Rolls-Royce Allison T56 is a single shaft, modular design military turboprop with a 14 stage axial flow compressor driven by a four stage turbine. It was originally developed by the Allison Engine Company for the Lockheed C-130 transport entering production in 1954. It is now produced under Rolls-Royce which acquired Allison in 1995. The commercial version is designated 501-D. With an unusually long and numerous production run, over 18,000 engines have been produced since 1954, logging over 200 million flying hours.

General characteristics :
Type: Turboprop
Length: 146.1 in (3,711 mm)
Diameter: 27 in (690 mm)
Dry weight: 1,940 lb (880 kg)

Components :
Compressor: 14 stage axial flow
Combustors: 6 cylindrical flow-through
Turbine: 4 stage
Fuel type: JP8 2412 pounds per hour

Performance :
Maximum power output: 4,350 shp (3,915 kW) limited to 4,100
Turbine inlet temperature: 860°C
Power-to-weight ratio: 2.75:1 (shp/lb)

S&S Turbine Services Middle East LLC
No. 49 , DIP Dubai-UAE
POBOX: 450630/Dubai
Tel: +97 14 88 00 281
Fax: + 97 14 88 00 291
Mob: +97 150 55 16 779

Email: info@ssturbineme.com
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