UK-68V
vibration indicator
Description
UK-68V operating purpose
UK-68V is a engine vibration indicator. Displays the vibration level measured at engine supports by the connected vibration-monitoring system. It operates inside an aircraft measuring or navigation channel and must be evaluated together with the sensors, computers, power supply and wiring of the exact installation.
Vibration sensors and matching units condition the signal for the IV-500A system, which drives the UK-68V pointer. Serviceability of the pointer alone therefore does not validate the complete system. A functional check must also cover input signals, interconnecting lines, associated units and the specified test procedure.
Full descriptionCollapse description
UK-68V in the associated system
Associated system: IV-500A engine vibration monitoring system. Nearest connected equipment: MV-03-2 vibration sensors, USS-6 matching units, BE-9A electronic unit and aircraft warning circuits. These items form a functional chain but are not automatically included in the delivery set of one indicator.
Documented with TV2-117 engine installations and the Mi-8 family; other engines require system confirmation. Applicability to another aircraft modification must not be inferred from appearance and requires confirmation in the parts catalogue, wiring diagram or maintenance manual.
Indication, power and cockpit installation
Indication range or presentation: 0–100% scale corresponding to the calibrated vibration-velocity range of the complete system. Power and input channel: From the IV-500A system circuits; the indicator input is documented as a low-current measuring channel.
Installation: Engine-instrument panel in the cockpit. Before fitting, verify the complete designation, series, scale, connector or pressure ports, mounting, housing, glass and nameplate condition. The installed unit is then checked under the procedure for the applicable system and aircraft.
Identification of UK-68V
The original Soviet/Russian factory designation is Cyrillic: УК-68В. The English card uses the consistent Latin transliteration UK-68V. Similar-looking Cyrillic and Latin characters are not mixed inside the primary designation.
A normal test command should move the pointer into the documented control sector; it does not by itself validate every remote sensor. A visually similar instrument, adjacent series or comparable scale does not prove interchangeability. Selection requires a nameplate photograph, exact index, aircraft type, associated system and documentation requirement.
Ordering and related indicators
An inquiry for UK-68V should state required condition, delivery set, passport and bench-test needs. Card defaults are Condition: New, Warranty: 6 Months and Stock Status: Pre-Order; actual lead time and documentation are confirmed in the quotation.
More instruments are available in the Aviamisto Altimeters and Indicators category. Related positions: UI1-100K, URVK-18K, UT-7M, UMS-2.5-2I. They belong to nearby functional channels or the same equipment group and are not confirmed replacements without direct technical documentation.
Technical details
- Product Type
- Engine vibration indicator
- Designation
- UK-68V
- Original Cyrillic Designation
- УК-68В
- Alternative Designations
- UK-68V; UK 68V; УК-68В
- Function
- Displays the vibration level measured at engine supports by the connected vibration-monitoring system.
All specificationsCollapse specifications
- Operating Principle
- Vibration sensors and matching units condition the signal for the IV-500A system, which drives the UK-68V pointer.
- Associated System
- IV-500A engine vibration monitoring system.
- Connected Equipment
- MV-03-2 vibration sensors, USS-6 matching units, BE-9A electronic unit and aircraft warning circuits.
- Range / Indication
- 0–100% scale corresponding to the calibrated vibration-velocity range of the complete system.
- Power Supply / Input
- From the IV-500A system circuits; the indicator input is documented as a low-current measuring channel.
- Application
- Documented with TV2-117 engine installations and the Mi-8 family; other engines require system confirmation.
- Installation Area
- Engine-instrument panel in the cockpit.
- Compatibility Note
- A normal test command should move the pointer into the documented control sector; it does not by itself validate every remote sensor.
- Technical Documentation
- Product passport, associated-system documentation, aircraft manual and test records when available
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.
Payment & delivery terms