Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:aircraft
|
| gptkbp:avionicsUpgrade |
yes
|
| gptkbp:basedOn |
gptkb:Ilyushin_Il-76
|
| gptkbp:capacity |
60,000 kg
|
| gptkbp:cockpit |
yes
|
| gptkbp:countryOfOrigin |
gptkb:Russia
|
| gptkbp:crew |
5
|
| gptkbp:cruiseSpeed |
780–800 km/h
|
| gptkbp:developedBy |
gptkb:Ilyushin
|
| gptkbp:engineType |
Aviadvigatel PS-90A-76
|
| gptkbp:firstFlight |
2012
|
| gptkbp:height |
14.76 m
|
| gptkbp:introduced |
2015
|
| gptkbp:length |
46.6 m
|
| gptkbp:manufacturer |
gptkb:Aviastar-SP
|
| gptkbp:maxTakeoffWeight |
210,000 kg
|
| gptkbp:NATOReportingName |
gptkb:Candid
|
| gptkbp:numberOfEngines |
4
|
| gptkbp:operator |
gptkb:Russian_Air_Force
|
| gptkbp:primaryUser |
gptkb:Russian_Ministry_of_Defence
|
| gptkbp:range |
4,000 km (with max payload)
|
| gptkbp:role |
gptkb:airborne_command_post
aerial refueling strategic airlifter |
| gptkbp:wingspan |
50.5 m
|
| gptkbp:bfsParent |
gptkb:A-100
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Ilyushin Il-76MD-90A
|