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IN-4

Zero indicator

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Availability
In stock
Warranty
6 Months
Condition
New
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Description

IN-4 zero indicator in the AP-34B system

The IN-4 is an aircraft zero indicator used in automatic flight control systems of Mi-8 and Mi-17 family helicopters. In the AP-34B autopilot suite, it gives a visual indication of signal deviation in the control channels. The instrument shows how far the monitored signal has moved from its neutral reference position, allowing the crew or maintenance personnel to see whether the relevant channel is balanced or displaced. It does not generate control commands and does not correct the aircraft attitude by itself; it is an indicating instrument within the autopilot control chain.

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Visual monitoring through the IN-4 indicator

The IN-4 responds to changes in input current and moves its pointer according to the signal applied to the instrument. This makes it useful for monitoring deviations in autopilot circuits during operation or checks. In practical terms, the indicator helps show whether a channel is close to its neutral condition or whether there is a visible offset. This is important in systems where sensors, amplifiers and executive circuits must work together. A pointer deviation may guide the crew or technicians toward a channel that needs attention.

IN-4 in autopilot stabilization channels

Within the AP-34B system, the IN-4 is connected with stabilization and control circuits. It may be used to observe signal behavior linked to autopilot channels, sensors, amplifier blocks and downstream executive elements. Since the AP-34B system works through several control loops, visual indication can be useful during adjustment, fault isolation and system monitoring. The IN-4 does not replace electrical measurement equipment, but it gives a quick cockpit-level reference of whether the monitored signal is centered or shifted.

Cockpit installation of the IN-4 instrument

The IN-4 is installed on the cockpit instrument panel as part of the helicopter’s flight-control equipment. Because it is a crew-visible instrument, readability and pointer movement are important. The glass, scale, pointer, case, mounting and electrical connections should remain in good condition. A weak movement, sticking pointer, unstable indication or damaged face can create misleading information even if the connected autopilot channel is functioning correctly. For this reason, inspection of the IN-4 includes both external condition and electrical response.

Electrical operation of the IN-4 zero indicator

The indicator operates from the aircraft DC supply and reacts to small control currents. The pointer movement depends on the applied current, with defined values for start-up and full deflection. These parameters are important during bench checks and troubleshooting. Since the instrument works with low-level signals, connector condition and wiring quality matter. Poor contact, contamination, mechanical wear or incorrect power supply can affect pointer behavior and make the instrument appear faulty or cause it to display an incorrect channel condition.

Use of IN-4 on Mi-8 / Mi-17 helicopters

The IN-4 is used on Mi-8, Mi-8T, Mi-8MT, Mi-8AMT, Mi-17 and related helicopters equipped with AP-34B automatic flight control systems. Its role is tied to the autopilot and stabilization equipment rather than to general cockpit indication. Before replacement, the exact installation should be checked against the helicopter parts catalog and AP-34B documentation. Similar small cockpit instruments may look alike, but the IN-4 must be selected by designation, electrical characteristics, mounting format and system connection.

Identification and supply of the IN-4 indicator

In documents and spare-parts requests, the instrument may appear as IN-4, IN4 or IN-4. These notations usually refer to the same zero indicator, but the marking on the unit and manufacturer passport should still be checked before supply. The IN-4 is aviation technical equipment and may be supplied new, from storage, repaired, overhauled or serviceable depending on availability. For aircraft installation, passport documentation, manufacturer certification, service records and technical condition are normally checked before acceptance.

Technical details

Product Type
Zero indicator
Designation
IN-4
Alternative Designation
IN-4
Alternative Designations
IN4, IN-4, IN-4
Function
Visual indication of control signal deviations in the autopilot system
All specificationsCollapse specifications
Application / Where Used
AP-34B automatic flight control and stabilization channels
System / Installation Area
Cockpit instrument panel; autopilot indication circuits
Compatible Aircraft / Equipment
Mi-8, Mi-8T, Mi-8MT, Mi-8AMT, Mi-17 and related variants depending on AP-34B installation
System Role
Monitoring of signal deviation from neutral reference position in autopilot channels
Associated Equipment
AP-34B autopilot, sensors, amplification blocks and executive control circuits
Operating Principle
Pointer indication based on input current variation
Full Deflection Current
300 ±50 μA
Pointer Movement Current, Downwards
10 μA
Pointer Start-Up Current
Not more than 0.02 mA
Power Supply
27 V DC
Mounting
Cockpit instrument panel
Weight
Not more than 0.45 kg
Precious Metals Content
Gold approx. 0.223 g; silver approx. 0.386 g
Category
Aviation technical equipment / autopilot indication instrument
Technical Documentation
Manufacturer passport / certification documentation

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IN-4