C-130J HERCULES

Mission

The C-130 Hercules primarily performs the tactical portion 
of the airlift mission. The aircraft is capable of operating 
from rough, dirt strips and is the prime transport for air 
dropping troops and equipment into hostile areas. The C-130 
operates throughout the U.S. Air Force, serving with Air 
Mobility Command (stateside based), Air Force Special 
Operations Command, theater commands, Air National Guard and 
the Air Force Reserve Command, fulfilling a wide range of 
operational missions in both peace and war situations. Basic 
and specialized versions of the aircraft airframe perform a 
diverse number of roles, including airlift support, Antarctic 
ice resupply, aeromedical missions, weather reconnaissance, 
aerial spray missions, fire-fighting duties for the U.S. 
Forest Service and natural disaster relief missions.

Features
Using its aft loading ramp and door the C-130 can accommodate 
a wide variety of oversized cargo, including everything from 
utility helicopters and six-wheeled armored vehicles to 
standard palletized cargo and military personnel. In an aerial 
delivery role, it can airdrop loads up to 42,000 pounds or use 
its high-flotation landing gear to land and deliver cargo on 
rough, dirt strips.

The flexible design of the Hercules enables it to be configured 
for many different missions, allowing for one aircraft to perform 
the role of many. Much of the special mission equipment added to 
the Hercules is removable, allowing the aircraft to revert back 
to its cargo delivery role if desired. Additionally, the C-130 
can be rapidly reconfigured for the various types of cargo such 
as palletized equipment, floor-loaded material, airdrop platforms, 
container delivery system bundles, vehicles and personnel or 
aeromedical evacuation.

The C-130J is the latest addition to the C-130 fleet and will 
replace aging C-130E's. The C-130J incorporates state-of-the-art 
technology to reduce manpower requirements, lower operating and 
support costs, and provides life-cycle cost savings over earlier 
C-130 models. Compared to older C-130s, the J model climbs faster 
and higher, flies farther at a higher cruise speed, and takes off 
and lands in a shorter distance. The C-130J-30 is a stretch 
version, adding 15 feet to fuselage, increasing usable space in 
the cargo compartment.

C-130J/J-30 major system improvements include: advanced two-pilot 
flight station with fully integrated digital avionics; color 
multifunctional liquid crystal displays and head-up displays; 
state-of-the-art navigation systems with dual inertial navigation 
system and global positioning system; fully integrated defensive 
systems; low-power color radar; digital moving map display; new 
turboprop engines with six-bladed, all-composite propellers; 
digital auto pilot; improved fuel, environmental and ice-protection 
systems; and an enhanced cargo-handling system.

Background
Four decades have elapsed since the Air Force issued its original 
design specification, yet the remarkable C-130 remains in production. 
The initial production model was the C-130A, with four Allison 
T56-A-11 or -9 turboprops. A total of 219 were ordered and deliveries 
began in December 1956. The C-130B introduced Allison T56-A-7 
turboprops and the first of 134 entered Air Force service in May 1959. 

Introduced in August of 1962, the 389 C-130E's that were ordered used 
the same Allison T56-A-7 engine, but added two 1,290 gallon external 
fuel tanks and an increased maximum takeoff weight capability. June 
1974 introduced the first of 308 C-130H's with the more powerful 
Allison T56-A-15 turboprop engine. Nearly identical to the C-130E 
externally, the new engine brought major performance improvements to 
the aircraft. 

The latest C-130 to be produced, the C-130J entered the inventory in 
February 1999. With the noticeable difference of a six-bladed composite 
propeller coupled to a Rolls-Royce AE2100D3 turboprop engine, the C-130J 
brings substantial performance improvements over all previous models, 
and has allowed the introduction of the C-130J-30, a stretch version 
with a 15-foot fuselage extension. Air Force has selected the C-130J-30 
to replace retiring C-130E's. Approximately 168 C-130J/J-30s are planned 
for the inventory. To date, the Air Force has taken delivery of 32 C-130J 
aircraft from Lockheed Martin Aeronautics Company with orders for 
approximately 46 more aircraft.

