Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:helicopter
|
| gptkbp:avionics |
gptkb:Garmin_G5000H
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:crew |
2
|
| gptkbp:emptyWeight |
6,123 kg
|
| gptkbp:engine |
gptkb:GE_CT7-2F1
|
| gptkbp:engineType |
turboshaft
|
| gptkbp:firstAppearance |
2012
|
| gptkbp:firstFlight |
2015-07-01
|
| gptkbp:height |
5.1 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
Bell Model 525
|
| gptkbp:intendedUse |
search and rescue
corporate transport offshore transport |
| gptkbp:length |
20.4 m
|
| gptkbp:manufacturer |
gptkb:Bell_Helicopter
|
| gptkbp:maximumSpeed |
287 km/h
|
| gptkbp:maxTakeoffWeight |
9,300 kg
|
| gptkbp:notableFeature |
first commercial fly-by-wire helicopter
|
| gptkbp:numberOfEngines |
2
|
| gptkbp:range |
926 km
|
| gptkbp:role |
medium-lift helicopter
|
| gptkbp:rotorConfiguration |
five-blade main rotor
|
| gptkbp:seatingCapacity |
up to 20
|
| gptkbp:status |
in development
|
| gptkbp:tailRotorType |
four-blade
|
| gptkbp:bfsParent |
gptkb:Bell_Textron
|
| gptkbp:bfsLayer |
6
|