|3-1/8 UMA Airspeed Indicator|
Range: 40-240 MPH
These highly accurate Airspeed Indicators use a diaphragm to sense the difference between the pitot pressure and static pressure. Standard dial markings are black and white. NON TSO Approved. Intended for use in experimental aircraft only.
Note: An inverter is required for the Internal Lighting Option (P/N 10-02083 UMA 14V LIGHT INVERTER)
WARNING: The product may contain and/or expose you to a chemical(s) or substance(s) which are known to the State of California to cause cancer and/or birth defects or other reproductive harm. www.P65Warnings.ca.gov
Possibly 5 stars once I install and test. Quality and service good. Thank you AS.
Had to return my 0-240 kts UMA 2.25 gauge as it was reading 15 to 25 kts too fast per manometer test. Checked the new one that came in as replacement and it's spot on.
Way off. Reads 20 knots too slow.
WAY off, right out of the box. Read about 30% too low. Confirmed via water manometer check and against a 2nd airspeed indicator (+ GPS) in aircraft. Very disappointing that UMA does not seem to test/calibrate their ASIs before the ship them??? Last time I will buy a UMA gauge.
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The depth of 10-00512 is 3.25 inches.
These UMA instruments are manufactured in the USA.
Yes, add part # 10-02792 to your order for custom UMA range markings. (See Accessories)
Part # 10-04925 comes with 20-160 MPH.
When you add the main gauge to your cart, a popup will be displayed with the available options. You then select the custom range marking option and it will be added to the cart along with the gauge. Please keep in mind that custom range markings are special order and we cannot add to the unit that is in stock.
No you must order the lighting option as well as the inverter. the lighting option p/n: 11-07239 and the inverter is 10-02083.
These are intended for install in experimental aircraft only. If your aircraft is certified these cannot be legally installed.
Yes they just need pitot/static to function.
TSO refers to the FAA Approval. TSO instruments can be installed in certified aircraft. Non TSO can only be installed in experimental category aircraft.