Statements (57)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
aircraft
|
| gptkbp:aircraft |
cantilever wing
|
| gptkbp:cockpit |
glass cockpit
|
| gptkbp:constructionMaterial |
composite
NACA 4412 |
| gptkbp:controls |
flaps
ailerons elevator rudder trim tabs |
| gptkbp:covers |
split flaps
|
| gptkbp:crew |
1
|
| gptkbp:design |
low-wing monoplane
|
| gptkbp:emergencyServices |
ballistic parachute
|
| gptkbp:engine |
Rotax 912
|
| gptkbp:firstFlight |
1999
|
| gptkbp:fuelCapacity |
100 L
|
| gptkbp:headlights |
composite
T-tail |
| gptkbp:height |
2.5 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
Grob G120
|
| gptkbp:landingGear |
tricycle gear
retractable landing gear |
| gptkbp:length |
8.1 m
|
| gptkbp:manufacturer |
gptkb:Grob_Aircraft
|
| gptkbp:market |
global
|
| gptkbp:marketSegment |
general aviation
military training commercial pilot training |
| gptkbp:maxSpeed |
200 km/h
|
| gptkbp:maxTakeoffWeight |
1,200 kg
|
| gptkbp:notableFeature |
advanced avionics
easy maintenance low operating costs high visibility cockpit good handling characteristics |
| gptkbp:numberBuilt |
over 200
|
| gptkbp:passengerCapacity |
2
|
| gptkbp:primaryUser |
flight schools
|
| gptkbp:productionStartYear |
1999
|
| gptkbp:productionYears |
present
|
| gptkbp:propulsion |
variable-pitch propeller
|
| gptkbp:range |
1,000 km
|
| gptkbp:role |
pilot training
|
| gptkbp:safety |
high
|
| gptkbp:services |
4,500 m
|
| gptkbp:speed |
65 km/h
|
| gptkbp:supportRole |
basic flight training
aerobatic training advanced flight training instrument training |
| gptkbp:type |
trainer aircraft
|
| gptkbp:variant |
G120A
G120B G120TP |
| gptkbp:wingArea |
15.5 m²
|
| gptkbp:wingspan |
10.5 m
|