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Old November 30th 19, 04:21 PM posted to rec.aviation.soaring
Scott Williams[_2_]
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Posts: 83
Default Pitot/static leak issues when using a "squat switch"

On Saturday, November 30, 2019 at 12:45:34 AM UTC-6, Darryl Ramm wrote:
On Friday, November 29, 2019 at 8:45:37 PM UTC-8, wrote:
On Friday, November 29, 2019 at 5:58:13 PM UTC-8, Charles Longley wrote:
Yeah I am familiar with how a squat switch works. There’s no suspension in an ASW-20 except the tire so no place to put the squat switch.. I’ll take a look at it when I do the Condition Inspection. Maybe something will come to me.


Can anyone show me the FAA regulation that requires a squat switch in a glider?


You are repeating yourself. I answered this same question from you in the tenth post of this thread. Have regulations change since then?

You may not agree with the reasoning there, I think it's *awfully* written FWTW, but I'm pointing out this is the interpretation used in the avionics industry. I also think it was an bad idea for the FAA to require this for light aircraft and I wish they had left that with the RTCA DO-260 standard of not requiring light aircraft to transmit in ground mode at all (continue transmitting ADS-B airborne messages on on the ground).


Having had a trig 2020 compliant ADS-B out system installed in my Standard type certificated glider, I found the peregrine pneumatic switch elegant, compact, cheap, and reliable. not to mention readily available and acceptable to the documentation requirements.
I also understand the deep desire some have to 'invent a better mousetrap'
Good lift,
Scott