Statements (80)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:aircraft
|
| gptkbp:bfsLayer |
5
|
| gptkbp:bfsParent |
gptkb:No._43_Squadron_RNZAF
|
| gptkbp:capacity |
2
|
| gptkbp:certification |
gptkb:EASA_Type_Certificate
|
| gptkbp:cockpit |
glass cockpit
|
| gptkbp:controls |
dual control
|
| gptkbp:crew |
gptkb:musical
|
| gptkbp:design |
basic trainer
|
| gptkbp:engine |
Rotax 912
|
| gptkbp:first_flight |
gptkb:1999
|
| gptkbp:fuel_capacity |
120 L
|
| gptkbp:height |
2.3 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
Grob G120 A
|
| gptkbp:introduced |
gptkb:2000
|
| gptkbp:landing_gear |
tricycle gear
|
| gptkbp:length |
8.1 m
|
| gptkbp:manufacturer |
gptkb:Grob_Aircraft
|
| gptkbp:material |
low-wing
|
| gptkbp:max_speed |
200 km/h
|
| gptkbp:max_takeoff_weight |
1,200 kg
|
| gptkbp:number_built |
over 200
|
| gptkbp:primary_user |
air forces
|
| gptkbp:propulsion |
variable-pitch propeller
|
| gptkbp:range |
1,000 km
|
| gptkbp:service_ceiling |
4,500 m
|
| gptkbp:speed |
65 km/h
|
| gptkbp:successor |
gptkb:Grob_G120_TP
|
| gptkbp:type |
gptkb:aircraft
|
| gptkbp:variant |
G120 A-10
G120 A-11 G120 A-12 G120 A-13 G120 A-14 G120 A-15 G120 A-16 G120 A-17 G120 A-18 G120 A-19 G120 A-2 G120 A-20 G120 A-21 G120 A-22 G120 A-23 G120 A-24 G120 A-25 G120 A-26 G120 A-27 G120 A-28 G120 A-29 G120 A-3 G120 A-30 G120 A-31 G120 A-32 G120 A-33 G120 A-34 G120 A-35 G120 A-36 G120 A-37 G120 A-38 G120 A-39 G120 A-4 G120 A-40 G120 A-41 G120 A-42 G120 A-43 G120 A-44 G120 A-45 G120 A-46 G120 A-47 G120 A-48 G120 A-49 G120 A-5 G120 A-50 G120 A-6 G120 A-7 G120 A-8 G120 A-9 |
| gptkbp:wing_area |
14.5 m²
|
| gptkbp:wingspan |
10.5 m
|