MBB Bo 105 P

GPTKB entity

Statements (54)
Predicate Object
gptkbp:instance_of gptkb:helicopter
gptkbp:armament gptkb:none
gptkbp:crew gptkb:1
gptkbp:design_features high maneuverability
low noise levels
high altitude performance
retractable landing gear
fully articulated rotor system
versatile mission capabilities
two-blade tail rotor
two-blade main rotor
modular design for easy maintenance
glass cockpit in later variants
advanced avionics in later models
good visibility for pilot and passengers
safety features including crashworthy seats
gptkbp:diameter 10.70 m
gptkbp:engine_type gptkb:turbofan_engine
gptkbp:first_flight gptkb:1967
gptkbp:height 3.30 m
https://www.w3.org/2000/01/rdf-schema#label MBB Bo 105 P
gptkbp:length 11.68 m
gptkbp:manufacturer gptkb:MBB
gptkbp:max_speed 250 km/h
gptkbp:max_takeoff_weight 2,500 kg
gptkbp:notable_case various accidents and incidents during service
gptkbp:notable_features fenestron tail rotor
gptkbp:passenger_capacity gptkb:4
gptkbp:power_source 2 × Allison 250-C20 turboshaft engines
gptkbp:primary_user gptkb:German_Army
gptkb:German_Air_Force
gptkb:German_Police
search and rescue operations
firefighting services
private owners
tourism companies
various air ambulance services
news media organizations
gptkbp:produces 1970-2001
1,500 units
gptkbp:production_years gptkb:2001
gptkbp:range 600 km
gptkbp:role gptkb:helicopter
gptkbp:service_entry gptkb:1970
gptkbp:successor Eurocopter EC135
gptkbp:used_by various military and civilian operators
gptkbp:variant gptkb:MBB_Bo_105_LS
gptkb:MBB_Bo_105_PAH-1
gptkb:MBB_Bo_105_M
gptkb:MBB_Bo_105_CB
gptkb:MBB_Bo_105_D
gptkbp:weight 1,200 kg
gptkbp:bfsParent gptkb:MBB_Bo_105_D
gptkbp:bfsLayer 8