Statements (32)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:aircraft
|
| gptkbp:builtBy |
gptkb:Aerostar
|
| gptkbp:category |
gptkb:trainer_aircraft
low-wing aircraft single-engine aircraft civil utility aircraft |
| gptkbp:configuration |
tandem seating
|
| gptkbp:crew |
2
|
| gptkbp:emptyWeight |
998 kg
|
| gptkbp:engine |
gptkb:Vedeneyev_M-14P
|
| gptkbp:engineType |
gptkb:piston_engine
|
| gptkbp:exportedTo |
gptkb:Romania
|
| gptkbp:firstFlight |
1976
|
| gptkbp:height |
2.7 m
|
| gptkbp:landingGear |
retractable tricycle
|
| gptkbp:length |
7.745 m
|
| gptkbp:manufacturer |
gptkb:Yakovlev
|
| gptkbp:maximumSpeed |
285 km/h
|
| gptkbp:numberBuilt |
over 1,800
|
| gptkbp:numberOfEngines |
1
|
| gptkbp:origin |
gptkb:Soviet_Union
|
| gptkbp:primaryUser |
gptkb:DOSAAF
|
| gptkbp:produced |
1978–present
|
| gptkbp:range |
550 km
|
| gptkbp:role |
gptkb:trainer_aircraft
|
| gptkbp:usedFor |
aerobatic training
military pilot training |
| gptkbp:weight |
1,305 kg
|
| gptkbp:wingspan |
9.3 m
|
| gptkbp:bfsParent |
gptkb:Aeroflot
|
| gptkbp:bfsLayer |
6
|
| https://www.w3.org/2000/01/rdf-schema#label |
Yakovlev Yak-52
|