Jamie
Well Known Member
Way back when I was building my wings I decided to look for a good used pitot from an aircraft salvage yard rather than pay > $1000 for what amounts to nothing more than a tube with a heater element in it.
I called up a couple of salvage yards and found a good pitot off of a 1976 Skyhawk. I had read that the Gretz mount would work fine with this pitot so I bought it ($80.00!). A little filing and it fit perfectly.
Unfortunately, from my first flight I have been having IAS problems -- my IAS was typically 8 knots below where it should have been. I have two airspeed indicators (mechanical unit from Van's and my Dynon) and they read exactly the same airspeed. I did all of the usual debugging on this issue, including checking for static errors and pressure testing both pitot and static systems. In the course of my testing I found a small pitot leak on the back of my Dynon but that was easily remedied with the application of teflon tape to the threads. Alas, this still didn't fix my problem.
Since I had no pitot system leaks and no static position error or leaks it only left one thing -- an error with the pitot itself.
I borrowed a Gretz Pitot from a builder friend of mine (Steve Ashby, RV-8A builder, VAF forum member and one of the nicest guys you will ever meet) which fit right into my mast and flew it. Airspeed indication was definately up so I knew I was on the right track.
Back on the ground I re-installed my pitot. On the Cessna pitot there is a little drain hole on the bottom/back of the unit that allows the line to drain if the pitot freezes over (meaning that it will drop to 0 on the ASI). For my pressure testing I taped over this hole (obviously) but would remove the tape to go and fly.
Last night I decided to tape over that hole and fly. Voila...everything was perfect. I did 4-way GPS runs and entered the numbers into the GPS PEC spreadsheet (everyone should use this document for airspeed testing). My TAS on the Dynon was within 1 knot of the value calculated by the GPS PEC spreadsheet.
I will mix up some epoxy and plug that hole. Of all of the other heated pitots I have seen, none have a drain hole like the one on the Cessna pitot, so plugging that hole will give me the same safety level as those other pitots.
I had suspected the drain hole from the start, but everyone was telling me that couldn't be the problem. I should have gone with my instincts from the start.
My assumption is that Cessna airspeed indicators are calibrated to account for this hole. It seems to calibrate the ASI on the ground one would need to be able to provide a constant pressure to the pitot which would obviously leak air out of the drain hole.
I know that by searching the archives on VAF there are a lot of people who are using Cessna Pitots. I just can't imagine that no one else has seen this problem. After searching the archives to see if the drain hole was an issue, I don't think anyone else has ever posted about this issue. This is the primary reason for my post -- to get in the archives to hopefully save someone else the trouble of all that debugging.
So, has anyone else seen this problem?
I called up a couple of salvage yards and found a good pitot off of a 1976 Skyhawk. I had read that the Gretz mount would work fine with this pitot so I bought it ($80.00!). A little filing and it fit perfectly.
Unfortunately, from my first flight I have been having IAS problems -- my IAS was typically 8 knots below where it should have been. I have two airspeed indicators (mechanical unit from Van's and my Dynon) and they read exactly the same airspeed. I did all of the usual debugging on this issue, including checking for static errors and pressure testing both pitot and static systems. In the course of my testing I found a small pitot leak on the back of my Dynon but that was easily remedied with the application of teflon tape to the threads. Alas, this still didn't fix my problem.
Since I had no pitot system leaks and no static position error or leaks it only left one thing -- an error with the pitot itself.
I borrowed a Gretz Pitot from a builder friend of mine (Steve Ashby, RV-8A builder, VAF forum member and one of the nicest guys you will ever meet) which fit right into my mast and flew it. Airspeed indication was definately up so I knew I was on the right track.
Back on the ground I re-installed my pitot. On the Cessna pitot there is a little drain hole on the bottom/back of the unit that allows the line to drain if the pitot freezes over (meaning that it will drop to 0 on the ASI). For my pressure testing I taped over this hole (obviously) but would remove the tape to go and fly.
Last night I decided to tape over that hole and fly. Voila...everything was perfect. I did 4-way GPS runs and entered the numbers into the GPS PEC spreadsheet (everyone should use this document for airspeed testing). My TAS on the Dynon was within 1 knot of the value calculated by the GPS PEC spreadsheet.
I will mix up some epoxy and plug that hole. Of all of the other heated pitots I have seen, none have a drain hole like the one on the Cessna pitot, so plugging that hole will give me the same safety level as those other pitots.
I had suspected the drain hole from the start, but everyone was telling me that couldn't be the problem. I should have gone with my instincts from the start.
My assumption is that Cessna airspeed indicators are calibrated to account for this hole. It seems to calibrate the ASI on the ground one would need to be able to provide a constant pressure to the pitot which would obviously leak air out of the drain hole.
I know that by searching the archives on VAF there are a lot of people who are using Cessna Pitots. I just can't imagine that no one else has seen this problem. After searching the archives to see if the drain hole was an issue, I don't think anyone else has ever posted about this issue. This is the primary reason for my post -- to get in the archives to hopefully save someone else the trouble of all that debugging.
So, has anyone else seen this problem?