SUPPLYING TURBINE ENGINES, PARTS & SUPPORT SINCE 1972 For nearly fifty years, Transupport’s engine support has grown from locally to encompassing the globe. Our team of specialists have developed a world-wide network, locating and distributing hard to find parts, major components and complete engines. Situated on a 13 acre parcel of property in southern New Hampshire, Transupport houses over 50,000 square feet of engines and spares.

This gas turbine engine design is a scaled-up version of the T53 turboshaft and produces more than three times the shaft horsepower of its predecessor. The T55 turboshaft also came out of the Lycoming Turbine Engine Division in Stratford, Connecticut, and has operated for over 60 years. Transupport offers same day quoting/shipping for any T-55 parts, engines or support. Vehicles: CH-47 Chinook

The 2-170-700-21 (Triumph PN EMC-100) is a sophisticated, low cost, dual channel engine control in a single housing. The unit consists of two dissimilar, mechanically separated channels operating independently, but cooperating with each other. The software is organized in a multi-partition architecture which includes COTS real-time operating and application specific control system software. Most of the software has been developed to RTCA/DO-178B Level A (flight critical standard), but the software architecture permits partitions which perform non-critical functions to be developed to lower levels, thereby reducing life-cycle costs.

The 2-170-580-02 (Triumph PN EMC-32T) is a dual channel Full Authority Digital Engine Control (FADEC) system, designed for helicopter turboshaft engines. The Electronic Control Unit’s (ECU) primary channel provides precise engine power management and rotor speed control throughout the operational range of the engine. The reversionary backup channel provides full mission capability should a primary system failure occur. The Hydromechanical Unit accurately meters the engine fuel flow commanded by the ECU in both primary and reversionary mode operation. Additional functions provided by the HMU include electrical power generation, compressor air bleed management, and positive engine shutoff.

The 4155T12P09 (Triumph PN EMC-102) EDECU is configured as a common supervisory engine control for both T700-GE-701C/D and T700-GE-401C applications. Slated for use by the Army on current field models of Black Hawk helicopters, the control is configured with modern electronics, allowing for a more reliable alternative to the present UH-60 Black Hawk control and is also compatible with the AH-64 Apache. The control unit is qualified to the latest Army requirements for superior operability in adverse environments.

Triumph Systems, Electronics & Controls is the global leader in manufacturing and overhauling aerospace structures, systems, and components. Transupport works directly with their Systems, Electronics & Controls division in West Hartford, Connecticut being an Authorized Distributor since 1987.