position indicator
Price on request
position indicator
Partner Stock
IP52-03 / IP-52-03 is an aircraft position indicator used as part of onboard cockpit indication equipment. The instrument is intended for visual monitoring of the position of movable aircraft elements, such as landing gear, flaps, airbrakes, intake panels or other actuated systems, depending on aircraft configuration and documentation. The product belongs to aviation technical property and should not be confused with the IP52 enclosure protection rating. In this designation, “IP” refers to the Russian product name “position indicator”.
The main function of IP52-03 is to show the crew the current state of a controlled mechanism on the aircraft instrument panel. The indicator receives discrete signals from limit switches or related position-sensing circuits and displays the corresponding condition through built-in light indication. This allows the crew to verify whether the controlled element is extended, retracted, locked, in transit or in an abnormal position, depending on system logic. The indicator is used where direct visual confirmation of the mechanism is not possible from the cockpit.
In the supplied context, IP52-03 / IP52-03A is associated with Su-family combat aircraft, including Su-27 and Su-30 variants. Indicators of the IP52 series may display the position of landing gear, wing mechanization, airbrakes and automatic intake panels, depending on the aircraft and panel layout. Specific displayed states and legends depend on the version of the instrument and the aircraft wiring. Therefore, the exact function of a particular IP52-03 unit should be confirmed by the aircraft equipment list and cockpit panel documentation.
The indicator operates with discrete position signals from end switches or similar sensor circuits. According to the supplied context, input signals may come from switches such as VK2-200R or AM800K, depending on the controlled system. Green indication typically means that the controlled element is fixed in its required working position, while red indication may show an intermediate, unlocked or fault condition. Absence of illumination may indicate the element is retracted and locked, depending on aircraft circuit logic and the relevant technical manual.
IP52-03 is described as a cockpit-mounted aircraft instrument in a compact metal housing. It is installed on the instrument panel and connected to the aircraft electrical system through a rear plug connector / socket. Mounting may be performed by flange screws or a retaining clamp, depending on the version and panel design. The instrument is intended for operation in cockpit conditions and must withstand aviation vibration and temperature loads typical of combat aircraft. Connector pinout and mounting dimensions should be confirmed by the official drawing.
Before ordering IP52-03 / IP-52-03, the buyer should confirm the exact designation, drawing / TU reference, aircraft type, required modification and documentation requirements. Related versions include IP52-03A, IP52-04, IP52-05 and IP52-16A, but they may differ by indication layout, input logic or application. The product may be required for cockpit indication repair, replacement of a defective position indicator, aircraft restoration or spare parts stock. Passport, acceptance marks, serial number and bench-test records should be checked before shipment.
Product Type: Aircraft position indicator / cockpit indication instrument
Designation: IP52-03 / IP-52-03
Russian Designation: ИП52-03 / ИП-52-03
Alternative Designations: IP52-03A, ИП52-03А, IP52 series position indicator, ИП52 series
Drawing / Technical Specification Reference: 6Zh2.511.031
Russian Reference: 6Ж2.511.031 / ТУ 6Ж2.511.031
Function: Visual indication of the position of movable aircraft elements
Application / Where Used: Cockpit indication equipment of aircraft
System / Installation Area: Instrument panel / position indication circuits
Compatible Aircraft / Equipment: Su-27 and Su-30 family aircraft according to source context; other aircraft depending on documentation
Controlled Elements: Landing gear, flaps / wing mechanization, airbrakes, intake panels or other actuated elements depending on aircraft configuration
Input Signal Type: Discrete signals from limit switches or aircraft position circuits
Example Associated Switches: VK2-200R, AM800K according to source context
Power Supply: 27 V DC aircraft power supply
Current Consumption Reference: Not more than 0.15–0.2 A depending on number of illuminated segments, according to source context
Indication Elements: Built-in green and red signal lamps / light elements
Typical Green Indication: Controlled element fixed in the required working position, according to source context
Typical Red Indication: Intermediate, unlocked or fault condition, according to source context
No-Light Condition: Retracted and locked state depending on aircraft circuit logic, according to source context
Construction: Cockpit instrument in sealed metal housing for panel installation
Mounting: Flange screw mounting or retaining clamp, depending on version
Connector Interface: Rear aviation plug connector / socket
Operating Temperature Range: −60 °C to +60 °C
Vibration Resistance: Designed for vibration conditions of maneuverable combat aircraft equipment
Related Versions: IP52-04, IP52-05, IP52-16A according to source context
Condition: New / As-Stored / Overhauled / Serviceable, depending on availability
Technical Documentation: Product passport, TU 6Zh2.511.031, aircraft wiring diagram, cockpit panel documentation and bench-test records if available
All shipments are carried out from our international warehouse in Dubai (UAE), as well as from our partners’ remote warehouses.
In Stock — items available in stock at the Dubai warehouse are dispatched within 5–10 business days after receiving 100% prepayment.
Remote Stock — items available at our partners’ remote warehouses are supplied within an average of 30–45 business days after receiving 100% prepayment.
Pre-Order — made-to-order products are manufactured and delivered within an average of 45–60 business days. Payment terms: 50% advance payment to start production, with the remaining 50% paid before dispatch from the Dubai warehouse after full readiness for shipment.
