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Pitot Tubes
The dpm-i Pitot Tube is a new design concept in Pitot Static Tube technology. It is a multi-functional sensor. It can replace thermally heated instruments, where power requirements are high. Gives easy access to duct measurement compared to a standard Pitot Tube. For example, in ceilings voids and confined areas, where there is a thick lagging or metal cladding.
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PITOT STATIC TESTER
ADSE 745
The ADSE 745 caters fully for all aircraft types and the different electrical power supplies.It can be used for testing high performance civil and military aircraft, fix and rotary wing. The multi-pressure outlets option can suit the more complex pilot-static-systems. This Pitot Static Tester is designed primarily for flightline use to cover the testing of all barometric and manometric pressure instrument systems.
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Pitot Static Tester
ADSE 650
The ADSE 650 caters fully for all aircraft types and the different electrical power supplies.It can be used for testing high performance civil and military aircraft, fix and rotary wings. This Pitot Static Tester is designed primarily for flightline use to cover the testing of all barometric and manometric pressure instrument systems.The large touch screen display, with on-screen help ,enables all checks to be carried out easily on the flight deck or in the cockpit, by a single operator.
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Pitot Static Tester
ADSE 550
The ADSE 550 pitot static tester, housed in a plastic carrying case, is a portable, self contained field tester designed to test aircraft pilot ans static systems for leaks as well as the operation and calibration of airspeed, altimeter, engine pressure ratio, manifold pressure indicators, and other vacuum or low pressure units. The tester consists of a hand-operated vacuum pump, a hand-operated pressure pump vacuum and pressure gauges, 5 control valves, an altimeter and an airspeed indicator. The package accessories include two 25-foot hoses.
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Pitot Static Tester
ADSE 643
The ADSE 643 caters fully for all aircraft types and the different electrical power supplies.It can be used for testing high performance civil and military aircraft, fixed and rotary wing.This Pitot Static tester is designed primarily for flightline use to cover the testing of all barometric and manometric pressure instrument systems.The ease of use and portability enables all checks to be carried out easily on the flight deck or in the cockpit, by a single operator.The test set is housed in an anodized metal and rugged case.An attached case contains the pressure hoses and electrical cables.
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Pitot Static Tester
ADSE 746
The ADSE 746 caters fully for all aircraft types and the different electrical power supplies. It can be used for testing high performance civil and military aircraft, fixed and rotary wing. Themulti-pressure outlets option can suit themore complex pilot-staticsystems.This Pitot Static tester is designed primarily for flightline use to cover the testing of all barometric and manometric pressure instrument systems. The large touch screen display, with on-screen help, enables all checks to be carried out easily on the flight deck or in the cockpit, by a single operator. The test set is robust and housed in a mobile weatherproof case fitted with tire wheels. An attached bag contains the pressure hoses and electrical cables.
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Pitot Static Indicator
ADSE 740
The ADSE 740 is a complete high performance dual pressure Ps and Pt standalone test bench specially designed to be used in the workshop or in the laboratory to test and calibrate all air data equipment such as altimeters, vertical speed indicators, air speed indicators, MACH-meter, air data computers ...) and sensors.
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Pitot / Static Tester
ADSE 743
The ADSE 743 caters fully for all aircraft types and the different electrical power supplies.
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Pitot Tube Flow Meter
PTFM-1000V2
The Pitot Tube Flow Meter, PTFM-1000V2 is a standalone interface for measuring exhaust gas flow rate of combustion engines. The system uses the tried-and-tested pitot tube principle with high-frequency transducers to accurately measure highly pulsating exhaust flows with a sampling rate of 1kHz. This rapid capture rate ensures that any pulsations or exotic behaviour in an engine is measured, and the unique design of the PTFM pitot tube means reverse flows can be measured with the same guarantee of sensitivity. The interface can be run standalone with a laptop, or seamlessly integrated to run alongside an analyser system without adding any more steps to the test cycle process.
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Pitot Static Breakout Box (PSBB)
C-17
The C-17 Pitot Static Breakout Box is a derivative of TestVonics™ Line Switching Unit (LSU) Series. The assembly includes a multi-port distribution unit which provides 4 Pitot and 8 Static outputs from one channel of Pitot and Static controlled pressure. The LSU distributes pitot static supplies for the external services and connection of hose assemblies for testing of aircraft Pitot and Static ports for the C-17. The lightweight unit is housed in a highly durable and easy to maneuver case. Additionally, four (4) 30ft Pitot Hoses, eight (8) 30ft Static hoses, and two hose storage bags are included with the assembly.
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Pitot Static Tester / AoA TESTER
ADSE 744
This tester was specifically designed for the new-generation pitot tubes that integrate sensing probes, pressure sensors and powerful air data computer processing to provide all critical air data parameters including Pitot and static pressure, airspeed, altitude, and angle of attack. This Pitot Static tester is designed primarily for flightline use to cover the testing of all barometric and manometric pressure instrument systems. The AoA Channel behaves as a second Ps channel, in order to create a differential pressure between the 2 Ps Channel, allowing to performsimulations of different Angles of Attack. The large touch screen display, with on-screen help, enables all checks to be carried out easily on the flight deck or in the cockpit, by a single operator. The ADSE 744 is robust and housed in amobile weatherproof case. An attached bag contains the pressure hoses and electrical cables.
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Dual Pitot Tube Flow Meter
PTFM-ONE-DT
The Dual Pitot Tube Flow Meter, PTFM-ONE DT is a standalone interface for measuring exhaust gas flow rate of combustion engines. The system uses the tried-and-tested pitot tube principle with high-frequency transducers, with a sampling rate of 1kHz to accurately measure highly pulsating exhaust flows. This rapid capture rate ensures that any pulsations or exotic behaviour caused by the engine is measured, and the unique design of the PTFM-ONE DT means reverse flows can be calculated, with the same guarantee of sensitivity.
