Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
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:engineType |
gptkb:piston_engine
|
| gptkbp:firstFlight |
1965
|
| gptkbp:height |
2.15 m
|
| gptkbp:landingGear |
tailwheel
|
| gptkbp:length |
8.10 m
|
| gptkbp:manufacturer |
gptkb:Zlin_Aircraft
|
| gptkbp:maximumSpeed |
255 km/h
|
| gptkbp:maxTakeoffWeight |
1,070 kg
|
| gptkbp:powerOutput |
180 hp
|
| gptkbp:primaryUse |
training
aerobatics |
| gptkbp:range |
600 km
|
| gptkbp:role |
gptkb:aircraft
|
| gptkbp:serviceCeiling |
4,000 m
|
| gptkbp:successor |
gptkb:Zlin_Z_726
|
| gptkbp:wingspan |
10.60 m
|
| gptkbp:bfsParent |
gptkb:Zlin_Z_526
|
| gptkbp:bfsLayer |
8
|
| http://www.w3.org/2000/01/rdf-schema#label |
Zlin Z 526L
|