Showing results: 1 - 15 of 27 items found.
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Sigma Tek, Inc.
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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Sigma Tek, Inc.
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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Sigma Tek, Inc.
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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UMA, Inc.
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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UMA, Inc.
A device for measuring the forward speed of the aircraft.
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UMA, Inc.
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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TA-6055A -
Tech-Aid Products
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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Mensor Corp.
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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King Nutronics Corp.
For calibrating altimeters, airspeed indicators, rate-of-climbindicators and other avionic instruments.
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DO9847 -
Delta OHM S.r.L.
Combinations of all measurements in 3 channel portable datalogger: RH, temperature, pressure, airspeed, light, voltage and current.
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HD37AB1347 -
Delta OHM S.r.L.
Datalogger for indoor air quality analysis (IAQ). Measurement of airspeed, temperature, relative humidity, atmospheric pressure, CO² and CO.
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HD103T.0 -
Delta OHM S.r.L.
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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ADSE 550 -
ATEQ Aviation
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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TTU-205 Series -
TestVonics, Inc.
The TTU-205 Series are rugged, self-contained flightline test systems which can be used to accurately simulate in flight pressure conditions. This is done by precisely controlling and measuring Altitude and Airspeed pressure to aircraft’s pitot static system. The TTU-205 can be used to test, certify, calibrate, and troubleshoot aircraft pitot-static systems or associated pneumatic flight control systems. The dual channel operation allows operators to perform dynamic, qualitative calibration and leak test for "on ground" simulation of altitude and airspeed pressures. The accuracy and operational capabilities meets or exceeds test requirements for military as well as commercial aircraft. The TTU-205/J model is an RVSM compliant test set.
