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 |
piston engine
|
gptkbp:exportedTo |
gptkb:Romania
|
gptkbp:firstFlight |
1976
|
gptkbp:height |
2.7 m
|
https://www.w3.org/2000/01/rdf-schema#label |
Yakovlev Yak-52
|
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 |
5
|