Gang,
The vast majority of answers on this subject have focused on the filtration benefits of the gascolator. I think Dennis Johnson's observations are spot on. If one carefully sumps the tanks (ensuring the aircraft is sitting on a level surface) prior to engine start it would be nigh impossible to get a coherent slug of water large enough and to interfere significantly with engine operation. This is especially true for fuel injected Continental installations, where a significant portion of the fuel pumped to the engine is unused and returned to the tank. Is it possible for a very large slug of water to remain coherent in five gallons of fuel while agitated by aircraft motion and fuel recirculation? I suppose it is, but it seems unlikely to me.
That aside, no one has mentioned ever finding water in the gascolator of their Lancair. Which makes sense, because in order to do so water would have flow uphill while on the ground, or remain separated enough from the fuel to fall out while flowing thru the gascolator at something approaching a half-a-gallon per minute while the engine is running.
Regarding the filtration capabilities of the gascolator; I've emailed Andair for more information on the specifications (filtration level, filter material area, max fuel flow, etc.), but they have yet to respond. If anyone has this information I would greatly appreciate it.
Kevin Stallard suggested the gascolator would appear to be a better option as a filter than an inline style. The type of inline filter I'm talking about is not your prototypical one-inch diameter, one-inch long plastic see-thru filter we've all seen on our lawnmowers. I talking about something more like this:
This filter is 1.75" in diameter and 6.25" long. If the filtration media was a simple cylinder that size would yield 30+ square inches of filtration area. Since the media is pleated (much like your typical oil filter), the filtration area is actually much larger. Maximum flow rate is 150 gph, which is more than three times that required for an IO-550. That suggests this filter could be two-thirds clogged with crud and still have adequate fuel flow. And let's not forget there would be one filter for each tank; if one clogs I can still switch tanks.
Additionally, this isn't a throw-one-in-and-hope-it-works scenario. These filters would be installed in a location making it exceptionally easy to remove for inspection/servicing--something that would occur following every engine run up to first flight. My reasoning is that such a test regimen will reveal any problems of the type mentioned here.
Thoughts?
--Mark