Fuel Level Switch
Price on request
Fuel Level Switch
Available on back-order
DSMK14-2 is an aviation aircraft fuel level switch identified by its complete execution marking. Aircraft minimum-equipment and fuel-system documentation identifies ДСМК14-2 as a level signaliser in an aircraft fuel-quantity system. Existing exact-product data records 27 ±2.7 V DC supply, 0.1 MPa permitted overpressure and mass not more than 0.110 kg. 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 sensor provides a discrete level signal used by compatible fuel indication or pump-control equipment when fuel reaches the defined position. 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. Installation height, tank position, contact logic and exact liquid compatibility are controlled by the aircraft fuel-system documentation. 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.
Published aircraft documentation places DSMK14-2 in fuel-quantity and tank-pump monitoring; the precise aircraft modification and tank must be checked by illustrated parts catalogue. 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 DSMK-10-36 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 DSMK14-2, 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: Aircraft fuel level switch / signaliser
Original Designation: ДСМК14-2
Supply: 27 ±2.7 V DC according to existing exact-product data
Permitted Overpressure: 0.1 MPa
Recorded Media Temperature: Water / solutions +3 to +85 °C; hydrocarbon media −60 to +125 °C
Recorded Vibration: 5–2000 Hz, up to 10 g
Mass: Not more than 0.110 kg
Tank / Switching Height: Confirm from aircraft fuel-system documentation
Primary Designation: DSMK14-2
Original Cyrillic Designation: ДСМК14-2
Alternative Designations: DSMK14-2; DSMK-14-2; DSMK 14-2; ДСМК14-2; ДСМК-14-2; ДСМК 14-2
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
Interchangeability: Not established by family name or external appearance
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.
DSMK14-2 is an aviation aircraft fuel level switch identified by its complete execution marking. Aircraft minimum-equipment and fuel-system documentation identifies ДСМК14-2 as a level signaliser in an aircraft fuel-quantity system. Existing exact-product data records 27 ±2.7 V DC supply, 0.1 MPa permitted overpressure and mass not more than 0.110 kg. 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 sensor provides a discrete level signal used by compatible fuel indication or pump-control equipment when fuel reaches the defined position. 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. Installation height, tank position, contact logic and exact liquid compatibility are controlled by the aircraft fuel-system documentation. 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.
Published aircraft documentation places DSMK14-2 in fuel-quantity and tank-pump monitoring; the precise aircraft modification and tank must be checked by illustrated parts catalogue. 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 DSMK-10-36 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 DSMK14-2, 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: Aircraft fuel level switch / signaliser
Original Designation: ДСМК14-2
Supply: 27 ±2.7 V DC according to existing exact-product data
Permitted Overpressure: 0.1 MPa
Recorded Media Temperature: Water / solutions +3 to +85 °C; hydrocarbon media −60 to +125 °C
Recorded Vibration: 5–2000 Hz, up to 10 g
Mass: Not more than 0.110 kg
Tank / Switching Height: Confirm from aircraft fuel-system documentation
Primary Designation: DSMK14-2
Original Cyrillic Designation: ДСМК14-2
Alternative Designations: DSMK14-2; DSMK-14-2; DSMK 14-2; ДСМК14-2; ДСМК-14-2; ДСМК 14-2
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
Interchangeability: Not established by family name or external appearance
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.