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Active Air Speed Transmitter
HD103T.0
Active air speed transmitter with hotwire sensor. Probe with 5m cable. Speed 0.1…5 m/s. Outputs for temperature and airspeed.
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TSO'd Airspeed
Airspeed Indicator is intended for use on an aircraft to indicate the speed relative to the air at sea level and at any other altitude, to indicate the equivalent speed corresponding to the actual force of the air.
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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.
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Air Data Test Sets
For calibrating altimeters, airspeed indicators, rate-of-climbindicators and other avionic instruments.
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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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Mach Airspeed Test Fixture
TA-6055A
The TA-6055A is a Mach Airspeed Test Fixture built to support the testing and repair of the 2082 and 2083 series of Servoed Mach Airspeed Indicators (SMASI) used in some Boeing aircraft. These mach airspeeds are synchro driven and require a coarse and fine input for altitude and a third input for airspeed. This test fixture was designed around the test procedure and is interfaced with our TA-1001 panel which provides for two of the synchro sources and two Angle Position Indicators (API).
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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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All Measurements 3 Channel Portable Data Logger
DO9847
Combinations of all measurements in 3 channel portable datalogger: RH, temperature, pressure, airspeed, light, voltage and current.
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Air Data
Testing altitude and airspeed components in commercial and military air data applications are critical for the safety and performance of an aircraft. Mensor air data test set and indicators provide the high accuracy necessary for these applications. Air Data Test Sets control altitude /altitude rate and airspeed /airspeed rate, for testing altimeters and airspeed indicators or air data computers in a dynamic way that simulates actual flying conditions. Air data Indicators measure Altitude /Altitude Rate and Airspeed /Airspeed Rate for applications where conditions are externally controlled.
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Datalogger for IAQ Analysis
HD37AB1347
Datalogger for indoor air quality analysis (IAQ). Measurement of airspeed, temperature, relative humidity, atmospheric pressure, CO² and CO.
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Portable Testing Kit for Gulfstream Aircraft
ES-429TK-101
The ES-429TK-101 Portable Testing Kit (for Gulfstream aircraft) enables you to simulate Airspeed, Altitude and Radio Height values over an ARINC 429 bus. The ES-429TK-101 Portable Testing Kit consists of a DAS-429UNET/RT10, battery and the Exc429Tester application that runs on the host computer, a laptop or desktop PC running Windows. Using the ES- 429TK-101 Portable Testing Kit with a laptop provides a portable testing system.
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Pitot-Static Tester
PS-425
The PS-425 Pitot-Static tester is a low-maintenance, digital tester that is fully portable. The PS-425 is powered by an internal rechargeable 12 volt battery (included in purchase), which enables the test set to be used completely independent of any external power source. A connector is provided for an external 12 volt DC power adapter (included). The PS-425 incorporates the altitude, VSI, and airspeed in one single display. The PS-425 is designed and priced for non-RVSM markets, and includes two quick-connect hoses, 12 VDC power adapter, calibration certificate, and a limited 2-year warranty. This product is ideal for performing simple go/no-go leak tests, as well as for general use as a low-end pitot-static tester.
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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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Airspeed Warning Switches
Supply Voltage: 10÷30 Volts DC Current Rating: 200 mA max Switching Power: 5 A max 30VDC Temperature Range: -40° C to 120° C Pressure Fitting: 1/8" plastic Weight: 3.2 oz.
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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 / 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.
