Statements (30)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:countryOfOrigin |
gptkb:Russia
|
| gptkbp:crew |
2
|
| gptkbp:cruiseSpeed |
500 km/h
|
| gptkbp:developedBy |
gptkb:Soviet_Union
|
| gptkbp:engineType |
turboprop
|
| gptkbp:firstFlight |
1990-03-29
|
| gptkbp:height |
6.85 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
Ilyushin Il-114
|
| gptkbp:introduced |
1997
|
| gptkbp:length |
26.877 m
|
| gptkbp:manufacturer |
gptkb:Ilyushin
|
| gptkbp:maxTakeoffWeight |
23,500 kg
|
| gptkbp:numberBuilt |
20+
|
| gptkbp:primaryUser |
gptkb:Uzbekistan_Airways
|
| gptkbp:range |
1,000 km
|
| gptkbp:role |
regional airliner
|
| gptkbp:seatingCapacity |
64
|
| gptkbp:status |
in service
|
| gptkbp:successor |
gptkb:Antonov_An-24
|
| gptkbp:usedBy |
gptkb:Uzbekistan_Airways
gptkb:Russian_Air_Force gptkb:Vityaz-Aero |
| gptkbp:variant |
gptkb:Il-114-100
gptkb:Il-114T gptkb:Il-114LL |
| gptkbp:wingspan |
25.98 m
|
| gptkbp:bfsParent |
gptkb:Ilyushin
gptkb:Aeroflot |
| gptkbp:bfsLayer |
5
|