200M 400M 200M
RNG: 2.4 KM
BRG: 047°
ALT: 3,200 FT
SPD: 480 KTS
HDG: 012° N
TGT: ALPHA-7
MODE: SEARCH
PWR: NOMINAL
FREQ: X-BAND
STATUS: LOCK
NAVTGTWPNDEFRDRCOM
MIL-STD-1553IFF: ACTIVELINK-16: SYNC
SECTOR: ALPHA
THREAT: CLEAR
RADAR: ACTIVE
TRACK: 6 TGT
LAT 28.6213°N LON 77.3873°E
NX
Neometrix Target Acquired
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    Aircraft Servo Valve Hydraulic Test Equipment / 120–250 kg/cm² · 20–120°C ATF / Aero-Engine MRO / India
    ASVHTE · AERO-ENGINE SERVO VALVE TEST BENCH

    Aircraft Servo Valve Hydraulic Test Equipment, rated to 250 kg/cm² / 120°C ATF.

    A multi-circuit ATF hydraulic test bench that recreates aero-engine operating conditions for servo valves — high-pressure supply, 20–120°C thermal conditioning, and a dedicated drain circuit — with multi-stage filtration to 5–6 µm protecting micron-tolerance internal clearances.

    Aircraft servo valve hydraulic test equipment - elevated view of the enclosed ATF test cell with pumps, motors and control panel by Neometrix
    Fig · 01 Enclosed test cell · ATF hydraulic skid, filtration and control panel
    Test Pressure
    250kg/cm²
    Temperature Range
    20–120°C
    Fine Filtration
    5–6µm, β>1000
    Control Interface
    15in touchscreen HMI
    Test Cell Footprint
    3.6×4.2m
    01
    Overview

    The final gatekeeper before installation.

    Servo valves regulate fuel delivery, hydraulic actuation and dynamic response during throttle changes — every overhauled unit must be tested under conditions that precisely replicate the pressures, temperatures and dynamic loads it experiences in flight.

    Aircraft servo valve hydraulic test equipment wide view - full brick-walled ATF test cell enclosure with pump skid by Neometrix
    Fig · 02 Test cell enclosure · Beinlich pumps, ABB motors and copper ATF pipework

    The Aircraft Servo Valve Hydraulic Test Equipment, engineered by Neometrix Defence Limited, is a servo valve test stand that provides high-pressure ATF supply, controlled thermal environments from 20°C to 120°C, and stable flow regimes up to 250 kg/cm², enabling complete servo valve testing and functional validation of aircraft servo valves before they are cleared for installation on aero-engines.

    The equipment is built around an integrated multi-circuit hydraulic architecture that allows the operator to test the servo valve across its entire operating envelope. The primary high-pressure test circuit delivers regulated ATF at both 120 kg/cm² and 250 kg/cm², with stable temperature and flow control, while the drain circuit maintains a precisely controlled back-pressure vital for replicating an aircraft engine's internal manifold.

    One hundred twenty to two hundred fifty kilograms per square centimetre. Flight-ready, verified.

    A fully separate preservation circuit allows flushing, cleaning and long-term conditioning of the valve without cross-contaminating the main hydraulic loop — improving maintenance hygiene, reducing fluid degradation, and increasing repeatability across consecutive tests.

    02
    Architecture

    Six systems, one test cell.

    Every subsystem is engineered around replicating aero-engine conditions while protecting micron-tolerance servo valve clearances from contamination.

    Sub · 01

    High-Pressure Test Circuit

    Explosion-proof ABB motors and Beinlich pumps deliver stable, pulsation-free ATF at 120, 150 and 250 kg/cm² test pressure.

    Sub · 02

    Drain & Back-Pressure Circuit

    Maintains precisely controlled back-pressure, replicating the servo valve's behaviour inside an aircraft engine's internal manifold.

    Sub · 03

    Preservation Circuit

    Fully separate loop for flushing, cleaning and long-term conditioning of the valve without cross-contaminating the main test circuit.

    Sub · 04

    Thermal Control

    Dual-channel flameproof temperature sensors with closed-loop control and a plate-type heat exchanger hold ATF stable from 20°C to 120°C.

    Sub · 05

    Multi-Stage Filtration

    Coarse strainers, medium-pressure filters and fine high-pressure filters to 5–6 µm (β>1000), with clog indicators for real-time feedback.

    Sub · 06

    Operator Interface

    15-inch touchscreen HMI with integrated data acquisition, WIKA mechanical gauges, motorised and needle valves for precise flow control.

    03
    Downloads

    Design drawings.

    Design drawings for the Aircraft Servo Valve Hydraulic Test Equipment, available as PDF for procurement and technical review.

    04
    Specifications

    Full technical parameters.

    Key system parameters for the standard Neometrix Aircraft Servo Valve Hydraulic Test Equipment configuration.

