Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:aircraft
|
| gptkbp:armament |
gptkb:M61A1_Vulcan_cannon
bombs air-to-air missiles air-to-surface missiles |
| gptkbp:countryOfOrigin |
gptkb:Taiwan
|
| gptkbp:crew |
1
|
| gptkbp:developedBy |
gptkb:AIDC_F-CK-1_Ching-Kuo
|
| gptkbp:firstFlight |
1989
|
| gptkbp:height |
4.42 m
|
| gptkbp:introduced |
1994
|
| gptkbp:length |
14.21 m
|
| gptkbp:manufacturer |
gptkb:Aerospace_Industrial_Development_Corporation
|
| gptkbp:maximumSpeed |
Mach 1.8
|
| gptkbp:maxTakeoffWeight |
12,247 kg
|
| gptkbp:nickname |
gptkb:Ching-Kuo
|
| gptkbp:powerplant |
2 × Honeywell F125-GA-100 turbofans
|
| gptkbp:primaryUser |
gptkb:Republic_of_China_Air_Force
|
| gptkbp:range |
1,100 km
|
| gptkbp:role |
multirole fighter
|
| gptkbp:status |
in service
|
| gptkbp:wingspan |
9.46 m
|
| gptkbp:bfsParent |
gptkb:F-CK-1_Ching-kuo
gptkb:AIDC_F-CK-1_Ching-Kuo gptkb:AIDC_F-CK-1_Ching-kuo |
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
F-CK-1A
|