plunger pump
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plunger pump
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The PN-99 is an aircraft plunger-type pump used as part of gas turbine engine systems. It is intended for precision delivery of working fluid in engine-mounted fuel or hydraulic circuits where stable supply under pressure is required. The pump belongs to aviation precision equipment and is designed for operation in demanding engine environments, including military and special-purpose aircraft applications.
The main function of the PN-99 is to supply working fluid to engine subsystems with controlled and stable delivery. Depending on the exact engine configuration, the pump may be installed in a fuel-related or hydraulic control circuit. Its task is not simple transfer, but accurate supply of fluid for correct operation of the engine system. In this type of application, delivery stability is important for engine control, regulation and reliable operation under changing load conditions.
The PN-99 is a positive-displacement plunger / piston pump. This construction uses reciprocating plunger movement to move the working fluid and create pressure. Plunger pumps are used in aviation where a compact unit must provide accurate delivery under high load. Since the pump has precision working elements, cleanliness of the working fluid, correct filtration, proper inlet conditions and compatibility with the assigned medium are critical. Contamination or incorrect fluid can quickly affect the pump’s performance and service life.
The PN-99 is installed as part of an aircraft engine-mounted system. Depending on engine design, it may be connected to the fuel supply, hydraulic control or other engine service circuit. The pump is associated with gas turbine engines used on fighter and combat aircraft. Before replacement, the mounting position, drive connection, hydraulic or fuel ports, seals and exact engine modification must be checked against the engine documentation. The designation PN-99 alone is not enough to confirm interchangeability across different engine installations.
The PN-99 is associated with RD-33, RD-93 and AL-31F gas turbine engines according to supplied reference data. These engines are used on military aviation platforms, including fighter and combat aircraft. The exact pump role may differ depending on the engine version and system layout. It may work together with fuel-regulating equipment, hydraulic control units and other engine-mounted components. For procurement, the engine type and modification should be specified together with the pump designation.
The working medium for the PN-99 must be confirmed by the engine documentation. In descriptions of this pump, the medium may be referenced as fuel or oil depending on the system where the unit is installed. This should not be assumed during selection. A fuel-system version and a hydraulic / oil-system installation can have different requirements for seals, materials, testing and storage condition. Before installation, the pump should be checked against the required working fluid, operating pressure and engine technical documentation.
The PN-99 is historically associated with JSC “MPO named after I. Rumyantsev” in Moscow, a manufacturer known for aviation fuel and control equipment. The pump is aviation technical property and should be handled as a controlled precision unit. For aircraft engine use, documentation is important: passport, storage records, repair documents, bench-test data and traceability should be reviewed whenever available. Without documentation, the unit should be considered technically unconfirmed until inspected and tested.
For supply or replacement, the pump should be requested by its full designation: PN-99 / ПН-99. Before installation, the unit should be inspected for housing condition, drive interface, ports, sealing areas, corrosion, contamination, preservation state and signs of previous repair. Since available reference data does not specify operating pressure, performance, service life or assigned resource, these parameters should be checked through manufacturer documentation or engine manuals. Bench testing is recommended before installation in an aircraft engine system.
Product Type: Aircraft plunger pump
Designation: PN-99
Alternative Designations: ПН-99, PN-99
Function: Supply of working fluid within aircraft gas turbine engine systems
Application / Where Used: Gas turbine engine systems of military and special-purpose aviation equipment
System / Installation Area: Engine-mounted fuel or hydraulic system depending on configuration
Operating Role: Precision supply pump for engine subsystems
Pump Type: Positive-displacement plunger / piston pump
Compatible Engines: RD-33, RD-93, AL-31F gas turbine engines according to supplied reference data
Compatible Aircraft / Equipment: Fighter and combat aircraft equipped with compatible engine installations, depending on configuration
Associated Equipment: Fuel-regulating equipment, hydraulic control units and engine-mounted control components depending on engine layout
Working Medium: Not specified; fuel or oil depending on engine system documentation
Operating Pressure: Not specified
Performance: Not specified
Assigned Resource: Not specified
Assigned Service Life: Not specified
Storage Life: Not specified
Manufacturer Reference: JSC “MPO named after I. Rumyantsev” according to supplied reference data
Scope of Supply: Not specified; to be confirmed by purchase order and supplier documents
Inspection / Testing: Housing inspection, port cleanliness check, drive interface inspection, seal inspection, leakage check and bench testing according to engine documentation
Technical Documentation: Manufacturer technical documentation, product passport and engine documentation as applicable
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 PN-99 is an aircraft plunger-type pump used as part of gas turbine engine systems. It is intended for precision delivery of working fluid in engine-mounted fuel or hydraulic circuits where stable supply under pressure is required. The pump belongs to aviation precision equipment and is designed for operation in demanding engine environments, including military and special-purpose aircraft applications.
