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
|