Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:helicopter
|
| gptkbp:crew |
2
|
| gptkbp:diameter |
14.63 m
|
| gptkbp:engine_type |
gptkb:turbofan_engine
|
| gptkbp:first_flight |
gptkb:1968
|
| gptkbp:height |
4.57 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
Bell 212 Z
|
| gptkbp:length |
15.24 m
|
| gptkbp:manufacturer |
gptkb:Bell_Helicopter
|
| gptkbp:max_speed |
130 knots
|
| gptkbp:notable_features |
twin-engine design
|
| gptkbp:passenger_capacity |
gptkb:15
|
| gptkbp:power_output |
1,400 shp
|
| gptkbp:primary_user |
Canada, United States
|
| gptkbp:production_years |
1968-1988
|
| gptkbp:range |
400 nautical miles
|
| gptkbp:role |
gptkb:helicopter
|
| gptkbp:service_entry |
gptkb:1971
|
| gptkbp:successor |
gptkb:Bell_412
|
| gptkbp:used_by |
military and civilian operators
|
| gptkbp:variant |
gptkb:Bell_204
|
| gptkbp:weight |
3,175 kg
|
| gptkbp:bfsParent |
gptkb:Bell_212
|
| gptkbp:bfsLayer |
6
|