U139A

U139A pressure reducing valve for aircraft systems

U139A is an aircraft pressure reducing valve used as an aviation spare part for hydraulic or pneumatic systems of helicopters and aircraft. The unit is intended to reduce and automatically maintain a stable working pressure in control circuits and auxiliary aircraft systems. Depending on the specific installation and aircraft modification, the valve may work with compressed air or aviation hydraulic fluid. Its function is to provide regulated pressure to downstream units where direct system pressure would be too high or unstable for normal operation.

Pressure regulation function of the U139A valve

The U139A valve automatically reduces incoming pressure and maintains the required outlet pressure level within the controlled circuit. This allows connected units to operate under stable pressure conditions despite changes in supply pressure or system demand. The valve uses a mechanical spring-loaded regulating principle and does not require electronic control. In operation, this type of valve supports predictable system behavior and protects downstream elements from excessive pressure. Correct adjustment, cleanliness of the working medium and seal condition are important for stable pressure regulation.

U139A in hydraulic and pneumatic aircraft circuits

The U139A may be used in hydraulic or pneumatic control circuits, depending on the aircraft configuration and installation documentation. In pneumatic applications, the working medium is compressed air. In hydraulic applications, the medium may be aviation hydraulic oil approved for the aircraft system. Since the same general designation can appear in different maintenance contexts, the exact application should be checked against the aircraft parts catalog, system diagram and maintenance documentation before installation. This is especially important when selecting fittings, seals and compatible working medium.

Construction and operating principle of U139A

The U139A is a compact mechanically controlled pressure reducing unit. The body is typically made from high-strength aluminum alloy with protective anti-corrosion coating. The regulating mechanism is spring-loaded and operates automatically according to pressure balance inside the valve. This construction is suitable for aircraft environments where vibration, pressure fluctuations and temperature changes are expected. During inspection or overhaul, attention is normally paid to body condition, ports, fittings, spring mechanism, sealing surfaces and the absence of contamination inside the flow passages.

Alternative designation PU-7 for U139A

The U139A valve may also be referenced as PU-7 control valve / valve panel, depending on documentation and supplier terminology. When ordering the item, both designations should be checked to avoid confusion with similar aircraft pressure control units. The required aircraft type, system installation area, working medium and documentation requirements should be specified in the request. If the unit is supplied from storage or as repaired stock, the condition, test records, passport and traceability documents should be reviewed before acceptance.

Identification and supply of U139A

Before ordering U139A, it is useful to confirm whether a new-production unit, storage stock or repair stock is required. The buyer should also specify whether the product passport, authenticity documents and aviation technical property certificates are needed. Since pressure reducing valves are installed in controlled aircraft systems, documentation is important for maintenance acceptance and installation eligibility. For precise supply, it is also useful to confirm connection fittings, thread type, installation circuit and whether the valve will be used in a pneumatic or hydraulic system.

Product Type: Aircraft pressure reducing valve / control unit
Designation: U139A
Alternative Designations: У139А, PU-7, ПУ-7
Function: Reduction and automatic maintenance of stable working pressure
Application / Where Used: Aircraft hydraulic or pneumatic systems
System / Installation Area: Control circuits and pressure regulation units according to aircraft documentation
Compatible Aircraft / Equipment: Helicopters and aircraft using the U139A / PU-7 valve according to applicable documentation
Working Medium: Compressed air or aviation hydraulic oil, depending on aircraft system configuration
Control Type: Automatic mechanical spring-loaded regulation
Body Material: High-strength aluminum alloy with anti-corrosion protective coating
Weight: Approximately 0.42 kg
Weight Tolerance Reference: May vary by approximately ±0.03 kg depending on installed fittings
Condition: New, storage stock or repair stock, depending on availability
Technical Documentation: Product passport, aviation spare part documentation and authenticity certificates, if required

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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.