Grobs G120 TP

GPTKB entity

Statements (54)
Predicate Object
gptkbp:instance_of gptkb:aircraft
gptkbp:aircraft_operated gptkb:light_aircraft
gptkbp:aircraft_type single-engine aircraft
gptkbp:capacity 2
gptkbp:climb_rate 5 m/s
gptkbp:cockpit glass cockpit
gptkbp:control_surfaces elevator, ailerons, rudder
gptkbp:country_of_origin gptkb:Germany
gptkbp:crew gptkb:1
gptkbp:design low-wing monoplane
gptkbp:design_features high visibility cockpit
gptkbp:engine Rotax 912
gptkbp:engine_type four-stroke engine
gptkbp:first_delivery gptkb:2000
gptkbp:first_flight gptkb:1999
gptkbp:flaps split flaps
gptkbp:fuel_capacity 120 L
gptkbp:fuselage_material gptkb:NACA_4412
aluminum construction
gptkbp:height 2.3 m
https://www.w3.org/2000/01/rdf-schema#label Grobs G120 TP
gptkbp:introduced gptkb:2000
gptkbp:landing_distance 250 m
gptkbp:landing_gear tricycle gear
gptkbp:length 8.1 m
gptkbp:manufacturer gptkb:Grob_Aircraft
gptkbp:market general aviation
gptkbp:max_speed 200 km/h
gptkbp:max_takeoff_weight 1,200 kg
gptkbp:notable_users gptkb:German_Air_Force
gptkbp:number_built over 200
gptkbp:offers_certificate gptkb:EASA
gptkbp:operational_history used in various countries
gptkbp:payload_capacity 400 kg
gptkbp:production_years 1999-present
gptkbp:propeller variable pitch propeller
gptkbp:propulsion 0.12 k W/kg
gptkbp:range 1,000 km
gptkbp:related_aircraft gptkb:Boeing_707
gptkbp:role gptkb:trainer_aircraft
gptkbp:service_ceiling 4,500 m
gptkbp:stall_speed 65 km/h
gptkbp:tail_type T-tail
gptkbp:takeoff_distance 300 m
gptkbp:training pilot training
basic flight training
gptkbp:used_by various flight schools
gptkbp:variant G120 TP-2
gptkbp:weight 750 kg
gptkbp:wing_area 15.5 m²
gptkbp:wing_configuration 77 kg/m²
gptkbp:wingspan 11.0 m
gptkbp:bfsParent gptkb:The_British_Air_Force
gptkbp:bfsLayer 4