Statements (26)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:aircraft
|
| gptkbp:armament |
gptkb:none
|
| gptkbp:cockpit |
tandem seating
|
| gptkbp:crew |
gptkb:1
|
| gptkbp:engine |
PT6 A-25 A
|
| gptkbp:first_flight |
gptkb:1966
|
| gptkbp:fuel_capacity |
300 L
|
| https://www.w3.org/2000/01/rdf-schema#label |
PC-7
|
| gptkbp:introduced |
gptkb:1970
|
| gptkbp:landing_gear |
tricycle gear
|
| gptkbp:length |
8.4 m
|
| gptkbp:manufacturer |
gptkb:Pilatus_Aircraft
|
| gptkbp:max_speed |
300 km/h
|
| gptkbp:max_takeoff_weight |
1,600 kg
|
| gptkbp:number_built |
over 1,000
|
| gptkbp:primary_user |
gptkb:Swiss_Air_Force
|
| gptkbp:range |
1,500 km
|
| gptkbp:role |
gptkb:trainer_aircraft
|
| gptkbp:service_ceiling |
3,000 m
|
| gptkbp:type |
single-engine turboprop
|
| gptkbp:variant |
PC-9
|
| gptkbp:weight |
1,200 kg
|
| gptkbp:weight_limit |
1,600 kg
|
| gptkbp:wingspan |
10.8 m
|
| gptkbp:bfsParent |
gptkb:Royal_Netherlands_Air_Force
|
| gptkbp:bfsLayer |
5
|