Fuel Tank Level Sensor
Price on request
Fuel Tank Level Sensor
Available on back-order
SKES-2027A Tank R is an aviation fuel tank level sensor identified by its complete execution marking. This card represents the Tank R sensor position of the SKES-2027A helicopter fuel quantity gauge system. Published system records list Tank R as a separate sensor position; the letter is retained as the authoritative installation label. The designation must be treated as the primary ordering reference because products from the same family can differ in range, electrical interface, calibration, connector, mounting arrangement or system role. External resemblance is not evidence of interchangeability. Selection should be made from the product passport, the aircraft illustrated parts catalogue and the approved maintenance documentation for the exact installation.
The lever-float mechanism follows fuel level and produces the position-specific electrical signal used for quantity indication and system status. The unit is a sensing element within a larger aircraft circuit; it is not a complete indicator, controller or protective system by itself. Its output is interpreted by compatible receiving equipment, so supply characteristics, polarity or phase, connector pinout, load and calibration must match the documented configuration. Tank R geometry and calibration must not be replaced by D or PL data; exact flange, lever, resistance and connector require the drawing. A general explanation of the underlying measurement class is available in this technical reference. That general reference explains the principle only and does not replace product-specific documentation.
The sensor is associated with SKES-2027A installations on Mi-8-family helicopters and must be matched to the documented tank arrangement. Where an aircraft or engine family is named, the statement identifies a documented installation context rather than universal applicability to every modification. The exact equipment set, production series and installed connector must be checked before ordering. Related products in the aviation sensors category are provided for catalogue navigation. The SKES-2027A card is another same-category reference, but the link does not state that the two units are interchangeable or perform the same function.
Before installation, technicians should compare the nameplate, suffix, connector, mounting faces and available acceptance record with the approved requirement. The housing, pressure ports or mechanical input, electrical contacts and sealing features should be inspected without altering calibration. Wiring continuity, insulation and output checks must follow the passport limits for this execution. Do not apply a supply voltage, pressure, acceleration, rotation or test signal taken from a neighbouring model. Storage condition and preservation date should also be reviewed when the unit has remained in stock for an extended period.
After installation, functional testing must be performed as part of the complete aircraft circuit, using approved test equipment and the limits defined by the maintenance manual. A correct bench response alone does not prove that the installation wiring, pneumatic lines, mechanical linkage or receiving unit is serviceable. Any discrepancy should be traced without adjusting sealed elements unless the repair documentation expressly authorises that procedure. The maintenance record should identify the fitted designation and serial number so that later troubleshooting does not confuse adjacent family executions.
An enquiry should state SKES-2027A Tank R, the required condition, quantity, aircraft or equipment context and the documentation needed with delivery. If the installed marking is incomplete, provide a clear photograph of the label, connector and mounting arrangement together with the relevant catalogue reference. Aviamisto can compare these identifiers before supply, but final installation approval remains with the operator or maintenance organisation. Technical Details below separates confirmed data from values that still require passport verification. Same-category cross-sells are navigation aids only; they must never be interpreted as approved replacements.
For a traceable quotation, also state whether a new-production unit, preserved stock item or another documented condition is acceptable. Requested acceptance documents, test records and packing requirements should be agreed before order placement.
Product Type: Tank-specific lever-float fuel level sensor
System: SKES-2027A
Position Marking: Tank R / бак Р
Output: Level-dependent electrical signal for the compatible system
Documented Platform Family: Mi-8 / Mi-17 / Mi-171
Interchangeability: Not established by family name or external appearance
Primary Designation: SKES-2027A Tank R
Original Cyrillic Designation: СКЭС-2027А бак Р
Alternative Designations: SKES-2027A Tank R; SKES 2027A BAK R; СКЭС-2027А бак Р; СКЭС2027А бак Р
Manufacturer: Not confirmed for the offered unit
Aircraft / Equipment Application: According to the exact aircraft, engine or equipment documentation stated above
Installation Position: Confirm from the illustrated parts catalogue and maintenance manual
Connector / Pinout: Confirm from the passport for the exact execution
Documentation: Product passport and applicable installation / maintenance documentation
Ordering Check: Full marking, suffix, connector, required condition and documents
Acceptance Control: Compare marking, interfaces and test record with the approved requirement before installation
Data Rule: Unlisted values must be confirmed from the exact passport and not copied from another execution
Related Products: Same-category links are navigation only and do not state interchangeability
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.
