Statements (39)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:helicopter
|
| gptkbp:armament |
gptkb:TOW_missiles
|
| gptkbp:country_of_origin |
gptkb:Germany
|
| gptkbp:crew |
2
|
| gptkbp:design |
high speed
lightweight twin-engine high maneuverability low noise multi-role tandem rotor |
| gptkbp:engine |
gptkb:Allison_250-C20
|
| gptkbp:first_flight |
gptkb:1967
|
| https://www.w3.org/2000/01/rdf-schema#label |
MBB Bo 105 PAH
|
| gptkbp:introduced |
gptkb:1970
|
| gptkbp:length |
13.3 m
|
| gptkbp:manufacturer |
gptkb:MBB
|
| gptkbp:max_speed |
250 km/h
|
| gptkbp:number_built |
over 1,500
|
| gptkbp:range |
600 km
|
| gptkbp:retired |
2000s
|
| gptkbp:role |
gptkb:transportation
gptkb:training gptkb:helicopter reconnaissance medical evacuation |
| gptkbp:service_ceiling |
4,500 m
|
| gptkbp:used_by |
gptkb:Argentina
gptkb:Brazil gptkb:Germany gptkb:Netherlands gptkb:Pakistan gptkb:Philippines gptkb:South_Africa gptkb:Spain gptkb:United_States |
| gptkbp:variant |
gptkb:MBB_Bo_105_CB
|
| gptkbp:bfsParent |
gptkb:MBB_Bo_105_CB
|
| gptkbp:bfsLayer |
8
|