
4.57 m
|
| gptkbp:introduced |
1978
|
| gptkbp:length |
12.17 m
|
| gptkbp:manufacturer |
gptkb:Beechcraft
|
| gptkbp:maximumSpeed |
289 knots
|
| gptkbp:maxTakeoffWeight |
4,763 kg
|
| gptkbp:numberBuilt |
202
|
| gptkbp:numberOfEngines |
2
|
| gptkbp:primaryUse |
air taxi
military liaison business aviation |
| gptkbp:range |
1,335 nautical miles
|
| gptkbp:retired |
2002
|
| gptkbp:seatingCapacity |
6
|
| gptkbp:serviceCeiling |
30,000 ft
|
| gptkbp:wingspan |
16.61 m
|
| gptkbp:bfsParent |
gptkb:Pratt_&_Whitney_Canada_PT6
|
| gptkbp:bfsLayer |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
Beechcraft F90 King Air
|