Statements (32)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:helicopter
|
| gptkbp:capacity |
up to 10 passengers
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:crew |
1 or 2
|
| gptkbp:engine |
gptkb:Lycoming_LTS101
|
| gptkbp:engineType |
twin turboshaft
|
| gptkbp:firstFlight |
1976
|
| gptkbp:fuselageMaterial |
gptkb:aluminum_alloy
|
| gptkbp:height |
3.51 m
|
| gptkbp:introduced |
1979
|
| gptkbp:landingGear |
Retractable tricycle
|
| gptkbp:length |
13.39 m
|
| gptkbp:mainRotorDiameter |
two
11.28 m |
| gptkbp:manufacturer |
gptkb:Bell_Helicopter
|
| gptkbp:maximumSpeed |
230 km/h
|
| gptkbp:maxTakeoffWeight |
3,670 kg
|
| gptkbp:notableFor |
gptkb:Airwolf_TV_series
|
| gptkbp:numberBuilt |
199
|
| gptkbp:primaryUser |
civilian operators
|
| gptkbp:range |
693 km
|
| gptkbp:role |
gptkb:helicopter
|
| gptkbp:status |
retired
|
| gptkbp:successor |
gptkb:Bell_230
|
| gptkbp:tailRotorType |
two-bladed
|
| gptkbp:variant |
gptkb:Bell_222B
gptkb:Bell_222UT gptkb:Bell_222A |
| gptkbp:bfsParent |
gptkb:Bell_Textron
gptkb:Royal_Bahraini_Air_Force |
| gptkbp:bfsLayer |
6
|
| https://www.w3.org/2000/01/rdf-schema#label |
Bell 222
|