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EMC-32T

Triumph Group Systems & Support

The 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.

P/N: 2-170-580-02
NSN: 2915-01-371-9305
Cage Code: 11599
Engine: Honeywell T55-L-712F/-714
Vehicles: CH-47 Chinook

Need parts for the EMC-32T?

You can also call (603) 424-3111 to check availability.
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Rated speed: 4,200 rpm
Rated flow: 0 – 2,700 gpm
Discharge pressure: 450 psi
Inlet pressure: 0.45 V/L
Ambient temperature range: –65˚F to +260˚F
Fuel inlet temperature range: –65˚F to +160˚F
Primary fuel types: Jet A, Jet A-1, Jet B, JP-4, JP-5

Request a Quote

Interested in parts for the EMC-32T? Fill out the form below and we’ll get back to you within 1-3 business days with more information.
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To upload your own RFQ, or to add more information, please use our advanced quote form. You can also call or email the sales representative listed below.

Ken Foote
Vice President

Request a Quote

Interested in the EMC-32T? Fill out the form below and we’ll get back to you within 1-3 business days with more information.
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Name:*
Please enter a number greater than or equal to 1.

To upload your own RFQ, or to add more information, please use our advanced quote form. You can also call or email the sales representative listed below.

Ken Foote
Vice President