processing module
BE-9E
Price on request
processing module
Partner Stock
Description
BE-9E electronic unit is a core processing element of the IV-500E vibration monitoring equipment used on Mi-8/Mi-17 family helicopters and other aircraft powered by TV3-117 engines.
This version represents the baseline configuration of the block without series marking, predating later production variants such as BE-9E Series 2.
The unit receives vibration signals from MV-03/MV-03-1 sensors installed on the engines via USS-6 matching devices, converts them into electrical control outputs, and activates cockpit annunciator lights when vibration levels exceed caution or hazard thresholds.
BE-9E provides continuous vibration monitoring and automated decision logic that alerts the crew to abnormal engine vibration conditions associated with rotor imbalance, shaft misalignment or bearing degradation.
It is designed for continuous airborne operation with high resistance to vibration, temperature variation and electromagnetic interference.
Alternate designations:
BE-9E, BE9E, БЭ-9Е, БЭ9Е, 6Л2.009.005
All refer to the same electronic unit.
Details
Purpose: Vibration signal processing and warning logic
System Role: Part of IV-500E vibration monitoring equipment
Application: Mi-8, Mi-17, Mi-171 (TV3-117 engines)
Product Type: Electronic processing module
Signal Inputs: MV-03/MV-03-1 sensors via USS-6
Outputs: Yellow caution / red hazard annunciation signals
Caution Trigger Level: ~45 mm/s (system standard)
Hazard Trigger Level: ~60 mm/s (system standard)
Built-In Test Compatibility: Via IV-500E test pushbutton
Power Supply: 115 V AC, 400 Hz (system input)
Installation: Avionics bay or cargo cabin mounts
Condition: As applicable
Documentation: Passport supplied upon request
Payment & delivery
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.
- Description
- Details
- Payment & delivery
BE-9E electronic unit is a core processing element of the IV-500E vibration monitoring equipment used on Mi-8/Mi-17 family helicopters and other aircraft powered by TV3-117 engines.
This version represents the baseline configuration of the block without series marking, predating later production variants such as BE-9E Series 2.
The unit receives vibration signals from MV-03/MV-03-1 sensors installed on the engines via USS-6 matching devices, converts them into electrical control outputs, and activates cockpit annunciator lights when vibration levels exceed caution or hazard thresholds.
BE-9E provides continuous vibration monitoring and automated decision logic that alerts the crew to abnormal engine vibration conditions associated with rotor imbalance, shaft misalignment or bearing degradation.
It is designed for continuous airborne operation with high resistance to vibration, temperature variation and electromagnetic interference.
Alternate designations:
BE-9E, BE9E, БЭ-9Е, БЭ9Е, 6Л2.009.005
All refer to the same electronic unit.
Purpose: Vibration signal processing and warning logic
System Role: Part of IV-500E vibration monitoring equipment
Application: Mi-8, Mi-17, Mi-171 (TV3-117 engines)
Product Type: Electronic processing module
Signal Inputs: MV-03/MV-03-1 sensors via USS-6
Outputs: Yellow caution / red hazard annunciation signals
Caution Trigger Level: ~45 mm/s (system standard)
Hazard Trigger Level: ~60 mm/s (system standard)
Built-In Test Compatibility: Via IV-500E test pushbutton
Power Supply: 115 V AC, 400 Hz (system input)
Installation: Avionics bay or cargo cabin mounts
Condition: As applicable
Documentation: Passport supplied upon request
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.