Statements (32)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:aircraft
|
| gptkbp:configuration |
low-wing monoplane
|
| gptkbp:countryOfOrigin |
gptkb:Czechoslovakia
|
| gptkbp:crew |
2
|
| gptkbp:cruiseSpeed |
200 km/h
|
| gptkbp:developedBy |
gptkb:Zlin_Z-42
|
| gptkbp:emptyWeight |
770 kg
|
| gptkbp:engine |
gptkb:Avia_M_137A
|
| gptkbp:engineType |
piston engine
|
| gptkbp:firstFlight |
1967
|
| gptkbp:fuelType |
120 L
|
| gptkbp:height |
2.55 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
Zlin Z-42D
|
| gptkbp:landingGear |
fixed tricycle
|
| gptkbp:length |
7.28 m
|
| gptkbp:manufacturer |
gptkb:Zlin_Aircraft
|
| gptkbp:maximumSpeed |
230 km/h
|
| gptkbp:maxTakeoffWeight |
1,050 kg
|
| gptkbp:powerplant |
1 × Avia M 137A inline engine
|
| gptkbp:primaryUser |
flight schools
|
| gptkbp:range |
800 km
|
| gptkbp:role |
gptkb:aircraft
gptkb:trainer_aircraft |
| gptkbp:serviceCeiling |
4,000 m
|
| gptkbp:successor |
gptkb:Zlin_Z-242
|
| gptkbp:usedBy |
gptkb:Czech_Air_Force
gptkb:Hungarian_Air_Force gptkb:Slovak_Air_Force civilian operators |
| gptkbp:wingspan |
9.76 m
|
| gptkbp:bfsParent |
gptkb:Hungarian_Air_Force
|
| gptkbp:bfsLayer |
6
|