SKES-2027A Tank R is an aviation fuel tank level sensor identified by its complete execution marking. This card represents the Tank R sensor position of the SKES-2027A helicopter fuel quantity gauge system. Published system records list Tank R as a separate sensor position; the letter is retained as the authoritative installation label. The designation must be treated as the primary ordering reference because products from the same family can differ in range, electrical interface, calibration, connector, mounting arrangement or system role. External resemblance is not evidence of interchangeability. Selection should be made from the product passport, the aircraft illustrated parts catalogue and the approved maintenance documentation for the exact installation.
The lever-float mechanism follows fuel level and produces the position-specific electrical signal used for quantity indication and system status. The unit is a sensing element within a larger aircraft circuit; it is not a complete indicator, controller or protective system by itself. Its output is interpreted by compatible receiving equipment, so supply characteristics, polarity or phase, connector pinout, load and calibration must match the documented configuration. Tank R geometry and calibration must not be replaced by D or PL data; exact flange, lever, resistance and connector require the drawing. A general explanation of the underlying measurement class is available in this technical reference. That general reference explains the principle only and does not replace product-specific documentation.
The sensor is associated with SKES-2027A installations on Mi-8-family helicopters and must be matched to the documented tank arrangement. Where an aircraft or engine family is named, the statement identifies a documented installation context rather than universal applicability to every modification. The exact equipment set, production series and installed connector must be checked before ordering. Related products in the aviation sensors category are provided for catalogue navigation. The SKES-2027A card is another same-category reference, but the link does not state that the two units are interchangeable or perform the same function.
Before installation, technicians should compare the nameplate, suffix, connector, mounting faces and available acceptance record with the approved requirement. The housing, pressure ports or mechanical input, electrical contacts and sealing features should be inspected without altering calibration. Wiring continuity, insulation and output checks must follow the passport limits for this execution. Do not apply a supply voltage, pressure, acceleration, rotation or test signal taken from a neighbouring model. Storage condition and preservation date should also be reviewed when the unit has remained in stock for an extended period.
After installation, functional testing must be performed as part of the complete aircraft circuit, using approved test equipment and the limits defined by the maintenance manual. A correct bench response alone does not prove that the installation wiring, pneumatic lines, mechanical linkage or receiving unit is serviceable. Any discrepancy should be traced without adjusting sealed elements unless the repair documentation expressly authorises that procedure. The maintenance record should identify the fitted designation and serial number so that later troubleshooting does not confuse adjacent family executions.
An enquiry should state SKES-2027A Tank R, the required condition, quantity, aircraft or equipment context and the documentation needed with delivery. If the installed marking is incomplete, provide a clear photograph of the label, connector and mounting arrangement together with the relevant catalogue reference. Aviamisto can compare these identifiers before supply, but final installation approval remains with the operator or maintenance organisation. Technical Details below separates confirmed data from values that still require passport verification. Same-category cross-sells are navigation aids only; they must never be interpreted as approved replacements.
For a traceable quotation, also state whether a new-production unit, preserved stock item or another documented condition is acceptable. Requested acceptance documents, test records and packing requirements should be agreed before order placement.
Product Type: Tank-specific lever-float fuel level sensor
System: SKES-2027A
Position Marking: Tank R / бак Р
Output: Level-dependent electrical signal for the compatible system
Documented Platform Family: Mi-8 / Mi-17 / Mi-171
Interchangeability: Not established by family name or external appearance
Primary Designation: SKES-2027A Tank R
Original Cyrillic Designation: СКЭС-2027А бак Р
Alternative Designations: SKES-2027A Tank R; SKES 2027A BAK R; СКЭС-2027А бак Р; СКЭС2027А бак Р
Manufacturer: Not confirmed for the offered unit
Aircraft / Equipment Application: According to the exact aircraft, engine or equipment documentation stated above
Installation Position: Confirm from the illustrated parts catalogue and maintenance manual
Connector / Pinout: Confirm from the passport for the exact execution
Documentation: Product passport and applicable installation / maintenance documentation
Ordering Check: Full marking, suffix, connector, required condition and documents
Acceptance Control: Compare marking, interfaces and test record with the approved requirement before installation
Data Rule: Unlisted values must be confirmed from the exact passport and not copied from another execution
Related Products: Same-category links are navigation only and do not state interchangeability
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.