    Test Pressure Range120 kg/cm², 150 kg/cm², 250 kg/cm²
    Operating Temperature Range20°C to 120°C
    Hydraulic FluidATF (Aviation Turbine Fluid)
    Filtration LevelsSuction: 100–150 µm; Medium: 10–16 µm; Fine High-Pressure: 5–6 µm (β>1000)
    Pumps & MotorsBeinlich high-pressure pumps, explosion-proof ABB motors
    Thermal Control SystemDual flameproof temperature sensors, closed-loop temperature controller, plate-type heat exchanger
    Control Interface15-inch touchscreen HMI with integrated data acquisition system
    System Layout FootprintApprox. 3600 × 4200 mm
    Safety FeaturesExplosion-proof sensors & motors, emergency stop, pressure relief paths, flameproof switches
    05
    Applications

    Where it clears valves.

    From MRO overhaul lines to R&D validation, the ASVHTE serves any facility that must certify servo valves before flight.

    A · 01Aircraft engine overhaul & MRO facilities validating servo valves during maintenance
    A · 02Aerospace hydraulic component testing for fuel, actuation and throttle-response valves
    A · 03Quality assurance & certification labs verifying performance and contamination-control standards
    A · 04R&D and engineering validation for teams developing or refining servo valve designs
    A · 05Failure analysis & troubleshooting of sluggish response, leakage or contamination
    A · 06Preservation & conditioning operations — flushing, de-aeration and long-term storage
    06
    In Depth

    The complete technical read.

    Engineering narrative for MRO engineers, procurement teams and QA managers who want the full picture before committing to an installation.

    Introduction

    Servo valves are among the smallest yet most consequential components inside an aircraft engine. They regulate fuel delivery, hydraulic actuation and dynamic response during throttle changes. Any inaccuracy — sluggish response, improper seat sealing or contamination — can directly affect thrust stability, altitude performance, or even trigger unsafe engine behaviour. Because of this, every servo valve leaving an overhaul facility must be tested under conditions that precisely replicate the pressures, temperatures and dynamic loads it experiences in flight. The Aircraft Servo Valve Hydraulic Test Equipment recreates these exact conditions, acting as the final gatekeeper ensuring that the aircraft's fuel and actuation subsystems remain dependable, consistent and safe.

    System architecture & operating philosophy

    The equipment is built around an integrated multi-circuit hydraulic architecture that allows the operator to test the servo valve across its entire operating envelope. The primary high-pressure test circuit delivers regulated ATF at both 120 kg/cm² and 250 kg/cm², with stable temperature and flow control. The drain circuit maintains a precisely controlled back-pressure, vital for ensuring the valve behaves the same way it would inside an aircraft engine's internal manifold. A fully separate preservation circuit allows flushing, cleaning and long-term conditioning of the valve without cross-contaminating the main hydraulic loop.

    • Functional testing under high-pressure ATF.
    • Servo valve priming and de-aeration.
    • Temperature-conditioned evaluation up to 120°C.
    • Drain pressure emulation to simulate engine manifolds.
    • Preservation flushing and storage conditioning.

    Thermal control & high-pressure performance

    Aircraft servo valves operate in harsh thermal zones, especially near hot engine sections. To simulate these conditions, the system employs dual-channel flameproof temperature sensors paired with a closed-loop thermal control architecture. The plate-type heat exchanger provides smooth and consistent ATF cooling, enabling temperature stability even during extended high-load tests. The high-pressure hydraulic loop — powered by explosion-proof ABB motors and precise Beinlich pumps — allows repeatable performance assessment at both medium and high pressure. The ability to test at 120 kg/cm², 150 kg/cm² and 250 kg/cm² ensures that the valve is validated for realistic flight loads, including transient conditions that occur during rapid throttle transitions.

    Filtration & contamination control

    Servo valves rely on micron-tolerance internal clearances. Even minute particulate contamination can cause drift, degrade response time, or lead to critical in-service failure. For this reason, the machine incorporates a robust multi-stage filtration chain beginning with coarse strainers and progressing through medium-pressure filters before reaching fine high-pressure filters rated at 6 µm and below, each featuring β-ratios above 1000. Clog indicators provide real-time feedback, prompting filter replacement before performance is compromised. All filter housings and wetted components are manufactured from aircraft-grade stainless steel or aluminium alloys, ensuring compatibility with high-temperature ATF and preventing internal corrosion during long-term operation.

    • Suction strainers (100–150 µm).
    • Medium filtration (10–16 µm).
    • Fine high-pressure filtration (5–6 µm).
    • Mechanical clog-indicator alerts.

    Operator interface, instrumentation & control philosophy

    The control panel gives the operator complete situational awareness during testing. Key parameters — temperature, pressure, flow rate, differential behaviour, drain pressure and electrical consumption — are visible at a glance through a combination of digital readings and high-accuracy WIKA mechanical gauges. A 15-inch touchscreen HMI, integrated with a data acquisition system, ensures that all measurements can be monitored, logged and analysed with high fidelity. Flow control is achieved through a combination of motorised valves, needle valves and precision 3-way valves chosen specifically for high-temperature, high-pressure aircraft applications. Safety features such as flameproof switches, explosion-proof motors, emergency-stop provisions and pressure relief paths ensure that both the equipment and operator remain protected even under abnormal load conditions.

