Statements (31)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:aircraft
|
| gptkbp:configuration |
side-by-side seating
|
| gptkbp:countryOfOrigin |
gptkb:Czech_Republic
|
| gptkbp:crew |
2
|
| gptkbp:developedBy |
gptkb:Zlin_Z-42
|
| gptkbp:emptyWeight |
770 kg
|
| gptkbp:engine |
gptkb:Lycoming_AEIO-360
|
| gptkbp:engineType |
piston engine
|
| gptkbp:firstFlight |
1979
|
| gptkbp:fuelType |
130 liters
|
| gptkbp:height |
2.72 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
Zlin Z242L
|
| gptkbp:landingGear |
fixed tricycle
|
| gptkbp:length |
7.02 m
|
| gptkbp:manufacturer |
gptkb:Zlin_Aircraft
|
| gptkbp:maximumSpeed |
285 km/h
|
| gptkbp:maxTakeoffWeight |
1,150 kg
|
| gptkbp:numberOfEngines |
1
|
| gptkbp:propulsion |
2-bladed constant speed
|
| gptkbp:range |
950 km
|
| gptkbp:role |
gptkb:aircraft
gptkb:trainer_aircraft |
| gptkbp:serviceCeiling |
5000 m
|
| gptkbp:usedBy |
gptkb:Mexican_Air_Force
gptkb:Czech_Air_Force gptkb:Slovak_Air_Force other civil operators |
| gptkbp:variant |
Zlin Z-42 family
|
| gptkbp:wingspan |
9.8 m
|
| gptkbp:bfsParent |
gptkb:Indira_Gandhi_Rashtriya_Uran_Akademi
|
| gptkbp:bfsLayer |
7
|