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C-130E Hercules American Transport Aircraft

C-130E

Twin-Engine Utility Aircraft
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Basic Information
Name
C-130E Hercules American Transport Aircraft
Designation
C-130E
Alternate Designation
Equipment Type
Twin-Engine Utility Aircraft
Manufacturer
Lockheed Martin
Date of Introduction
1962
Description

Introduced in August 1962, the C-130E conducted critical United States Air Force (USAF) missions during the Vietnam War through the wars in Afghanistan and Iraq. It also supported countless USAF humanitarian efforts around the globe and in all climates. Originally designed by Lockheed as an assault transport capable of operating from unpaved airstrips, the C-130 Hercules made its first flight in August 1954. Over the next half century, the USAF used various versions of this versatile aircraft for aeromedical evacuation, mid-air refueling of helicopters, mid-air space capsule recovery, search and rescue, reconnaissance, as a gunship, and for many other missions. The C-130E (serial number 63-7868) on display entered service in April 1964. It had a long career, including extensive service in Southeast Asia during the Vietnam War for both the USAF and Air America. Before the Vietnam War, 7868 participated in Operation Red Dragon, the deployment of Belgian paratroopers and the rescue of hostages in the Congo in November 1964. The aircraft’s last assignment was to Little Rock Air Force Base, Arkansas, where it was used for aircrew training.

Air & Air Defense Specifications
Crew 5
Engine Turboprop (4200 hp)
Max Speed 555.0 km/h
Variants
C-130A/B/E/F/G/H/K/T Tactical airlifter basic models
C-130A-II Dreamboat Early version Electronic Intelligence/Signals Intelligence (ELINT/SIGINT) aircraft
C-130J Super Hercules Tactical airlifter, with new engines, avionics, and updated systems
C-130B BLC A one-off conversion of C-130B 58-0712, modified with a double Allison YT56 gas generator pod under each outer wing, to provide bleed air for all the control surfaces and flaps.
C-130K Designation for RAF Hercules C1/W2/C3 aircraft (C-130Js in RAF service are the Hercules C.4 and Hercules C.5)
AC-130A/E/H/J/U/W Gunship variants
C-130D/D-6 Ski-equipped version for snow and ice operations United States Air Force / Air National Guard
CC-130E/H/J Hercules Designation for Canadian Armed Forces / Royal Canadian Air Force Hercules aircraft. U.S. Air Force used the CC-130J designation to differentiate the standard C-130J variant from the "stretched" C-130J (company designation C-130J-30).
C-130M Designation used by the Brazilian Air Force for locally modified / up-graded C-130H aircraft.
DC-130A/E/H USAF and USN Drone control
EC-130 EC-130E/J Commando Solo – USAF / Air National Guard psychological operations version
GC-130 Permanently grounded instructional airframes
JC-130 Temporary conversion for flight test operations; used to recover drones and spy satellite film capsules.
KC-130F/R/T/J United States Marine Corps aerial refueling tanker and tactical airlifter
LC-130F/H/R USAF / Air National Guard – Ski-equipped version for Arctic and Antarctic support operations; LC-130F and R previously operated by USN
MC-130 Special operations infiltration/extraction variant
NC-130 Permanent conversion for flight test operations
PC-130/C-130-MP Maritime patrol
RC-130A/S Surveillance aircraft for reconnaissance
Surveillance aircraft for reconnaissance Proposed maritime patrol version of the C-130J, designed for coastal surveillance and anti-submarine warfare.
TC-130 Aircrew training
VC-130H VIP transport
WC-130A/B/E/H/J Weather reconnaissance ("Hurricane Hunter") version for USAF / Air Force Reserve Command's 53d Weather Reconnaissance Squadron in support of the National Weather Service's National Hurricane Center
System
Alternate Designation(s) C-130E Hercules
Type Transport Aircraft
Manufacturer Lockheed Corporation Lockheed Martin
Crew 5 (two pilots, navigator, flight engineer, radio operator/loadmaster)
Passengers 92 troops; or 64 paratroops; or 74 litters and 2 attendants
Maximum Payload Capacity 1,850 km
Number of Engines 4
Number of Hard Points INA
Dimensions
Length 29.79 m
Width (Wing Span) 40.41 m
Wing Area 162.12 m sq
Height 11.84 m
Ramp Opening, Length 3.12 m
Ramp Opening, Width 3.02 m
Cargo Hold, Length 12.31 m
Cargo Hold, Height 2.74 m
Cargo Hold, Width 3.02 m
Cargo Volume 127.4 cu m
Weight, Unloaded 34,686 kg
Maximum Takeoff Weight 69,750 kg
Automotive
Engine Name 4 x Allison T56-A-7
Engine Type Turboprop
Engine Power 4,200 shp each
Fuel Capacity 36,636 liters internal
Maximum Speed 555 km/h
Economy Speed INA
Stall Speed 185 km/h
Ceiling 5,846 m
Takeoff Run 1,091 m
Landing Run 518 m
Rate of Climb 579 m/min
Range, with Maximum Payload 1,940 km
Fire Control / Avionics
Navigation Radar AN/APN-241 weather and navigational radar.
Protection
Stealth Properties None
Heat Signature Reduction No
Add on Armor INA
NBC Protection INA
EW Counter Measures INA
Chaffs/Flares Yes
Details
Country of Origin United States
Category Fixed Wing Aircraft
Air > Fixed Wing Aircraft
Filter Label
C
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
29.79 m
Width
40.41 m
Height
11.84 m
Weight
34686 kg
Operators (12)
Israel
Poland
Sweden
Turkey
Iran
Pakistan
Brazil
Argentina
Ecuador
Iraq
Jordan
Mexico
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