K-140 Control unit of the de-icing system of open-fan propulsors. 3.70-22656899-006-97
-140 Control unit of the de-icing system of fins. 3.70-22656899-005-97
-140
-140-01
Control units of the de-icing system of the airframe. 3.70-22656899-004-97
-140-02 Control unit of the de-icing system of the airframe and fins. 35.3-22656899-040-2001
-140
-140-01
Windshield control and thermal management units. 3.70-22656899-005-2000
-140 Windshield control and thermal management unit, control unit of the airflow of the cockpit’s glazing, control of heating pilots leg room. 35.3-22656899-072-2003
-70

Control units of the air bleeding subsystem. 35.3-22656899-050-2002
-70

Exchange modules of integral de-icing control and air treatment system. 35.3-22656899-049-2002
-70 Control unit of the electric-heating de-icing system of the airframe. 35.3-22656899-059-2002
T-70 Control unit of air-heating de-icing system. 35.3-22656899-057-2002
-70 Control unit of the power unit de-icing system. 35.3-22656899-060-2002
-70 Control device for heating the windshield and control of de-icing detectors. 35.3-22656899-052-2002
-140 Digital control device for the complex air-conditioning system. 35.3-22656899-95:2005
K-70

Digital control device for the air-conditioning system of -70 aircraft. 35.3-22656899-091:2005
K-334 Digital control device for the air-conditioning system of -334 aircraft. 35.3-22656899-96:2005
7311 Control device for the air-conditioning system. 35.3-22656899-106:2007
6808.01 Digital control device for the air bleeding subsystem. 35.3-22656899-107:2007
-334 Digital control device for the air bleeding subsystem. 35.3-22656899-102:2006
-77 Multiplex information distribution and conversion system 35.3-22656899-132:2012
Information conversion device 30.3-22656899-141:2012
2500 Turboshaft engine electronic controller Ne=2000 … 2500 hp 468332.080
2500 Turboshaft engine operation time and control counter Ne=2000 2500 hp 468137.001

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