Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:business_jet
|
| gptkbp:avionics |
gptkb:Honeywell_Primus_2000
|
| gptkbp:countryOfOrigin |
gptkb:France
|
| gptkbp:crew |
2
|
| gptkbp:engine |
gptkb:Honeywell_TFE731-5BR-1C
|
| gptkbp:engineType |
turbofan
|
| gptkbp:family |
gptkb:Dassault_Falcon_900
|
| gptkbp:firstFlight |
1994
|
| gptkbp:height |
7.55 m
|
| gptkbp:length |
20.21 m
|
| gptkbp:manufacturer |
gptkb:Dassault_Aviation
|
| gptkbp:maximumSpeed |
Mach 0.84
|
| gptkbp:maxTakeoffWeight |
21,863 kg
|
| gptkbp:numberOfEngines |
3
|
| gptkbp:range |
4,500 nautical miles
|
| gptkbp:seatingCapacity |
up to 19
|
| gptkbp:successor |
gptkb:Falcon_900EX
|
| gptkbp:variant |
gptkb:Dassault_Falcon_900
|
| gptkbp:wingspan |
21.38 m
|
| gptkbp:bfsParent |
gptkb:Dassault_Falcon_900
gptkb:Falcon_900 |
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Falcon 900C
|