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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:bfsLayer
|
4
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gptkbp:bfsParent
|
gptkb:The_British_Air_Force
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gptkbp:aircraft_operated
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gptkb:aircraft
single-engine aircraft
77 kg/m²
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gptkbp:capacity
|
2
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gptkbp:certification
|
gptkb:EASA
|
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gptkbp:climb_rate
|
5 m/s
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gptkbp:cockpit
|
glass cockpit
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gptkbp:crew
|
gptkb:musical
|
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gptkbp:design
|
low-wing monoplane
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gptkbp:engine
|
Rotax 912
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gptkbp:engine_type
|
four-stroke engine
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gptkbp:features
|
high visibility cockpit
|
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gptkbp:first_flight
|
gptkb:1999
|
|
gptkbp:first_released
|
gptkb:2000
|
|
gptkbp:flaps
|
split flaps
|
|
gptkbp:fuel_capacity
|
120 L
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gptkbp:height
|
2.3 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Grobs G120 TP
|
|
gptkbp:introduced
|
gptkb:2000
|
|
gptkbp:is_used_by
|
various flight schools
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
8.1 m
|
|
gptkbp:manufacturer
|
gptkb:Grob_Aircraft
|
|
gptkbp:market
|
general aviation
|
|
gptkbp:material
|
gptkb:NACA_4412
aluminum construction
|
|
gptkbp:max_speed
|
200 km/h
|
|
gptkbp:max_takeoff_weight
|
300 m
1,200 kg
250 m
|
|
gptkbp:notable_users
|
gptkb:German_Air_Force
|
|
gptkbp:number_built
|
over 200
|
|
gptkbp:operational_history
|
used in various countries
|
|
gptkbp:origin
|
gptkb:government_agency
|
|
gptkbp:production_years
|
1999-present
|
|
gptkbp:propulsion
|
variable pitch propeller
0.12 k W/kg
|
|
gptkbp:range
|
1,000 km
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:seating_capacity
|
400 kg
|
|
gptkbp:service_ceiling
|
4,500 m
|
|
gptkbp:speed
|
65 km/h
|
|
gptkbp:surface
|
elevator, ailerons, rudder
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:training
|
pilot training
basic flight training
|
|
gptkbp:variant
|
G120 TP-2
|
|
gptkbp:weight
|
750 kg
|
|
gptkbp:wing_area
|
15.5 m²
|
|
gptkbp:wingspan
|
11.0 m
|