General Characteristics
Primary Function: Global airlift
Contractor: Lockheed Martin Aeronautics Company
Power Plant: 
C-130E: Four Allison T56-A-7 turboprops; 4,200 prop shaft horsepower
C-130H: Four Allison T56-A-15 turboprops; 4,591prop shaft horsepower
C-130J: Four Rolls-Royce AE 2100D3 turboprops; 4,700 horsepower
Length: C-130E/H/J: 97 feet, 9 inches (29.3 meters)
C-130J-30: 112 feet, 9 inches (34.69 meters) 
Height: 38 feet, 10 inches (11. 9 meters)
Wingspan: 132 feet, 7 inches (39.7 meters)
Cargo Compartment: 
C-130E/H/J: length, 40 feet (12.31 meters); width, 119 inches (3.12 meters); 
height, 9 feet (2.74 meters). 
Rear ramp: length, 123 inches (3.12 meters); width, 119 inches (3.02 meters)
C-130J-30: length, 55 feet (16.9 meters); width, 119 inches (3.12 meters); 
height, 9 feet (2.74 meters).
Speed: 
C-130E: 345 mph/300 ktas (Mach 0.49) at 20,000 feet (6,060 meters)
C-130H: 366 mph/318 ktas (Mach 0.52) at 20,000 feet (6,060 meters)
C-130J: 417 mph/362 ktas (Mach 0.59) at 22,000 feet (6,706 meters)
C-130J-30: 410 mph/356 ktas (Mach 0.58) at 22,000 feet (6,706 meters)
Ceiling:
C-130J: 28,000 feet (8,615 meters) with 42,000 pounds (19,090 kilograms) payload
C-130J-30: 26,000 feet (8,000 meters) with 44,500 pounds (20,227 kilograms) payload.
C-130H: 23,000 feet (7,077 meters) with 42,000 pounds (19,090 kilograms) payload.
C-130E: 19,000 feet (5,846 meters) with 42,000 pounds (19,090 kilograms) payload
Maximum Takeoff Weight: 
C-130E/H/J: 155,000 pounds (69,750 kilograms)
C-130J-30: 164,000 pounds (74,393 kilograms) 
Maximum Allowable Payload: 
C-130E, 42,000 pounds (19,090 kilograms)
C-130H, 42,000 pounds (19,090 kilograms)
C-130J, 42,000 pounds (19,090 kilograms) 
C-130J-30, 44,000 (19,958 kilograms)
Maximum Normal Payload: 
C-130E, 36,500 pounds (16,590 kilograms) 
C-130H, 36,500 pounds (16,590 kilograms) 
C-130J, 34,000 pounds (15,422 kilograms) 
C-130J-30, 36,000 pounds (16,329 kilograms)
Range at Maximum Normal Payload: 
C-130E, 1,150 miles (1,000 nautical miles)
C-130H, 1,208 miles (1,050 nautical miles)
C-130J, 2,071 miles (1,800 nautical miles)
C-130J-30, 1,956 miles (1,700 nautical miles)
Range with 35,000 pounds of Payload: 
C-130E, 1,438 miles (1,250 nautical miles)
C-130H, 1,496 miles (1,300 nautical miles)
C-130J, 1,841 miles (1,600 nautical miles)
C-130J-30, 2,417 miles (2,100 nautical miles)
Maximum Load: 
C-130E/H/J: 6 pallets or 74 litters or 16 CDS bundles or 
92 combat troops or 64 paratroopers, or a combination of 
any of these up to the cargo compartment capacity or 
maximum allowable weight.
C-130J-30: 8 pallets or 97 litters or 24 CDS bundles or 
128 combat troops or 92 paratroopers, or a combination of 
any of these up to the cargo compartment capacity or 
maximum allowable weight.
Crew: C-130E/H: Five (two pilots, navigator, 
flight engineer and loadmaster)
C-130J/J-30: Three (two pilots and loadmaster)
Aeromedical Evacuation Role: Minimum medical crew of three 
is added (one flight nurse and two medical technicians). 
Medical crew may be increased to two flight nurses and four 
medical technicians as required by the needs of the patients.
Unit Cost: C-130E, $11.9, C-130H, $30.1, 
C-130J, $48.5 (FY 1998 constant dollars in millions)
Date Deployed: C-130A, Dec 1956; C-130B, May 1959; 
C-130E, Aug 1962; C-130H, Jun 1974; C-130J, Feb 1999
Inventory: Active force, 186; Air National Guard, 222; 
Air Force Reserve, 106


Copyright © 2001-2008
Intellectual Property
Charles E. Geck III
Founder/Owner/Publisher
GlobalSpecialOperations.com (TM)
Special Forces Assn.
Life Member #M-7514
All Rights Reserved

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