Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:aircraft
|
| gptkbp:aircraftType |
gptkb:aircraft
|
| gptkbp:configuration |
low-wing monoplane
|
| gptkbp:countryOfOrigin |
gptkb:Czechoslovakia
|
| gptkbp:crew |
2
|
| gptkbp:emptyWeight |
820 kg
|
| gptkbp:engine |
gptkb:Avia_M_137A
|
| gptkbp:enginePower |
180 hp
|
| gptkbp:engineType |
piston engine
|
| gptkbp:firstFlight |
1965
|
| gptkbp:height |
2.10 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
Zlin Z-526L
|
| gptkbp:landingGear |
retractable tailwheel
|
| gptkbp:length |
8.10 m
|
| gptkbp:manufacturer |
gptkb:Zlin_Aircraft
|
| gptkbp:maximumSpeed |
255 km/h
|
| gptkbp:maxTakeoffWeight |
1,050 kg
|
| gptkbp:primaryUse |
aerobatic training
sport flying |
| gptkbp:range |
600 km
|
| gptkbp:serviceCeiling |
4,000 m
|
| gptkbp:successor |
gptkb:Zlin_Z-726
|
| gptkbp:wingspan |
10.60 m
|
| gptkbp:bfsParent |
gptkb:Zlin_Z-526
|
| gptkbp:bfsLayer |
6
|