Fuel Pump
Price on request
Fuel Pump
Out of stock
The DTSN-82 is an engine-driven centrifugal fuel pump used in aircraft engine fuel and fuel-regulation systems. Its main function is to supply aviation kerosene under pressure and maintain the required flow conditions before the main high-pressure fuel control equipment. In the engine fuel chain, the DTSN-82 works as a first-stage booster pump. It receives fuel from the aircraft tank system, increases pressure at the engine level and sends the fuel further toward filtration and fuel regulation units.
The DTSN-82 provides preliminary fuel pressure before the fuel reaches the main pump-regulator. This first pressure stage is important because the downstream regulator must receive fuel without starvation, cavitation or unstable inlet conditions. The pump creates continuous fuel flow using the centrifugal force of its rotating impeller. In normal operation, the DTSN-82 helps keep the fuel supply stable across engine operating modes, especially where fuel demand changes quickly or the engine operates at high power settings.
The DTSN-82 is installed on the engine accessory gearbox / engine unit gearbox of the main aircraft engine. It is not an electrically driven pump and does not have its own motor. The rotor is driven mechanically from the engine shaft through a gear train and drive connection. Because of this, inspection of the pump must include the drive interface, shaft condition, mounting flange, sealing surfaces and gearbox connection. Any problem in the drive or mounting area can affect pump output and fuel-system reliability.
The DTSN-82 operates as a centrifugal rotary pump. Fuel enters the pump, is captured by the impeller blades and is accelerated inside the pump casing. The rotating impeller converts mechanical energy from the engine drive into fuel flow and pressure. This design allows the pump to handle high flow rates while remaining compact enough for engine-mounted installation. Clean fuel, correct inlet pressure and proper drive speed are essential for correct operation. Contamination, inlet restriction or wear can reduce pressure and affect the connected fuel-control system.
In the engine fuel system, the DTSN-82 supplies fuel through the fine fuel filter toward the NR-31V high-pressure pump-regulator. The NR-31V then meters fuel and distributes it to the main and afterburner combustion circuits, depending on engine configuration. This makes the DTSN-82 an important upstream unit in the fuel-control chain. A fault in the DTSN-82 can appear later as unstable regulator operation, pressure drop, reduced fuel delivery or abnormal behavior of the main and afterburner fuel circuits.
The DTSN-82 is designed for high fuel delivery. According to the supplied data, the pump flow rate is 81,000 L/h, with shaft speed around 8,000 rpm. The inlet pressure range is 0.45–3.5 kgf/cm², and the excess pressure range is 6.8–8.3 kgf/cm². These values indicate that the pump is intended for a powerful engine fuel system where large fuel flow and stable pressure are required. For installation or acceptance, these parameters should be checked against the engine documentation and test procedure.
DTSN-series pumps may exist in single-circuit, dual-circuit or integral configurations depending on the engine fuel system. The DTSN-82 should therefore be selected not only by designation, but also by engine application and installation configuration. Similar centrifugal engine pumps may differ by flow rate, pressure, mounting, drive interface or regulator compatibility. Before replacement, the pump must be checked against the engine parts catalog, fuel-system diagram and approved interchangeability data.
For supply, the pump should be requested by its full designation: DTSN-82 / ДЦН-82. Since it is part of the aircraft engine fuel system, documentation and testing are important. Units supplied from storage or after repair should be checked by passport, acceptance records and available bench-test data. Before installation, maintenance personnel should inspect the housing, drive connection, flange, sealing areas, hydraulic ports, cleanliness of the flow path, leakage and pressure performance.
Product Type: Engine-driven centrifugal fuel pump
Designation: DTSN-82
Alternative Designations: ДЦН-82; DTSN-82
Function: First-stage fuel boosting and supply to engine fuel-regulating equipment
Application / Where Used: Aircraft engine fuel and fuel-regulation systems
System / Installation Area: Engine accessory gearbox / engine unit gearbox
Part of System / Included in Set: First-stage fuel supply before fine filter and main pump-regulator
Associated Fuel-Control Equipment: NR-31V high-pressure pump-regulator, according to supplied data
Fuel Flow Path: Aircraft tanks → DTSN-82 → fine fuel filter → NR-31V pump-regulator → main and afterburner fuel circuits
Pump Type: Engine-driven centrifugal rotary fuel pump
Drive Type: Mechanical drive from engine accessory gearbox through gear transmission
Own Electric Motor: Not installed
Working Medium: Aviation fuel / kerosene
Flow Rate: 81,000 L/h
Shaft Rotational Speed: 8,000 rpm
Inlet Pressure: 0.45–3.5 kgf/cm²
Excess / Boost Pressure: 6.8–8.3 kgf/cm²
General Outlet Pressure Reference for DTSN-Series Pumps: 0.3–0.47 kgf/cm² according to supplied general series data
General Excess Pressure Reference for DTSN-Series Pumps: 1.8–20.5 kgf/cm² depending on mode and configuration
Construction Type: Centrifugal pump; possible single-circuit, dual-circuit or integral configuration depending on engine system
Installation Feature: Mounted on the engine accessory gearbox / KDA of the main engine
Overall Dimensions: 132 × 184 mm, according to supplied data
Weight: 3.2 kg
Inspection / Testing: Flow rate check, inlet pressure check, boost pressure check, drive interface inspection, leakage check, housing, flange and sealing inspection
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.
