Hans,
Excellent work. The approach was well thought out. Curious though, did the test aircraft have the new teflon conduits? I am planning to change the conduits in my '65 260 in mid June. The same test procedure should produce good data regarding the benefits of new conduits vs. the originals in my airplane. I have less than 25 hours on a complete gear overhaul per the 1000hr AD so I believe my airplane is as close to "nominal" as you can get.
Would it be possible to borrow the same test apparatus for a before and after comparison of gear/transmission loads relative to new style conduits?
Chris
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Gear Retraction Load Test Results
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Gear Retraction Load Test Results
by Hansmeister » Mon Apr 20, 2009 1:15 am
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Comanche Gear Motor Load Tests.doc- (5.12 MiB) Downloaded 272 times
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Hansmeister - ICS member
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Zach Grant L1011jock - Technical Advisor
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by Hansmeister » Mon Apr 20, 2009 5:15 am
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by JIMICS2452 » Mon Apr 20, 2009 1:26 pm
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by JIMICS2452 » Mon Apr 20, 2009 1:27 pm
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JIMICS2452 - ICS member
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Zach Grant L1011jock - Technical Advisor
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by Chris Kuyoth » Wed Apr 29, 2009 8:15 pm
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by Hansmeister » Thu Apr 30, 2009 2:39 am
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by Chris Kuyoth » Thu May 28, 2009 2:30 pm
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by Hansmeister » Thu May 28, 2009 6:55 pm
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by Chris Kuyoth » Fri May 29, 2009 2:10 pm
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by Chris Kuyoth » Wed Jun 03, 2009 4:17 pm
Hans,
Just wanted to confirm that you were able to send the jack and attachment fixtures. I am hoping to start the project this weekend.
Thanks,
Chris
Just wanted to confirm that you were able to send the jack and attachment fixtures. I am hoping to start the project this weekend.
Thanks,
Chris
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by Hansmeister » Wed Jun 03, 2009 5:43 pm
It's been sitting in my truck. I've been very busy trying to finish a technical report. It will go out today.
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by Hansmeister » Thu Jun 04, 2009 1:19 am
Cris, the box went out today via FedEx Ground.
Your tracking number is 468810710088188.
Your tracking number is 468810710088188.
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