alfadog
Final Approach
Or cylinder leak-down testing, if you prefer.
So I consider myself a fairly green A&P. I've got now about 2 years under my belt of actual twirling wrenches and bucking rivets. For a while when I was doing a compression test, I would position the prop at what felt like top dead center against the 80 psi and take what I got as being the number. Meaning that I was kind of halfway between when it would snatch forward and when it would snatch backwards. But I found that I was getting a few low numbers but if I did it a different way I would get a better number. The different way being I would see what position of the prop in that narrow band before the pressure in the cylinder moves the prop one way or another, gave me the highest reading on the right-hand gauge. Meaning that I would rotate the prop in the direction of normal rotation and if I found a position where the prop would hold and the pressure was its highest, then maybe I should be using that number.
Question one, does that sound right to you? If not, how would you go about doing it differently?
Which brings us to question two. So, on the last engine I did a compression check on a few days ago, one cylinder would only give a decent reading when it was just about ready to snatch the prop forward. Like the slightest vibration and the prop would shoot forward. It was not in that sweet spot but was really far forward. Did I mention that it was far forward? So I took that number based on my thinking that that's how I should go about it. What could have caused it to act that way? A very small ridge or some rust in the cylinder at TDC or a sticky ring? This airplane has been sitting for awhile.
So I consider myself a fairly green A&P. I've got now about 2 years under my belt of actual twirling wrenches and bucking rivets. For a while when I was doing a compression test, I would position the prop at what felt like top dead center against the 80 psi and take what I got as being the number. Meaning that I was kind of halfway between when it would snatch forward and when it would snatch backwards. But I found that I was getting a few low numbers but if I did it a different way I would get a better number. The different way being I would see what position of the prop in that narrow band before the pressure in the cylinder moves the prop one way or another, gave me the highest reading on the right-hand gauge. Meaning that I would rotate the prop in the direction of normal rotation and if I found a position where the prop would hold and the pressure was its highest, then maybe I should be using that number.
Question one, does that sound right to you? If not, how would you go about doing it differently?
Which brings us to question two. So, on the last engine I did a compression check on a few days ago, one cylinder would only give a decent reading when it was just about ready to snatch the prop forward. Like the slightest vibration and the prop would shoot forward. It was not in that sweet spot but was really far forward. Did I mention that it was far forward? So I took that number based on my thinking that that's how I should go about it. What could have caused it to act that way? A very small ridge or some rust in the cylinder at TDC or a sticky ring? This airplane has been sitting for awhile.