|
gptkbp:instanceOf
|
aircraft
|
|
gptkbp:avionics
|
modern avionics
|
|
gptkbp:climbRate
|
5 m/s
|
|
gptkbp:cockpit
|
glass cockpit
|
|
gptkbp:controls
|
ailerons
elevator
rudder
|
|
gptkbp:covers
|
yes
|
|
gptkbp:crew
|
1
|
|
gptkbp:design
|
training
lightweight construction
high aspect ratio wings
low-wing design
|
|
gptkbp:emergencyServices
|
parachute system
|
|
gptkbp:engineType
|
turboprop
|
|
gptkbp:firstFlight
|
1995
|
|
gptkbp:fuelCapacity
|
150 L
|
|
gptkbp:height
|
1.5 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Grob G520
|
|
gptkbp:landingGear
|
tricycle
|
|
gptkbp:length
|
8.5 m
|
|
gptkbp:manufacturer
|
gptkb:Grob_Aircraft_AG
|
|
gptkbp:market
|
civil aviation
|
|
gptkbp:maxSpeed
|
200 km/h
|
|
gptkbp:maxTakeoffWeight
|
750 kg
|
|
gptkbp:notableUsers
|
flight schools
private owners
aerobatic teams
|
|
gptkbp:numberBuilt
|
200
|
|
gptkbp:numberOfEpisodes
|
1
|
|
gptkbp:performance
|
good stability
excellent maneuverability
high lift capability
|
|
gptkbp:productionYears
|
1995-2000
|
|
gptkbp:range
|
1000 km
|
|
gptkbp:regulatoryCompliance
|
EASA_standards
FAA_standards
|
|
gptkbp:relatedModel
|
gptkb:Grob_G120
gptkb:Grob_G150
Grob_G109
|
|
gptkbp:role
|
aerobatics
|
|
gptkbp:services
|
5000 m
|
|
gptkbp:speed
|
60 km/h
|
|
gptkbp:successor
|
Grob_G540
|
|
gptkbp:targetMarket
|
private pilots
flight schools
aerobatic teams
|
|
gptkbp:trimLevels
|
yes
|
|
gptkbp:type
|
glider
|
|
gptkbp:weight
|
400 kg
|
|
gptkbp:wingArea
|
20 m²
|
|
gptkbp:wingspan
|
20 m
|