Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:certification |
gptkb:EASA
|
| gptkbp:configuration |
single-shaft
|
| gptkbp:countryOfOrigin |
gptkb:Czech_Republic
|
| gptkbp:diameter |
0.5 m
|
| gptkbp:firstFlight |
1967
|
| gptkbp:fuelType |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Walter M601 turboprop
|
| gptkbp:length |
1.7 m
|
| gptkbp:manufacturer |
gptkb:Walter_Aircraft_Engines
|
| gptkbp:numberOfEngines |
6
|
| gptkbp:powerOutput |
580 shp
|
| gptkbp:successor |
gptkb:GE_H80
|
| gptkbp:usedInAircraft |
gptkb:Let_L-410_Turbolet
gptkb:PZL_M-18_Dromader gptkb:Ayres_Thrush |
| gptkbp:variant |
M601A
M601B M601D M601E |
| gptkbp:weight |
200 kg
|
| gptkbp:bfsParent |
gptkb:PZL-294
|
| gptkbp:bfsLayer |
6
|