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Pitot / Static Tester for Laboratories and Workshops
ADSE 741
The ADSE 741 is a complete high performance three channel Ps, Pt and AoA stand-alone test bench specially designed to be used in the workshop or in the laboratory to test and calibrate all air data equipment such as altimeters, vertical speed indicators, air speed indicators, pneumatic AoA (Angle of Attack) indicators, MACH-meter, air data computers, specific probes and sensors.The high precision embedded sensors enable the ADSE 741 to be used as a pressure standard.The user interface is programmed underWindows and Labview, with a data base managed in a spreadsheet for easy evaluation, management, statistics and presentation.
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High Temperature Pitot Probe Protective Cover
This Pitot Probe Cover developed by Nav-Aids Ltd. withstands temperature to 950 degrees F when installed on the pitot tube.With the Nav-Aids Ltd. High Temperature Pitot Probe Cover installed on the pitot tube, and the heat inadvertently activated, there will be : No melting of material No significant residue on the pitot tube No filling of static or drain holes No need to change a pitot probe No cause for aircraft dispatch delay
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Pitot Static Test & RVSM Air Data Accs Kits
ADA320-723
Kit Model ADA320-723 (Bar type) contains the equipment required to connect the Air Data Tester to the pitot and static ports, for the performance of a complete test of the main and alternate Air Data System of the Airbus Industries A-319, A-320, A-321 aircraft. The equipment is approved by Airbus Industries.
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Air Speed Micromanometer-Thermometer
HD2134P.0
Micromanometer-Thermometer for air speed and flow rate measurement by means of Pitot tubes
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Air Speed Micromanomenter-Thermometer Data Logger
HD2134P.2
Micromanometer-Thermometer Data Logger for air speed and flow rate measurement by means of Pitot tubes
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Pilot Static Adapters and Kits
TestVonics offers Pitot Static Adaptors and Kits for most of the worlds aircraft including Civil, Commuter, Corporate, Military, and Helicopters. Pitot Static Adaptor Kits & Air Data Accessories are manufactured to the highest standards by skilled technicians using only the best materials available. These products are unrivaled in quality & simplicity of design.
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Alnor Micromanometer
AXD610
The Alnor® Micromanometer AXD610 is an easy to use, handheld digital micromanometer for fast, accurate and reliable pressure measurement. It can also calculate velocity when used with a pitot tube. Ideal applications include HVAC commissioning and troubleshooting, testing and balancing, Pitot tube duct traverses, static pressure measurements and differential pressure measurements.
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Pressure Sensors For Motorsport
Our range of Pressure Sensors for Motorsport Applications. Includes EPT pressure transducers and pressure sensing pitot sensors.
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Line Switching Unit Series
TestVonics™ Line Switching Unit (LSU) is a multi-port distribution unit which can provide up to 6 outputs from one channel of controlled pressure. The LSU distributes pitot static supplies for the external services and connection of hose assemblies for testing of aircraft Pitot and Static ports. The lightweight unit is housed in a highly durable and easy to maneuver case.
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Air Speed Micromanometer-Thermometer
HD2114P.0
Handheld Micromanometer-Thermometer with LCD display for air speed and flow rate measurement by means of Pitot tubes, full scale 20 mbar for speed measurements from 2…55 m/s.
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Air Data Tester
PS131bII
Aircraft Development Industries cc
The Model PS131bII is an advanced Air Data - Pitot Static Tester, which drastically simplifies the process of testing the aircraft's Pitot and Static system. The test altitudes, airspeeds and vertical speeds are achieved by simply typing in the values and the tester will automatically do the rest. The Model PS131bII is a completely digital, microprocessor-controlled device using all solid state transducers and components.
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Air Speed Micromanomenter-Thermometer Data Logger
HD2114P.2
Handheld Micromanometer-Thermometer data logger with LCD display for air speed and flow rate measurement by means of Pitot tubes, full scale 20 mbar for speed measurements from 2…55 m/s.
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Micromanometer
6700
The Handheld Micromanometer – Model 6700 can be used with pitot tubes, flow grids, differential pressure tubing, or the optional velocity-grid (for average face velocity readings). It comes standard with the Model 6715 TABmaster Capture Hood, but is also available for purchase separately.
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Differential Pressure Instruments
The testo 512 differential pressure meter is available as four models. This model has a measuring range from 0.0.29 psi and is ideal for measuring pressure differences at filters and for carrying out pitot static tube measurements in air ducts at air flow speeds between 16 and 180 fps.
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Pressure Gas Leak Detectors
The testo 512 differential pressure meter is available as four models. This model has a measuring range from 0.0.29 psi and is ideal for measuring pressure differences at filters and for carrying out pitot static tube measurements in air ducts at air flow speeds between 16 and 180 fps.
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Alnor Micromanometer
AXD620
The Alnor® Micromanometer AXD620 is a rugged, compact, comprehensive micromanometer that measures pressure. It can be used with pitot tubes to measure velocity and then calculate flow rates with user–input duct size and shape. Premium features make it ideal for HVAC, environmental safeguards, commissioning, process control and system balancing.
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True Airspeeds
These true speed indicators are differential pressure indicators that measure the difference between static and total pressure produced by ram air from the pitot. The indicated airspeed can be corrected for changes in altitude by turning the knob to align the outside air temperature with the altitude. The moveable airspeed scale will then show the actual, or true, airspeed.
