|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:aircraft_configuration
|
twin boom tail design
|
|
gptkbp:aircraft_operated
|
gptkb:transport_aircraft
in service
|
|
gptkbp:aircraft_role
|
gptkb:transportation
|
|
gptkbp:aircraft_type
|
gptkb:ship
military and civilian transport aircraft
|
|
gptkbp:avionics
|
modernized in various upgrades
|
|
gptkbp:built
|
approximately 114 units
|
|
gptkbp:capacity
|
up to 45,000 pounds
|
|
gptkbp:cargo_capacity
|
42,000 lb
3,000 cubic feet
up to 92 passengers or 72 stretchers
|
|
gptkbp:cargo_types
|
rear ramp door
roll-on/roll-off capability
can be equipped with cargo handling systems
capable of rapid loading and unloading
|
|
gptkbp:crash_incidents
|
multiple incidents reported
|
|
gptkbp:crew
|
gptkb:3
|
|
gptkbp:design
|
allows for various configurations
high-wing, four-engine turboprop
|
|
gptkbp:design_features
|
high-wing design
|
|
gptkbp:drops
|
can perform aerial delivery missions
|
|
gptkbp:engine
|
4 × Allison T56-A-15 turboprop engines
|
|
gptkbp:engine_power
|
4,590 shp per engine
|
|
gptkbp:engine_type
|
turboprop
|
|
gptkbp:first_delivery
|
gptkb:1965
|
|
gptkbp:first_flight
|
gptkb:1964
|
|
gptkbp:fuel_capacity
|
23,000 lb
12,000 lb
|
|
gptkbp:global_presence
|
operated in many countries worldwide
|
|
gptkbp:height
|
38 ft 10 in
|
|
gptkbp:historical_significance
|
used in various humanitarian missions
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Lockheed L-100-30 Hercules
|
|
gptkbp:introduced
|
gptkb:1964
|
|
gptkbp:landing_distance
|
130,000 lb
|
|
gptkbp:landing_gear
|
tricycle gear
tricycle landing gear
|
|
gptkbp:length
|
97 ft 9 in
|
|
gptkbp:manufacturer
|
gptkb:Lockheed_Martin
|
|
gptkbp:max_speed
|
366 knots
|
|
gptkbp:max_takeoff_weight
|
155,000 lb
|
|
gptkbp:military_technology
|
gptkb:C-130_Hercules
C-130 variants used in combat
used for firefighting and disaster relief
L-100-20, L-100-30
|
|
gptkbp:modifications
|
various military and civilian modifications
|
|
gptkbp:notable_case
|
involved in several notable crashes.
|
|
gptkbp:notable_users
|
gptkb:Philippine_Air_Force
gptkb:Royal_Air_Force
gptkb:United_Nations
gptkb:United_States_Air_Force
gptkb:Hellenic_Air_Force
gptkb:Air_Force_of_Zimbabwe
Various cargo airlines
|
|
gptkbp:number_built
|
approximately 114
|
|
gptkbp:number_of_engines
|
gptkb:4
|
|
gptkbp:operational_history
|
used in various humanitarian missions
|
|
gptkbp:operational_range
|
1,500 nautical miles with max payload
2,500 nautical miles with max payload
|
|
gptkbp:operational_use
|
transport, medical evacuation, and reconnaissance
|
|
gptkbp:passenger_capacity
|
92
|
|
gptkbp:payload_capacity
|
45,000 lb
|
|
gptkbp:primary_user
|
civilian operators
|
|
gptkbp:production_years
|
1964-1992
1964 to 1992
|
|
gptkbp:range
|
2,500 nautical miles
2,400 nautical miles
|
|
gptkbp:related_aircraft
|
gptkb:Lockheed_C-130_family
|
|
gptkbp:retired
|
various dates
still in service with some operators
|
|
gptkbp:role
|
gptkb:military_logistics
gptkb:transport_aircraft
|
|
gptkbp:safety_record
|
varied by operator
|
|
gptkbp:service_ceiling
|
25,000 ft
|
|
gptkbp:successor
|
gptkb:Lockheed_Martin_C-130_J_Super_Hercules
gptkb:Lockheed_Martin_LM-100_J
|
|
gptkbp:tail_type
|
T-tail configuration
|
|
gptkbp:used_by
|
gptkb:United_States_Air_Force
various airlines
|
|
gptkbp:variant
|
gptkb:Lockheed_C-130_Hercules
|
|
gptkbp:wing_area
|
1,745 ft²
1,745 sq ft
|
|
gptkbp:wing_configuration
|
high-wing
high-wing, cantilever design
|
|
gptkbp:wingspan
|
132 ft 7 in
|