Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:helicopter
|
| gptkbp:bfsLayer |
5
|
| gptkbp:bfsParent |
gptkb:Bell_404
|
| gptkbp:armament |
gptkb:none
|
| gptkbp:crew |
2
|
| gptkbp:design |
twin-engine
|
| gptkbp:diameter |
10.7 meters
|
| gptkbp:engine_type |
gptkb:engine
|
| gptkbp:first_flight |
gptkb:1980
|
| gptkbp:fuel_capacity |
1,200 liters
|
| gptkbp:height |
3.5 meters
|
| https://www.w3.org/2000/01/rdf-schema#label |
Bell 404 A
|
| gptkbp:length |
12.5 meters
|
| gptkbp:manufacturer |
gptkb:Bell_Helicopter
|
| gptkbp:max_speed |
130 knots
|
| gptkbp:max_takeoff_weight |
4,500 kg
|
| gptkbp:primary_source |
gptkb:aircraft
|
| gptkbp:production_years |
1980-1990
|
| gptkbp:range |
400 nautical miles
|
| gptkbp:role |
gptkb:helicopter
|
| gptkbp:seating_capacity |
gptkb:6
|
| gptkbp:service_ceiling |
15,000 feet
|
| gptkbp:services |
gptkb:1981
|
| gptkbp:successor |
gptkb:Bell_407
|
| gptkbp:weight |
2,500 kg
|