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MG-1M

electromechanism

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Availability
Partner stock
Condition
New
Warranty
6 Months
Ref
V00436
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Description

MG-1M aircraft electromechanism

MG-1M is a compact aircraft electromechanism used in onboard equipment systems of Soviet and Russian aviation. The unit is described as a small DC commutator electromechanism intended for remote actuation of pneumatic drives, air valves and related aircraft system components. It is not a cockpit indicator or control panel, but an internal actuator installed in technical compartments, pneumatic lines or equipment bays, depending on the aircraft type and system configuration.

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MG-1M control function in pneumatic systems

The main function of MG-1M is remote control of executive pneumatic elements. The mechanism may be used to open, close or position pneumatic valves, air shut-off valves, dampers and other system elements controlled from the aircraft electrical system. In this role, it converts a DC electrical command into mechanical action applied to a linked pneumatic device. Correct operation of the mechanism is important for reliable switching of air supply, bleed-air routing, ventilation, anti-icing or other aircraft pneumatic circuits.

MG-1M as a compact DC actuator

MG-1M belongs to the class of compact aviation DC electromechanisms. The source context describes it as a commutator-type unit intended for operation from a standard aircraft DC network. The internal brush-collector assembly provides motor commutation and requires attention during inspection, especially for items from long-term storage. Brush wear, collector condition, insulation resistance, connector condition and smooth movement of the driven part should be checked before installation or release to service.

Operating environment of the MG-1M electromechanism

The MG-1M electromechanism is intended for aircraft operating conditions, including vibration, temperature variation and loads typical of technical compartments and onboard system installations. According to the supplied context, the operating temperature range is from -60 °C to +60 °C, with short-term exposure to higher temperatures possible in engine or equipment compartments. Since exact environmental ratings and dimensions are normally defined in the product passport or drawing, installation and acceptance should be based on the specific aircraft documentation and form records.

Aircraft and ground equipment application

MG-1M may be used in pneumatic, air-conditioning, ventilation, engine-start, anti-icing and auxiliary aircraft system circuits. The source context associates compact MG-series mechanisms with Mil and Kamov helicopters, including Mi-8 / Mi-17, Mi-24, Ka-27 / Ka-32, and with transport or passenger aircraft of An, Il and Tu families. The mechanism may also be encountered in aircraft repair plant test benches or control and test equipment where onboard pneumatic system operation is simulated.

Identification and ordering of MG-1M

Before ordering MG-1M, the buyer should confirm the aircraft type, functional system, installation position, required condition and documentation set. Since exact drawing numbers, mounting dimensions, shaft configuration and mass may depend on execution, these details should be checked against the product passport or aircraft maintenance documentation. The unit may be required for repair of pneumatic controls, replacement of an air valve actuator, restoration of onboard system equipment or spare parts stock. Passport availability, storage condition, inspection records and operating test results should be agreed before shipment.

Related equipment: MVD4E15B, MZK-2 Series 2, MPK-13BTV. These links are grouped by function and system context and do not indicate interchangeability.

Technical details

Product Type
Compact aircraft electromechanism / DC actuator
Designation
MG-1M
Russian Designation
МГ-1М
Alternative Designations
МГ1М, MG1M, МГ-1М electromechanism
Function
Remote control of pneumatic drives, air valves, dampers and onboard system executive elements
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Application / Where Used
Aircraft pneumatic systems, air-conditioning systems, ventilation, engine-start air circuits and anti-icing systems
System / Installation Area
Technical compartments, pneumatic lines, air valve assemblies and onboard equipment bays
Compatible Aircraft / Equipment
Mi-8 / Mi-17, Mi-24, Ka-27 / Ka-32, An, Il and Tu aircraft families according to source context and documentation
Ground Equipment Context
Aircraft repair plant test benches and control / test equipment where applicable
Device Type
Small-size aircraft DC commutator electromechanism
Current Type
Direct current
Nominal Supply Voltage
27 V DC
Permitted Aircraft DC Network Reference
24 to 30 V DC, according to source context
Motor Type
DC commutator motor
Duty Mode
Short-time or repeated short-time operation, depending on system use
Commutation Type
Internal brush-collector assembly
Operating Temperature Range
-60 °C to +60 °C, according to source context
Short-Term Temperature Context
Up to +80 °C in engine or technical compartments, according to source context
Estimated Length Reference
Approximately 120–150 mm, according to source context
Estimated Body Diameter / Section Reference
Approximately 40–60 mm, according to source context
Estimated Weight Reference
Approximately 0.5–1.2 kg, depending on execution
Construction Features
Compact DC motor, actuator mechanism, aircraft connector and brush-collector unit
Maintenance Checks
Brush condition, collector condition, insulation resistance, connector condition, smooth movement and operating response
Technical Documentation
Product passport, aircraft maintenance documentation, system documentation, wiring data, inspection records and test documents if available

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