There are 2 images added between 8 November 2010 and 17 September 2012
Initial Operational Capability (IOC):
Total Production: ?
Also Known As: T56-A-14
Origin: United Kingdom
Corporations: Rolls-Royce
Parent System: T56
Initial Operational Capability (IOC):
Total Production: 17,000
Family Members: T56-A-16, T56-A-17, T56-A-425, T56-A-427, T56-A-501D and T56-A-7
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Description: The T56 engine is the leading large turboprop in the world on the basis of units sold. It is reliable and robust and has been installed in both civil and military aircraft.

In the military range, C-130, E-2 and P-3 are powered by this engine.

T56-A-15 Applications

Support Aircraft C-130H Hercules P-3C Orion

T56-A-15 Specifications

Max Power at TakeOff: 4,508 shp (3,363 kW)
Dry Weight: 828 kilogram (1,825 pound)
CEP: Circular Error Probable
Meters (m)   Kilometers (km)   Nautic Miles (nm)   Inch (in)   Yard (yd)   Foot (ft)   Millimeter (mm)
Pound (lb)   Kilogram (kg)   kN (KiloNewton)   Ton (t)
Meters per Second (mps)   Kilometers per Hour (kph)   Knot (kt)   Miles per Hour (mph)
Liter (l)   Galon (gl)
Year (yr)   Minutes (min)   Second (sec)
Shaft-Horse-Power (shp)

T56-A-15 News

There are 2 news between
22 Jun 2011 and 17 Sep 2012
Monday, September 17, 2012USAF C-130H Completes First Flight with T56 Series 3.5 Engines
Wednesday, June 22, 2011Rolls-Royce and Lockheed Martin Sign Engine Fuel Efficiency Agreement

Operators & Related Equipment


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