The main function of the PN-99 is to supply working fluid to engine subsystems with controlled and stable delivery. Depending on the exact engine configuration, the pump may be installed in a fuel-related or hydraulic control circuit. Its task is not simple transfer, but accurate supply of fluid for correct operation of the engine system. In this type of application, delivery stability is important for engine control, regulation and reliable operation under changing load conditions.
The PN-99 is a positive-displacement plunger / piston pump. This construction uses reciprocating plunger movement to move the working fluid and create pressure. Plunger pumps are used in aviation where a compact unit must provide accurate delivery under high load. Since the pump has precision working elements, cleanliness of the working fluid, correct filtration, proper inlet conditions and compatibility with the assigned medium are critical. Contamination or incorrect fluid can quickly affect the pump’s performance and service life.
The PN-99 is installed as part of an aircraft engine-mounted system. Depending on engine design, it may be connected to the fuel supply, hydraulic control or other engine service circuit. The pump is associated with gas turbine engines used on fighter and combat aircraft. Before replacement, the mounting position, drive connection, hydraulic or fuel ports, seals and exact engine modification must be checked against the engine documentation. The designation PN-99 alone is not enough to confirm interchangeability across different engine installations.
The PN-99 is associated with RD-33, RD-93 and AL-31F gas turbine engines according to supplied reference data. These engines are used on military aviation platforms, including fighter and combat aircraft. The exact pump role may differ depending on the engine version and system layout. It may work together with fuel-regulating equipment, hydraulic control units and other engine-mounted components. For procurement, the engine type and modification should be specified together with the pump designation.
The working medium for the PN-99 must be confirmed by the engine documentation. In descriptions of this pump, the medium may be referenced as fuel or oil depending on the system where the unit is installed. This should not be assumed during selection. A fuel-system version and a hydraulic / oil-system installation can have different requirements for seals, materials, testing and storage condition. Before installation, the pump should be checked against the required working fluid, operating pressure and engine technical documentation.
The PN-99 is historically associated with JSC “MPO named after I. Rumyantsev” in Moscow, a manufacturer known for aviation fuel and control equipment. The pump is aviation technical property and should be handled as a controlled precision unit. For aircraft engine use, documentation is important: passport, storage records, repair documents, bench-test data and traceability should be reviewed whenever available. Without documentation, the unit should be considered technically unconfirmed until inspected and tested.
For supply or replacement, the pump should be requested by its full designation: PN-99 / ПН-99. Before installation, the unit should be inspected for housing condition, drive interface, ports, sealing areas, corrosion, contamination, preservation state and signs of previous repair. Since available reference data does not specify operating pressure, performance, service life or assigned resource, these parameters should be checked through manufacturer documentation or engine manuals. Bench testing is recommended before installation in an aircraft engine system.
Product Type: Aircraft plunger pump
Designation: PN-99
Alternative Designations: ПН-99, PN-99
Function: Supply of working fluid within aircraft gas turbine engine systems
Application / Where Used: Gas turbine engine systems of military and special-purpose aviation equipment
System / Installation Area: Engine-mounted fuel or hydraulic system depending on configuration
Operating Role: Precision supply pump for engine subsystems
Pump Type: Positive-displacement plunger / piston pump
Compatible Engines: RD-33, RD-93, AL-31F gas turbine engines according to supplied reference data
Compatible Aircraft / Equipment: Fighter and combat aircraft equipped with compatible engine installations, depending on configuration
Associated Equipment: Fuel-regulating equipment, hydraulic control units and engine-mounted control components depending on engine layout
Working Medium: Not specified; fuel or oil depending on engine system documentation
Operating Pressure: Not specified
Performance: Not specified
Assigned Resource: Not specified
Assigned Service Life: Not specified
Storage Life: Not specified
Manufacturer Reference: JSC “MPO named after I. Rumyantsev” according to supplied reference data
Scope of Supply: Not specified; to be confirmed by purchase order and supplier documents
Inspection / Testing: Housing inspection, port cleanliness check, drive interface inspection, seal inspection, leakage check and bench testing according to engine documentation
Technical Documentation: Manufacturer technical documentation, product passport and engine documentation as applicable
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.