    Structural layout & ergonomic design

    According to the GA drawing, the system is divided into a working table and a standing platform, enabling a clean separation between operator space and high-pressure rotating machinery. The test cell layout, occupying roughly 3600 × 4200 mm, is compact yet spacious enough for maintenance access. Pumps, motors and hydraulic skids are positioned to allow straightforward serviceability, while the test table and control panel remain at the front of the test cell for operator convenience.

    • Clean segregation of test area and power sections.
    • Easy access to filtration units, heat exchangers, sensors and valves.
    • Logical hose and pipe routing for safety and clarity.
    • Compact footprint suitable for aircraft MRO shops.

    Safety & reliability built for aviation

    All components used — including the flameproof sensors, explosion-proof motors, diaphragm accumulators, high-pressure relief valves and visual level indicators — reflect an aviation-centred safety philosophy. The equipment is designed to withstand sudden pressure deviations, unexpected flow surges and operator errors without compromising the integrity of the test or the safety of personnel. Its multi-layered redundancy ensures that any servo valve tested on this platform is assessed with the same level of caution and precision that governs the aviation industry itself.

    Conclusion

    The Aircraft Servo Valve Hydraulic Test Equipment from Neometrix Defence Limited is a precision-engineered solution designed to ensure the safety and performance of aircraft servo valves. With high-pressure simulation, thermal conditioning, contamination-control architecture and an operator-friendly control interface, the system delivers complete confidence that every tested valve is restored to flight-ready reliability — an indispensable tool for any aircraft engine overhaul facility where precision, consistency and safety define the operational standard.

    07
    FAQ

    Common questions.

    Plain-language answers from the engineering team.

    Q · 01 What is an Aircraft Servo Valve Hydraulic Test Equipment?
    It is a specialised aircraft servo valve test bench used to verify and calibrate servo valves for aero engines. It recreates real operating conditions with ATF at high pressure, acting as an aviation hydraulic test rig and aircraft component test stand for aircraft MRO facilities.
    Q · 02 Why is a dedicated aircraft servo valve test bench needed in an MRO facility?
    A dedicated test bench ensures accurate testing of fuel control and hydraulic servos before they return to service. Using a controlled ATF high-pressure test stand reduces failures on wing, improves reliability, and adds traceability to aircraft component test procedures.
    Q · 03 Can this system also test aircraft fuel control valves?
    Yes, the same platform can function as an aircraft fuel control valve test bench and an aerospace servo valve calibration station, making it a versatile aircraft component test stand for multiple hydraulic devices.
    Q · 04 What pressure and temperature range does the equipment support?
    The system delivers regulated ATF at 120 kg/cm², 150 kg/cm² and 250 kg/cm² test pressure, with closed-loop thermal control from 20°C to 120°C, covering the servo valve's full flight-load envelope.
    Q · 05 How is fluid contamination controlled?
    A multi-stage filtration chain progresses from 100–150 µm suction strainers through 10–16 µm medium filters to 5–6 µm fine high-pressure filters rated at β>1000, with clog indicators giving real-time feedback before performance is compromised.
    Q · 06 What is the difference between the test circuit and the preservation circuit?
    The primary high-pressure circuit delivers regulated ATF for functional testing, while a fully separate preservation circuit allows flushing, cleaning and long-term conditioning of the valve without cross-contaminating the main hydraulic loop.
    Q · 07 What safety features protect the equipment and operator?
    Flameproof temperature sensors, explosion-proof ABB motors, diaphragm accumulators, high-pressure relief valves, emergency-stop provisions and visual level indicators together protect against sudden pressure deviations and unexpected flow surges.
    Q · 08 What is the equipment's footprint and layout?
    The test cell occupies approximately 3600 × 4200 mm, divided into a working table and a standing platform to separate operator space from high-pressure rotating machinery, while keeping filtration units, heat exchangers, sensors and valves accessible for maintenance.
    Q · 09 Is the Aircraft Servo Valve Hydraulic Test Equipment customizable?
    Yes, Neometrix offers customized versions of the equipment tailored to specific client requirements, operational parameters, and servo valve types.
    Q · 10 How can I get a quotation for the Aircraft Servo Valve Hydraulic Test Equipment?
    You can request a quotation by contacting Neometrix Engineering Pvt Ltd through https://neometrixgroup.com/products/aircraft-servo-valve-hydraulic-test-equipment or by phone at +91-7777-876-876.
    Get a proposal

    Tell us your servo valve
    test requirements.

    We size the test circuit, configure filtration and thermal control, and walk through documentation and site requirements with your MRO team before you commit.

    Request proposal +91 7777 876 876

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    NATO STANAG
    RTCA/EUROCAE DO-160
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