Statements (54)
Predicate | Object |
---|---|
gptkbp:instance_of |
gptkb:helicopter
|
gptkbp:bfsLayer |
5
|
gptkbp:bfsParent |
gptkb:Rolls-Royce_250
gptkb:Rolls-Royce_250-C20_R gptkb:T63_turboshaft |
gptkbp:capacity |
gptkb:5
|
gptkbp:crew |
gptkb:musical
|
gptkbp:design |
light helicopter
|
gptkbp:engine_type |
turboshaft
|
gptkbp:first_flight |
gptkb:1966
|
gptkbp:height |
3.05 m
|
https://www.w3.org/2000/01/rdf-schema#label |
Mc Donnell Douglas MD 500
|
gptkbp:introduced |
gptkb:1968
|
gptkbp:is_used_by |
gptkb:military_unit
|
gptkbp:length |
11.68 m
|
gptkbp:manufacturer |
gptkb:Mc_Donnell_Douglas
|
gptkbp:max_speed |
222 km/h
|
gptkbp:notable_features |
lightweight construction
advanced avionics high maneuverability low noise levels reliable performance easy maintenance low operating costs good visibility high altitude performance proven track record adaptable to various environments good fuel efficiency various engine options excellent stability versatile configurations twin-blade rotor system customizable payloads tail rotor design wide range of missions |
gptkbp:number_built |
over 1,000
|
gptkbp:primary_user |
gptkb:aircraft
gptkb:military_unit gptkb:battle search and rescue operations law enforcement agencies medical evacuation services firefighting services commercial operators news media organizations |
gptkbp:range |
500 km
|
gptkbp:role |
gptkb:helicopter
|
gptkbp:service_ceiling |
3,000 m
|
gptkbp:successor |
gptkb:MD_530_F
|
gptkbp:variant |
gptkb:MD_500_C
gptkb:MD_500_D gptkb:MD_500_E gptkb:MD_500_N |