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.
IP52-03 / IP-52-03 is an aircraft position indicator used as part of onboard cockpit indication equipment. The instrument is intended for visual monitoring of the position of movable aircraft elements, such as landing gear, flaps, airbrakes, intake panels or other actuated systems, depending on aircraft configuration and documentation. The product belongs to aviation technical property and should not be confused with the IP52 enclosure protection rating. In this designation, “IP” refers to the Russian product name “position indicator”.
The main function of IP52-03 is to show the crew the current state of a controlled mechanism on the aircraft instrument panel. The indicator receives discrete signals from limit switches or related position-sensing circuits and displays the corresponding condition through built-in light indication. This allows the crew to verify whether the controlled element is extended, retracted, locked, in transit or in an abnormal position, depending on system logic. The indicator is used where direct visual confirmation of the mechanism is not possible from the cockpit.
In the supplied context, IP52-03 / IP52-03A is associated with Su-family combat aircraft, including Su-27 and Su-30 variants. Indicators of the IP52 series may display the position of landing gear, wing mechanization, airbrakes and automatic intake panels, depending on the aircraft and panel layout. Specific displayed states and legends depend on the version of the instrument and the aircraft wiring. Therefore, the exact function of a particular IP52-03 unit should be confirmed by the aircraft equipment list and cockpit panel documentation.
The indicator operates with discrete position signals from end switches or similar sensor circuits. According to the supplied context, input signals may come from switches such as VK2-200R or AM800K, depending on the controlled system. Green indication typically means that the controlled element is fixed in its required working position, while red indication may show an intermediate, unlocked or fault condition. Absence of illumination may indicate the element is retracted and locked, depending on aircraft circuit logic and the relevant technical manual.
IP52-03 is described as a cockpit-mounted aircraft instrument in a compact metal housing. It is installed on the instrument panel and connected to the aircraft electrical system through a rear plug connector / socket. Mounting may be performed by flange screws or a retaining clamp, depending on the version and panel design. The instrument is intended for operation in cockpit conditions and must withstand aviation vibration and temperature loads typical of combat aircraft. Connector pinout and mounting dimensions should be confirmed by the official drawing.
Before ordering IP52-03 / IP-52-03, the buyer should confirm the exact designation, drawing / TU reference, aircraft type, required modification and documentation requirements. Related versions include IP52-03A, IP52-04, IP52-05 and IP52-16A, but they may differ by indication layout, input logic or application. The product may be required for cockpit indication repair, replacement of a defective position indicator, aircraft restoration or spare parts stock. Passport, acceptance marks, serial number and bench-test records should be checked before shipment.
Product Type: Aircraft position indicator / cockpit indication instrument
Designation: IP52-03 / IP-52-03
Russian Designation: ИП52-03 / ИП-52-03
Alternative Designations: IP52-03A, ИП52-03А, IP52 series position indicator, ИП52 series
Drawing / Technical Specification Reference: 6Zh2.511.031
Russian Reference: 6Ж2.511.031 / ТУ 6Ж2.511.031
Function: Visual indication of the position of movable aircraft elements
Application / Where Used: Cockpit indication equipment of aircraft
System / Installation Area: Instrument panel / position indication circuits
Compatible Aircraft / Equipment: Su-27 and Su-30 family aircraft according to source context; other aircraft depending on documentation
Controlled Elements: Landing gear, flaps / wing mechanization, airbrakes, intake panels or other actuated elements depending on aircraft configuration
Input Signal Type: Discrete signals from limit switches or aircraft position circuits
Example Associated Switches: VK2-200R, AM800K according to source context
Power Supply: 27 V DC aircraft power supply
Current Consumption Reference: Not more than 0.15–0.2 A depending on number of illuminated segments, according to source context
Indication Elements: Built-in green and red signal lamps / light elements
Typical Green Indication: Controlled element fixed in the required working position, according to source context
Typical Red Indication: Intermediate, unlocked or fault condition, according to source context
No-Light Condition: Retracted and locked state depending on aircraft circuit logic, according to source context
Construction: Cockpit instrument in sealed metal housing for panel installation
Mounting: Flange screw mounting or retaining clamp, depending on version
Connector Interface: Rear aviation plug connector / socket
Operating Temperature Range: −60 °C to +60 °C
Vibration Resistance: Designed for vibration conditions of maneuverable combat aircraft equipment
Related Versions: IP52-04, IP52-05, IP52-16A according to source context
Condition: New / As-Stored / Overhauled / Serviceable, depending on availability
Technical Documentation: Product passport, TU 6Zh2.511.031, aircraft wiring diagram, cockpit panel documentation and bench-test records if available
All shipments are carried out from our international warehouse in Dubai (UAE), as well as from our partners’ remote warehouses.
In Stock — items available in stock at the Dubai warehouse are dispatched within 5–10 business days after receiving 100% prepayment.
Remote Stock — items available at our partners’ remote warehouses are supplied within an average of 30–45 business days after receiving 100% prepayment.
Pre-Order — made-to-order products are manufactured and delivered within an average of 45–60 business days. Payment terms: 50% advance payment to start production, with the remaining 50% paid before dispatch from the Dubai warehouse after full readiness for shipment.
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.