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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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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 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 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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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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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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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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Averaging Pilot Tubes
Meriam manufactures the widest range of Averaging Pitot Tubes for gases, liquids and steam with bi-directional flow capability. Under the Accutube brand name, there are four standard models; Inline, Insertion, Flanged and Wet Tap which can provide a flow solution for your toughest applications. To provide the complete flow solution that meets your specific needs, we can provide DP or Multivariable transmitters from the brand of your choice, or we will recommend the best fit for your application. These transmitters can be installed on the Accutube and configured to your specific flow requirements here at Meriam by qualified technicians, reducing your expense and time .
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Air Data Calibrator
ADC-2500V3
TestVonics ADC-2500V3 Air Data Calibrator is a high accuracy pitot static air dat calibrator. The calibrator is capable of controlling and measuring Altitude and Airspeed pressures with the highest degree of accuracy. The control and measurement ranges and accuracies of the calibrator meet and/or exceed requirements for both commercial and military applications . Currently all USAF PMEL organizations are standardizing their ADC-2500 calibrators to V3.
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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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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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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 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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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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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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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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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 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 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 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 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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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 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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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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Standard Airspeeds
These airspeed indicators have unrestrained movements.These instruments are actuated by ram air and ambient atmospheric pressure obtained from the aircraft pitot and static pressure systems. A moveable pointer and a fixed dial indicate airspeed with the zero index at the 12 o??lock position. Temperature compensation is internal and there is no external zero adjustment. Pointer damping is internally adjustable.
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Restrained Airspeeds
These airspeed indicators have restrained movements.These instruments are actuated by ram air and ambient atmospheric pressure obtained from the aircraft pitot and static pressure systems. A moveable pointer and a fixed dial indicate airspeed with the zero index at the 12 o’clock position. Temperature compensation is internal and there is no external zero adjustment. Pointer damping is internally adjustable.
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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.