The DTSN-82 is an engine-driven centrifugal fuel pump used in aircraft engine fuel and fuel-regulation systems. Its main function is to supply aviation kerosene under pressure and maintain the required flow conditions before the main high-pressure fuel control equipment. In the engine fuel chain, the DTSN-82 works as a first-stage booster pump. It receives fuel from the aircraft tank system, increases pressure at the engine level and sends the fuel further toward filtration and fuel regulation units.
The DTSN-82 provides preliminary fuel pressure before the fuel reaches the main pump-regulator. This first pressure stage is important because the downstream regulator must receive fuel without starvation, cavitation or unstable inlet conditions. The pump creates continuous fuel flow using the centrifugal force of its rotating impeller. In normal operation, the DTSN-82 helps keep the fuel supply stable across engine operating modes, especially where fuel demand changes quickly or the engine operates at high power settings.
The DTSN-82 is installed on the engine accessory gearbox / engine unit gearbox of the main aircraft engine. It is not an electrically driven pump and does not have its own motor. The rotor is driven mechanically from the engine shaft through a gear train and drive connection. Because of this, inspection of the pump must include the drive interface, shaft condition, mounting flange, sealing surfaces and gearbox connection. Any problem in the drive or mounting area can affect pump output and fuel-system reliability.
The DTSN-82 operates as a centrifugal rotary pump. Fuel enters the pump, is captured by the impeller blades and is accelerated inside the pump casing. The rotating impeller converts mechanical energy from the engine drive into fuel flow and pressure. This design allows the pump to handle high flow rates while remaining compact enough for engine-mounted installation. Clean fuel, correct inlet pressure and proper drive speed are essential for correct operation. Contamination, inlet restriction or wear can reduce pressure and affect the connected fuel-control system.
In the engine fuel system, the DTSN-82 supplies fuel through the fine fuel filter toward the NR-31V high-pressure pump-regulator. The NR-31V then meters fuel and distributes it to the main and afterburner combustion circuits, depending on engine configuration. This makes the DTSN-82 an important upstream unit in the fuel-control chain. A fault in the DTSN-82 can appear later as unstable regulator operation, pressure drop, reduced fuel delivery or abnormal behavior of the main and afterburner fuel circuits.
The DTSN-82 is designed for high fuel delivery. According to the supplied data, the pump flow rate is 81,000 L/h, with shaft speed around 8,000 rpm. The inlet pressure range is 0.45–3.5 kgf/cm², and the excess pressure range is 6.8–8.3 kgf/cm². These values indicate that the pump is intended for a powerful engine fuel system where large fuel flow and stable pressure are required. For installation or acceptance, these parameters should be checked against the engine documentation and test procedure.
DTSN-series pumps may exist in single-circuit, dual-circuit or integral configurations depending on the engine fuel system. The DTSN-82 should therefore be selected not only by designation, but also by engine application and installation configuration. Similar centrifugal engine pumps may differ by flow rate, pressure, mounting, drive interface or regulator compatibility. Before replacement, the pump must be checked against the engine parts catalog, fuel-system diagram and approved interchangeability data.
For supply, the pump should be requested by its full designation: DTSN-82 / ДЦН-82. Since it is part of the aircraft engine fuel system, documentation and testing are important. Units supplied from storage or after repair should be checked by passport, acceptance records and available bench-test data. Before installation, maintenance personnel should inspect the housing, drive connection, flange, sealing areas, hydraulic ports, cleanliness of the flow path, leakage and pressure performance.
Product Type: Engine-driven centrifugal fuel pump
Designation: DTSN-82
Alternative Designations: ДЦН-82; DTSN-82
Function: First-stage fuel boosting and supply to engine fuel-regulating equipment
Application / Where Used: Aircraft engine fuel and fuel-regulation systems
System / Installation Area: Engine accessory gearbox / engine unit gearbox
Part of System / Included in Set: First-stage fuel supply before fine filter and main pump-regulator
Associated Fuel-Control Equipment: NR-31V high-pressure pump-regulator, according to supplied data
Fuel Flow Path: Aircraft tanks → DTSN-82 → fine fuel filter → NR-31V pump-regulator → main and afterburner fuel circuits
Pump Type: Engine-driven centrifugal rotary fuel pump
Drive Type: Mechanical drive from engine accessory gearbox through gear transmission
Own Electric Motor: Not installed
Working Medium: Aviation fuel / kerosene
Flow Rate: 81,000 L/h
Shaft Rotational Speed: 8,000 rpm
Inlet Pressure: 0.45–3.5 kgf/cm²
Excess / Boost Pressure: 6.8–8.3 kgf/cm²
General Outlet Pressure Reference for DTSN-Series Pumps: 0.3–0.47 kgf/cm² according to supplied general series data
General Excess Pressure Reference for DTSN-Series Pumps: 1.8–20.5 kgf/cm² depending on mode and configuration
Construction Type: Centrifugal pump; possible single-circuit, dual-circuit or integral configuration depending on engine system
Installation Feature: Mounted on the engine accessory gearbox / KDA of the main engine
Overall Dimensions: 132 × 184 mm, according to supplied data
Weight: 3.2 kg
Inspection / Testing: Flow rate check, inlet pressure check, boost pressure check, drive interface inspection, leakage check, housing, flange and sealing inspection
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.