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rv9jim(at)juno.com Guest
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Posted: Mon Feb 04, 2008 12:55 pm Post subject: Pitot leak check |
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I am doing the leak check on my pitot system. What are the usual guide
lines. Right now, I have a leak down at this rate: 50K to 45K in
+2 min. 110K to 105K in 50 sec. The only joints left are the screw on
nuts at both of my air speed indicators.
Jim Nelson
N15JN
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recapen(at)earthlink.net Guest
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Posted: Mon Feb 04, 2008 1:10 pm Post subject: Pitot leak check |
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I remember hearing that you are 'allowed' 100'/min on your static system.
I don't recall hearing anything on the pitot system.
Have you tried the ASI's independantly of each other? One of them may be bad....it has happened......
I'll be monitoring this thread as I am interested too....
--
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rv9jim(at)juno.com Guest
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Posted: Mon Feb 04, 2008 2:05 pm Post subject: Pitot leak check |
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Yup, I'll need to make a close off fitting to do that. I think I will
do the Teflon grease on the tubing first and see how it does.
Jim
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s.hamer(at)verizon.net Guest
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Posted: Mon Feb 04, 2008 4:38 pm Post subject: Pitot leak check |
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Jim,
Look in AC 43.13 if you have a copy. It's all in there. My book is at the
hangar and I don't want to rely on my memory to give you the info.
Steve Hamer
RV-6
Apple Valley, Ca
Quote: |
I am doing the leak check on my pitot system. What are the usual guide
lines. Right now, I have a leak down at this rate: 50K to 45K in
+2 min. 110K to 105K in 50 sec. The only joints left are the screw on
nuts at both of my air speed indicators.
Jim Nelson
N15JN
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rvreynolds(at)macs.net Guest
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Posted: Mon Feb 04, 2008 5:11 pm Post subject: Pitot leak check |
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The pitot/static system tests are covered in FAR/AMT (Aviation Maintenance Technicians). The FAR/AMT is a good book to have and is available from Spruce, Sporties, etc.
FAR PART 23.1325(b)(2)(i) - Static Pressure System (Leak Test)
FAR APPENDIX E to PART 43 - Altimeter System Test and Inspection
These test are normally done by the avionic shop that "certifies" your transponder but you will save boo coos of money if you have a leak tight system before you go to the shop..
In accordance with FAR PART 23.1325(b)(2)(i), conducted proof test demonstrating the integrity of the static pressure system. At 1000 ft above airport elevation, The leakage was ----- ft in 1 minute. The requirement is less than 100 ft in 1 minute.
Be very careful in applying pressure or vacuum to your system. You can damage your instruments!
Richard Reynolds
Norfolk, VA
RV-6A 430 hrs.
On Feb 4, 2008, at 3:49 PM, James H Nelson wrote:
[quote]--> RV-List message posted by: James H Nelson <rv9jim(at)juno.com (rv9jim(at)juno.com)>
I am doing the leak check on my pitot system. What are the usual guide
lines. Right now, I have a leak down at this rate: 50K to 45K in
+2 min. 110K to 105K in 50 sec. The only joints left are the screw on
nuts at both of my air speed indicators.
Jim Nelson
N15JN
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Kellym
Joined: 10 Jan 2006 Posts: 1705 Location: Sun Lakes AZ
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Posted: Mon Feb 04, 2008 6:47 pm Post subject: Pitot leak check |
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Only specs for altimeter and static system, not pitot, at least if you
are referring to Appendix E.
S Hamer wrote:
Quote: |
Jim,
Look in AC 43.13 if you have a copy. It's all in there. My book is
at the hangar and I don't want to rely on my memory to give you the info.
Steve Hamer
RV-6
Apple Valley, Ca
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_________________ Kelly McMullen
A&P/IA, EAA Tech Counselor # 5286
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