Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:aircraft
|
| gptkbp:countryOfOrigin |
gptkb:France
|
| gptkbp:crew |
2
|
| gptkbp:engine |
gptkb:General_Electric_CF700
|
| gptkbp:engineType |
turbofan
|
| gptkbp:firstFlight |
1963
|
| gptkbp:height |
5.32 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
Falcon 20E
|
| gptkbp:length |
17.15 m
|
| gptkbp:manufacturer |
gptkb:Dassault_Aviation
|
| gptkbp:maximumSpeed |
870 km/h
|
| gptkbp:maxTakeoffWeight |
13,600 kg
|
| gptkbp:numberOfEngines |
2
|
| gptkbp:range |
3,400 km
|
| gptkbp:role |
gptkb:helicopter
business jet |
| gptkbp:seatingCapacity |
8
|
| gptkbp:serviceCeiling |
13,100 m
|
| gptkbp:status |
in service
|
| gptkbp:variant |
gptkb:Dassault_Falcon_20
|
| gptkbp:wingspan |
16.3 m
|
| gptkbp:bfsParent |
gptkb:Islamic_Republic_of_Iran_Navy
gptkb:Falcon_20 |
| gptkbp:bfsLayer |
6
|