It is out on the right wing lower surface. Just with the aircraft sitting there static the G3X reads 58F and the actual is 50F. Also ice seems to form on the wings before the G3X reads 32X.
Steve,
I let everything stabilize in the hanger overnight. The EGT and CHT's were dead on 50f and the OAT was on 52f. I will check the ring terminal and see what happens. Thanks for the quick response.
Jon
If they add a calibration, someone is bound to screw it up more than 4 degreesReally bizarre that there is no offset calibration in configuration mode to adjust it... By the way Aspen and MGL have this kind of calibration available on their products...
Regards,
Louis
If they add a calibration, someone is bound to screw it up more than 4 degrees
A gallon of water can be accurately measured by most anyone. There are lots of containers around that has a gallon capacity within 1%, not to mention most fuel pumps. Whereas I have yet to see a hangar with a calibrated temperature standard.We can calibrate our fuel tanks but not OAT?
As does Dynon.By the way Aspen and MGL have this kind of calibration available on their products...
Remember, RV speeds of 170+ knots does start touching into ram air heating (perhaps a degree F or two). I consider ice possible when OAT reaches 34 degrees. Now add the condition of sub-cooled liquid if clipping the top of a build up and you get ice.OAT probe position
It is out on the right wing lower surface. Just with the aircraft sitting there static the G3X reads 58F and the actual is 50F. Also ice seems to form on the wings before the G3X reads 32X.
Doesn't make any sense i have to change a 600$ probe for something it could be easily integrated in the software and make this working fine. As Garmin's competitors does...As does Dynon.
If the specs are that tight, I would look at installation. Make sure ring terminal is clean, no corrosion, and maybe add a ground wire from wing to fuselage. Any resistance more than 0.4 ohms will affect reading it seems. JMHODoesn't make any sense i have to change a 600$ probe for something it could be easily integrated in the software and make this working fine. As Garmin's competitors does...
I got the specification sheet from garmin and at 500 Ohms it should be 0 celcius.... tolerance is 499.40 to 500.60.
There is a small text funny to read at the bottom of the spec sheet :
''Note: There are no production tests performed on the probe. Any testing required will be at thediscretion of Quality Assurance, and will be performed as a part of receiving inspection.''
low cost sensor : https://vansairforce.net/threads/temp-sensor-for-gad13-or-gsu25.224929/Merci
Steve,
I let everything stabilize in the hanger overnight. The EGT and CHT's were dead on 50f and the OAT was on 52f. I will check the ring terminal and see what happens. Thanks for the quick response.
Jon
Ground is only for bounding not for reference to GSU25... my airplane is composite... I already made test with wire connected to ground and no difference...If the specs are that tight, I would look at installation. Make sure ring terminal is clean, no corrosion, and maybe add a ground wire from wing to fuselage. Any resistance more than 0.4 ohms will affect reading it seems. JMHO
Are your (resistantce type) fuel gauges accurate still?
Thanks for info, well appreciated...low cost sensor : https://vansairforce.net/threads/temp-sensor-for-gad13-or-gsu25.224929/
and curve for pt500 :