C-Series

Behind the scenes there are squadrons of men and women supporting the Air Force. From the ground crews supporting the flyers to C-series aircraft there are thousands of airmen flying countless missions in support of us military. In this program you’ll see the awesome power of the AC-130, meet the crew of a C-5 Galaxy, then go behind the scenes as these men and women go about the business of keeping the US military at the top of its game.

General Characteristics C-5 Galaxy
Primary Function: Outsize cargo transport
Prime Contractor: Lockheed-Georgia Co.

Power Plant: Four General Electric TF-39 engines

Thrust: 43,000 pounds, each engine
Wingspan: 222.9 feet (67.89 meters)
Length: 247.1 feet (75.3 meters)
Height: 65.1 feet (19.84 meters)
Cargo Compartment: height , 13.5 feet (4.11 meters); width, 19 feet (5.79 meters); length, 143 feet, 9 in (43.8 meters)
Pallet Positions: 36
Maximum Cargo: 270,000 pounds (122,472 kilograms)
Maximum Takeoff Weight: 769,000 pounds (348,818 kilograms) (peacetime), 840,000 pounds (381,024 kilograms) (wartime)
Speed: 518 mph (.77 Mach)
Range: 6,320 nautical miles without air refueling; unlimited with in-flight refueling
Crew: 7 (pilot, co-pilot, two flight engineers and three loadmasters)
Unit Cost: C-5A - $152.8 million (fiscal 1998 constant dollars) C-5B - $179 million (fiscal 1998 constant dollars)
Deployed: C-5A - 1969, C-5B - 1980
Inventory:  Total force, 111

General Characteristics - AC-130
Primary Function: Close air support, air interdiction and force protection
Builder: Lockheed/Boeing Corp.
Power Plant: Four Allison T56-A-15 turboprop engines
Thrust: 4,910 shaft horsepower each engine
Wingspan: 132 feet, 7 inches (40.4 meters)
Length: 97 feet, 9 inches (29.8 meters)
Height: 38 feet, 6 inches (11.7 meters)
Speed: 300 mph (Mach .4) (at sea level)
Range: Approximately 1,300 nautical miles; unlimited with air refueling.
Ceiling: 25,000 feet (7,576 meters
Maximum Takeoff Weight: 155,000 pounds (69,750 kilograms)
Armament: AC-130H: 40mm and 105mm cannons; AC-130U: 40mm and 105mm cannons and 25mm gatling gun. AC-130Us are being retrofitted with 30mm Mk-44 single barrel cannons in place of the 40mm cannon and the 25mm gatling gun.
Crew: AC-130U - pilot, co-pilot, navigator, fire control officer, electronic warfare officer (officers) and flight engineer, TV operator, infrared detection set operator, loadmaster, four aerial gunners (enlisted)
Deployment Date: AC-130H, 1972; AC-130U, 1995
Unit Cost: AC-130H, $132.4 million; AC-130U, $190 million (fiscal 2001 constant dollars)

Inventory: Active duty, AC-130H, 8; AC-130U, 17; Reserve, 0; ANG, 0

General Characteristics - C-17 Globemaster
Primary Function: Cargo and troop transport
Prime Contractor: Boeing Company
Power Plant: Four Pratt & Whitney F117-PW-100 turbofan engines
Thrust: 40,440 pounds, each engine
Wingspan: 169 feet 10 inches (to winglet tips) (51.75 meters)
Length: 174 feet (53 meters)
Height: 55 feet 1 inch (16.79 meters)
Cargo Compartment: length, 88 feet (26.82 meters); width, 18 feet (5.48 meters); height, 12 feet 4 inches (3.76 meters)
Speed: 450 knots at 28,000 feet (8,534 meters) (Mach .76)
Service Ceiling: 45,000 feet at cruising speed (13,716 meters)
Range: Global with in-flight refueling
Crew: Three (two pilots and one loadmaster)
Aeromedical Evacuation Crew: A basic crew of five (two flight nurses and three medical technicians) is added for aeromedical evacuation missions.  Medical crew may be altered as required by the needs of patients
Maximum Peacetime Takeoff Weight: 585,000 pounds (265,352 kilograms)
Load: 102 troops/paratroops; 36 litter and 54 ambulatory patients and attendants; 170,900 pounds (77,519 kilograms) of cargo (18 pallet positions)
Unit Cost: Unit Cost: $202.3 million (fiscal 1998 constant dollars)
Date Deployed: June 1993
Inventory:  Active duty, 158; Air National Guard, 8; Air Force Reserve, 8 transport and training aircraft

General Characteristics – C-130 Hercules
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). Rear ramp: length, 123 inches (3.12 meters); width, 119 inches (3.02 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 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)
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: A basic crew of five (two flight nurses and three medical technicians) is added for aeromedical evacuation missions. Medical crew may be decreased or increased as required by the needs of 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