IP21-15
position indicator
Description
IP21-15 position indicator for aircraft systems
IP21-15 is an aircraft position indicator used for visual monitoring of movable mechanical elements. The instrument receives a remote position signal and displays the position or angular displacement on a cockpit scale. It is used in onboard indication systems where the crew needs a direct visual reference for the condition of controlled aircraft mechanisms. Depending on the installed stencil and system configuration, the indicator may be used for rotor pitch indication or for other position-control circuits.
Full descriptionCollapse description
Remote indication through IP21-15
The instrument operates as part of a remote selsyn-type measuring system. In this arrangement, a transmitter installed near the monitored mechanism sends position data electrically to the cockpit indicator. The indicator then converts the received signal into pointer movement on the scale. This allows the crew or maintenance personnel to monitor the position of a mechanism without direct mechanical linkage to the cockpit. The unit is an indicating instrument, not an actuator or control drive.
IP21-15 with DS-type position transmitters
The indicator is used together with specialized selsyn transmitters, including DS-type units such as DS-11 or DS-P depending on the aircraft configuration. The transmitter and indicator must be matched according to the system documentation. A mismatch in transmitter type, scale stencil or wiring can lead to incorrect readings. During troubleshooting, the check should include the indicator, transmitter, aircraft wiring, power supply and mechanical linkage at the monitored unit.
Aircraft application of IP21-15
IP21-15 is used on civil and military aircraft equipment, including Mi-8, Mi-17 and Mi-171E family helicopters. In helicopter applications, it may be associated with the UP21-15 position or rotor pitch indication system. Exact use depends on the aircraft modification and installed cockpit panel layout. Similar instruments may have different scales, lighting arrangements or connection schemes, so applicability should be confirmed through the aircraft parts catalog or technical documentation.
Identification and ordering of IP21-15
Before ordering, the full marking and documentation reference should be checked. IP21-15 is linked with design documentation 6Zh2.511.014-15 and technical specification 6Zh2.511.014TU. It is important to confirm the required scale, lighting voltage, associated transmitter type and cockpit installation position. For correct selection, provide the aircraft type, system designation, existing instrument marking and a photo of the data plate or front scale. The product is also known under alternative designations IP21-15 and ИП21-15.
Technical details
- Product Type
- Aircraft position indicator / measuring indicator
- Function
- Visual indication of position or angular displacement of movable aircraft elements
- Application / Where Used
- Aircraft and helicopter mechanical system indication circuits
- System / Installation Area
- Cockpit instrument panel / remote position indication system
- Compatible Aircraft / Equipment
- Mi-8, Mi-17, Mi-171E and related helicopter configurations
All specificationsCollapse specifications
- Associated System
- UP21-15 position / rotor pitch indication system, depending on installation
- Measuring System Type
- Remote selsyn-type indication system
- Compatible Transmitters
- DS-type selsyn transmitters, including DS-11 or DS-P depending on configuration
- Power Supply for Selsyn Circuit
- 36 V AC, 400 Hz
- Lighting Supply
- 5.5 V DC or 27 V DC, depending on cockpit panel version
- Display Type
- Pointer indication on graduated scale
- Scale Function
- Rotor pitch or position of monitored aircraft mechanism, depending on stencil version
- Operating Temperature Range
- −60 to +60 °C
- Housing
- Round metal housing for recessed panel mounting
- Protection
- Dust- and splash-protected aircraft execution
- Mounting
- Flange mounting with screws
- Technical Specification
- 6Zh2.511.014TU
- Design Documentation Code
- 6Zh2.511.014-15
- Technical Documentation
- Product passport and aircraft system documentation
Payment & delivery
Orders ship from our hub in Dubai. Partner stock is first transferred to Dubai, then shipped to you.
Dubai stock: 100% before dispatch. Partner stock (Remote stock) and Pre-order: 50% advance payment to start the order and 50% before shipment from Dubai to you.
Availability, lead time, delivery cost and payment terms are confirmed for your order before payment.
In-person viewing of parts held in stock at our Dubai warehouse can be arranged on request.
Payment & delivery terms






