NP-43M-1

NP-43M-1 in aircraft hydraulic systems

The NP-43M-1 is an aircraft axial piston high-pressure hydraulic pump used to supply working fluid to onboard hydraulic systems. It belongs to the rotary piston / axial plunger pump family and is designed for systems where stable high-pressure hydraulic power is required. In aircraft operation, pumps of the NP-43 series are used to feed hydraulic circuits that operate flight-control-related mechanisms, landing gear systems, braking systems, wing high-lift devices and other hydraulic consumers, depending on aircraft configuration.

Hydraulic pressure generation by the NP-43M-1

The main function of the NP-43M-1 is to generate hydraulic pressure and deliver working fluid into the aircraft hydraulic system. The pump is rated for high-pressure operation and is used where hydraulic actuators need reliable pressure under changing load conditions. Since this is a variable-displacement pump, it is not just a fixed-flow supply unit. Its output adjusts according to the system demand and control logic, which helps maintain the required pressure while reducing unnecessary flow when demand is lower.

NP-43M-1 variable-displacement design

The NP-43M-1 is built as an axial piston pump with a rotating cylinder block and variable delivery. This design is typical for aircraft hydraulic systems where compact size, pressure capability and controlled output are required. The pump includes a through drive shaft arrangement and is intended for installation on an aircraft accessory gearbox or related drive point. Because the unit is mechanically driven, correct spline condition, drive alignment, mounting flange fit and seal condition are essential for reliable operation.

NP-43M-1 working fluid and cleanliness requirements

The pump operates with aviation hydraulic fluid, typically AMG-10 according to GOST 6794-75. For an axial piston pump, fluid cleanliness is critical. Contaminated hydraulic fluid, wrong viscosity, air in the suction line, low inlet pressure or blocked filters can cause wear, noise, pressure instability and reduced service life. If the pump does not reach normal pressure, the cause may be inside the pump, but it may also be in the hydraulic tank, suction line, filter, drainage line or downstream consumers.

Installation of the NP-43M-1 pump

The NP-43M-1 is mounted by flange connection, with sealing provided by a rubber O-ring according to the installation design. The drive is normally made through a splined connection to the aircraft accessory gearbox, for example on engine-related installations such as the D-30 system used on Tu-134 aircraft. The pump has standard connection points for suction, pressure and drain lines. Before installation, the mounting flange, splines, fittings, seals and drainage connection should be checked carefully, because small installation issues can lead to leakage, cavitation or drive damage.

Application of NP-43M-1 on aircraft and test systems

The NP-43M-1 is used in aircraft hydraulic systems and may also be applied in ground hydraulic test benches where aircraft hydraulic units are checked under pressure. Pumps of the NP-43 series are associated with Tu-134 and Tu-134A aircraft hydraulic systems, depending on the modification and installed equipment. The same pump family includes several versions, so applicability must be verified by the aircraft parts catalog, hydraulic system diagram and equipment documentation before replacement.

NP-43M series versions and identification

The NP-43M family includes several modifications, including NP-43M-1, NP-43M-2, NP-43M-3 and NP-43M-5. These versions may differ by installation details, adjustment, drive interface, port layout or application. For procurement, the exact full designation should be used rather than the general NP-43 name. When replacing a pump, it is useful to confirm the aircraft type, engine or accessory gearbox installation, required hydraulic fluid, pressure setting, documentation requirements and whether the unit must be new, overhauled or tested serviceable.

Supply and inspection of NP-43M-1

For aircraft use, the NP-43M-1 should be supplied with available passport, repair or bench-test documentation. Before installation, the pump should be inspected for housing condition, shaft and spline condition, flange face, port threads, seals, drainage fitting, external damage, corrosion and storage state. Bench testing is strongly recommended for high-pressure hydraulic pumps, because external appearance does not confirm delivery, pressure regulation or leakage level. A serviceable pump should build pressure, regulate correctly and operate without abnormal noise, vibration or overheating.

Product Type: Aircraft axial piston / rotary plunger hydraulic pump
Designation: NP-43M-1
Series: NP-43M
Other Series Modifications: NP-43M-2, NP-43M-3, NP-43M-5
Function: Supply of high-pressure working fluid to aircraft hydraulic systems
Application / Where Used: Aircraft hydraulic systems and ground hydraulic test benches
System / Installation Area: Main hydraulic circuits; hydraulic power supply lines depending on aircraft configuration
Typical Hydraulic Consumers: Control circuits, landing gear extension / retraction, braking system, wing high-lift devices and other hydraulic mechanisms depending on system layout
Compatible Aircraft / Equipment: Tu-134, Tu-134A and related hydraulic systems depending on configuration
Working Fluid: AMG-10 aviation hydraulic fluid according to GOST 6794-75
Pump Type: Rotary piston / axial plunger pump
Design Type: Variable-displacement axial piston pump
Nominal Working Pressure: 21 MPa / 210 kgf/cm²
Nominal Flow Rate: 35 L/min at nominal shaft speed
Fluid Temperature Range: −60 to +125 °C
Drive Type: Mechanical drive through splined shaft
Drive Arrangement: Through cardan drive shaft with rotating cylinder block
Installation: Flange-mounted on aircraft accessory gearbox or hydraulic drive point depending on aircraft system
Sealing: Rubber O-ring in flange connection
Hydraulic Ports: Suction line, pressure line and drain leakage line to hydraulic tank
Dry Weight: 12.1 kg
Technical Documentation: Product passport, operating manual and aircraft hydraulic system documentation as applicable

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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.