IP52-05 / IP-52-05

IP52-05 / IP-52-05 aircraft position indicator

IP52-05 / IP-52-05 is an aircraft position indicator used for cockpit visual monitoring of movable aircraft elements. The instrument belongs to aviation technical property and is installed on aircraft instrument panels as part of onboard indication equipment. In the supplied context, the indicator is associated with Su-family military aircraft, including Su-27, Su-30 and Su-34 variants, depending on configuration and documentation. The instrument helps the crew monitor the position or state of landing gear, wing mechanization, airbrakes or other actuated systems.

Function of the IP52-05 indicator

The main function of IP52-05 is to display the current condition of controlled aircraft mechanisms. The indicator can show whether an element is extended, retracted, locked or in an intermediate position, depending on the connected system logic. The unit works with position sensors, limit switches or other aircraft control circuits and converts their signals into visual information on the cockpit panel. This type of indication is important for systems where the pilot must quickly confirm the status of several actuated aircraft elements during flight, takeoff or landing.

Controlled aircraft elements

According to the supplied context, IP52-05 may be used for monitoring wing mechanization, landing gear, airbrake position or other movable structural elements. The instrument can be associated with flaps, slats, landing gear locks, brake shields or similar aircraft mechanisms depending on aircraft type and panel design. Exact displayed objects, markings and indication logic depend on the version of the indicator and the aircraft wiring. Therefore, the application of a specific IP52-05 unit should be confirmed through the aircraft equipment list and cockpit panel documentation.

Indication and cockpit display

The supplied context describes IP52-05 as a pointer-mnemonic type indicator with built-in illumination. It may display deflection angles or position states through scales, sectors, arrows, mnemonic elements or signal lamps. The lighting may be red-orange or white depending on the series and cockpit lighting system. The indication may include values in degrees or percentage for left and right wing mechanization elements, as well as signal sectors for landing gear or other controlled systems. Final display layout must be checked by the exact modification.

Electrical interface and signal sources

IP52-05 operates from the standard 27 V DC aircraft power supply. According to the supplied context, the indicator may receive analog signals from potentiometric sensors such as MU-615, inductive position sensors or related control circuits. Some associated systems may also use limit switches or position sensors to form indication signals. Because IP52 series instruments may differ by version, input type and scale, the electrical interface should be verified by the applicable aircraft wiring diagram, connector pinout and technical specifications.

Identification and ordering of IP52-05

Before ordering IP52-05 / IP-52-05, the buyer should confirm the exact designation, aircraft type, controlled system, required scale / panel layout and documentation requirements. Related versions include IP52-04, IP52-15 and other IP52 series indicators, but they may differ by signal type, indication layout, dimensions or aircraft application. The item may be required for cockpit indication repair, replacement of a defective instrument, aircraft restoration or spare parts stock. Product passport, serial number, condition category and bench-test records should be agreed before shipment.

Product Type: Aircraft position indicator / cockpit indication instrument
Designation: IP52-05 / IP-52-05
Russian Designation: ИП52-05 / ИП-52-05
Alternative Designations: IP52-05 position indicator, ИП52 series indicator, IP-52 series
Alternative Product Names: Position indicator, cockpit position indicator, pointer-mnemonic indicator, aircraft indication instrument
Function: Visual indication of the position or state of movable aircraft elements
Application / Where Used: Aircraft cockpit indication equipment
System / Installation Area: Instrument panel / position indication circuits
Compatible Aircraft / Equipment: Su-27, Su-30 and Su-34 family aircraft according to source context; other aircraft depending on documentation
Controlled Elements: Wing mechanization, landing gear, airbrakes, brake shields or other movable aircraft elements depending on configuration
Input Signal Type: Analog signals from potentiometric or inductive position sensors according to source context
Example Associated Sensor: MU-615 potentiometric sensor according to source context
Additional Signal Sources: Limit switches and position sensors depending on aircraft system configuration
Power Supply: 27 V DC aircraft power supply
DC Supply Range: 24 to 29.4 V according to source context
Current Consumption Reference: Not more than 0.15 A, depending on illumination mode and number of active lamps
Indicator Type: Pointer-mnemonic indicator according to source context
Display Elements: Scales, sectors, arrows, mnemonic elements or built-in signal lamps depending on version
Displayed Values: Deflection angles in degrees or percentage; landing gear extended / retracted sectors depending on version
Built-In Lighting: Red-orange or white illumination depending on series and cockpit lighting system
Panel Cutout Reference: Standard round aircraft instrument body for 60 mm panel cutout, according to source context
Weight Reference: Approximately 0.4–0.5 kg
Operating Temperature Range: −60 °C to +60 °C
Overload Resistance: Standard linear and vibration loads for frontline combat aircraft, according to source context
Vibration Resistance: Designed for aircraft cockpit vibration conditions
Related Versions: IP52-04, IP52-15 and other IP52 series indicators according to source context
Condition: New / As-Stored / Overhauled / Serviceable, depending on availability
Technical Documentation: Product passport, aircraft wiring diagram, cockpit panel documentation, connector pinout and bench-test records if available

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Returns & Changes (Restocking Fee)
For selected items, a RESTOCKING FEE of 10% may apply in case of return, order cancellation, or changes to the order specifications. This condition applies only to certain products and is confirmed at the order approval stage.

Warranty
All products are covered by a standard 6-month warranty.
Extended warranty is available upon request and is agreed individually; it may affect the final product price.