Statements (54)
Predicate | Object |
---|---|
gptkbp:instance_of |
gptkb:helicopter
|
gptkbp:avionics |
modern glass cockpit
|
gptkbp:configuration |
twin-engine
|
gptkbp:crew |
1-2
|
gptkbp:diameter |
11.0 m
|
gptkbp:engine_type |
twin-engine
|
gptkbp:features |
gptkb:Cooler
modular design advanced communication systems high maneuverability real-time data monitoring low noise levels reduced operational costs advanced safety systems advanced navigation systems low vibration levels multi-role capabilities high visibility cockpit high altitude performance easy maintenance access high payload capacity night vision compatibility automatic flight control system flexible cabin configuration digital flight control system excellent hover performance helicopter emergency egress system wireless data transfer capabilities |
gptkbp:first_flight |
gptkb:1994
|
gptkbp:height |
3.6 m
|
https://www.w3.org/2000/01/rdf-schema#label |
H135 P3
|
gptkbp:length |
13.1 m
|
gptkbp:manufacturer |
gptkb:Airbus
|
gptkbp:max_speed |
250 km/h
|
gptkbp:max_takeoff_weight |
3,175 kg
|
gptkbp:military_technology |
yes
|
gptkbp:notable_operators |
gptkb:Airbus
gptkb:emergency_services gptkb:military_forces police forces |
gptkbp:passenger_capacity |
up to 7
|
gptkbp:power_source |
2 x Turbomeca Arrius 2 B2
|
gptkbp:primary_use |
medical evacuation
|
gptkbp:produces |
ongoing
|
gptkbp:range |
600 km
|
gptkbp:role |
gptkb:helicopter
|
gptkbp:safety_record |
generally good
|
gptkbp:service_entry |
gptkb:1996
|
gptkbp:variant |
H135 T3
H135 P3 H H135 P3 M |
gptkbp:weight |
2,900 kg
|
gptkbp:bfsParent |
gptkb:Airbus
|
gptkbp:bfsLayer |
4
|