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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:bfsLayer
|
6
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gptkbp:bfsParent
|
gptkb:Lockheed_Martin_LM-100_J
|
|
gptkbp:aircraft_operated
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gptkb:starship
fixed-wing aircraft
high-wing
|
|
gptkbp:crew
|
2
|
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gptkbp:design
|
civilian cargo transport
|
|
gptkbp:developer
|
1960s
|
|
gptkbp:engine
|
gptkb:4
|
|
gptkbp:engine_type
|
turboprop
|
|
gptkbp:first_flight
|
gptkb:1964
|
|
gptkbp:fuel_capacity
|
6,000 pounds
|
|
gptkbp:height
|
38 feet 10 inches
|
|
gptkbp:historical_significance
|
first civilian version of the C-130
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
LM-100
|
|
gptkbp:introduced
|
gptkb:1964
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|
gptkbp:is_used_by
|
various military and civilian operators
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
96 feet 2 inches
|
|
gptkbp:logistics
|
transport oversized cargo
|
|
gptkbp:manufacturer
|
gptkb:Lockheed_Martin
|
|
gptkbp:max_speed
|
300 knots
|
|
gptkbp:max_takeoff_weight
|
155,000 pounds
130,000 pounds
|
|
gptkbp:modifications
|
various military and civilian modifications
|
|
gptkbp:notable_event
|
various accidents during service
|
|
gptkbp:notable_features
|
large cargo door
|
|
gptkbp:operational_range
|
1,500 miles with maximum payload
|
|
gptkbp:operational_status
|
retired from many operators
|
|
gptkbp:primary_user
|
airlines, military, humanitarian organizations
|
|
gptkbp:production_years
|
1964-1992
|
|
gptkbp:propulsion
|
turboprop engines
|
|
gptkbp:range
|
2,500 nautical miles
|
|
gptkbp:retirement_year
|
gptkb:1992
|
|
gptkbp:role
|
cargo transport
|
|
gptkbp:seating_capacity
|
roll-on/roll-off capability
3,000 cubic feet
42,000 pounds
|
|
gptkbp:service_ceiling
|
25,000 feet
|
|
gptkbp:status
|
some still in service
|
|
gptkbp:successor
|
gptkb:LM-100_J
|
|
gptkbp:surface
|
elevators, ailerons, rudder
|
|
gptkbp:variant
|
gptkb:Lockheed_C-130_Hercules
LM-100, LM-100 A, LM-100 J
|
|
gptkbp:wing_area
|
1,500 square feet
|
|
gptkbp:wingspan
|
132 feet 7 inches
|