H135 P3

GPTKB entity

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