|
-
POSTING RULES

-
Donate yearly (please).
-
Advertise in here!
-
Today's Posts
|
Insert Pics
|

08-10-2013, 03:06 PM
|
 |
|
|
Join Date: Jul 2009
Location: Mojave
Posts: 4,642
|
|
Help! Wrong Hinges On Rudder ?
Based on the problems with the elevators last flight, this morning I removed the rudder to lube/inspect. Found two GMM-3M-670 rod ends and one -670. This can't be right according to plans, right? The -680's were barely hanging on with only 3 threads engaged in the nutplate!  At least the jam nuts were tight.
So, assuming this is NOT according to plans, where are the shorter -670's used so I can go hunt for my two missing -680's?
Otherwise, I'm ordering a new set from Spruce.
Thanks
__________________
WARNING! Incorrect design and/or fabrication of aircraft and/or components may result in injury or death. Information presented in this post is based on my own experience - Reader has sole responsibility for determining accuracy or suitability for use.
Michael Robinson
______________
Harmon Rocket II -SDS EFI
RV-8 - SDS CPI
1940 Taylorcraft BL-65
1984 L39C
|

08-10-2013, 05:21 PM
|
 |
|
|
Join Date: Mar 2005
Location: DVT Phoenix
Posts: 1,187
|
|
From my experience. What you have is correct. Sometimes it is noticed that the vertical is not trimmed enough forward at the top so the bearings in the rudder are not installed in as far in as they should be. The bottom bearing is longer so to accommodate the rudder horn. Some builders have installed the longer bearings in the top and center because of the issue you have come up against. Larry
|

08-10-2013, 05:31 PM
|
|
|
|
Join Date: Oct 2012
Location: Tellico Plains, TN
Posts: 12
|
|
I just finished the rudder on my RV-7. DWG-7 calls out MD3614M rod end bearing for the top 2, and a larger MD3616M at the bottom. At each location there is a unique spar web-to-bolt-center dimension. You need a set of plans to determine the proper rigging. I don't know the details of your RV-8, but I wouldn't be concerned about different hardware in different locations.
|

08-10-2013, 07:10 PM
|
 |
|
|
Join Date: Jul 2009
Location: Mojave
Posts: 4,642
|
|
OK, weird.
However, these top hinges are only catching a few threads and that is a major problem in my book. Going to have to look at this more carefully, because there is not much room to bring the rudder forward. Certainly not enough to get the threads fully engaged, anyway.
Thanks much for the heads up!
__________________
WARNING! Incorrect design and/or fabrication of aircraft and/or components may result in injury or death. Information presented in this post is based on my own experience - Reader has sole responsibility for determining accuracy or suitability for use.
Michael Robinson
______________
Harmon Rocket II -SDS EFI
RV-8 - SDS CPI
1940 Taylorcraft BL-65
1984 L39C
|

08-11-2013, 12:15 AM
|
|
|
|
Join Date: Apr 2011
Location: SF East Bay
Posts: 852
|
|
Quote:
Originally Posted by larharris2
I just finished the rudder on my RV-7. DWG-7 calls out MD3614M rod end bearing for the top 2, and a larger MD3616M at the bottom. At each location there is a unique spar web-to-bolt-center dimension. You need a set of plans to determine the proper rigging. I don't know the details of your RV-8, but I wouldn't be concerned about different hardware in different locations.
|
Just for a data point. My 8 plans show the same set up. 14s for the top and middle and 16 for the bottom.
__________________
Sam
RV-8 with the Showplanes Fastback conversion
Emp completed except for glass work
Wings completed except for bottom skin and glass work
Fuselage underway
N18451 reserved
|

08-11-2013, 06:19 AM
|
|
|
|
Join Date: Feb 2005
Location: Chesterfield, Missouri
Posts: 4,514
|
|
Quote:
Originally Posted by Toobuilder
OK, weird.
However, these top hinges are only catching a few threads and that is a major problem in my book. Going to have to look at this more carefully, because there is not much room to bring the rudder forward. Certainly not enough to get the threads fully engaged, anyway.
Thanks much for the heads up!
|
Each is set at a specific distance from the attach bulkhead. I made a couple wood jigs with a bolt inserted in a hole to get them near that distance. Later today I will find that specification if you need it.
__________________
RV-12 Build Helper
RV-7A...Sold #70374
The RV-8...Sold #83261
I'm in, dues paid 2019 This place is worth it!
|

08-11-2013, 07:55 AM
|
 |
|
|
Join Date: Jul 2009
Location: Mojave
Posts: 4,642
|
|
I'm at a disadvantage without plans, but is there any reason why the longer rod ends are not used on the top? Is there some structure aft of the rudder spar that the longer shank would interfere with? In other words, if you had say a half inch of thread protrusion through the nut plate, would that be bad (aside from dead weight)?
__________________
WARNING! Incorrect design and/or fabrication of aircraft and/or components may result in injury or death. Information presented in this post is based on my own experience - Reader has sole responsibility for determining accuracy or suitability for use.
Michael Robinson
______________
Harmon Rocket II -SDS EFI
RV-8 - SDS CPI
1940 Taylorcraft BL-65
1984 L39C
|

08-11-2013, 08:09 AM
|
 |
|
|
Join Date: Mar 2005
Location: DVT Phoenix
Posts: 1,187
|
|
I recommend getting and having plans on hand so that the issues that come up can be addressed properly. If the parts are assembled per plans and the correct measurements are obtained from the plans, the supplied parts should work just fine. I have and others as well have seen your scenario pertaining to the rod end bearings way to many times. Please get a copy of the plans and go from there and maybe ask a seasoned builder to look it over. :-) Larry
|

08-11-2013, 09:19 AM
|
 |
|
|
Join Date: Nov 2012
Location: Half Moon Bay, CA
Posts: 1,031
|
|
FWIW ... I put those rod end bearings in my -7 rudder a few months ago and I had to run them in until the threads were nearly invisible to make the dimensions called out in the plans. I only had to tighten the jam nut a turn or two to lock it down.
__________________
Bill Bencze
N430WB RV-7 #74152 @ KHAF, tip-up; IO-360-M1B; Hartzell CS. !! Phase 1 !!
2357 hrs over 8.5 years to get to flying. Log at: http://rv7.wbencze.com
VAF 2020 donation happily made
Last edited by wjb : 08-13-2013 at 01:03 AM.
|

08-11-2013, 09:25 AM
|
|
|
|
Join Date: Mar 2006
Location: Kyle, TX
Posts: 566
|
|
Rod End Bearing Length
If you feel uncomfortable with how many threads are engaged, I recommend purchasing a couple of the longer ones and simply replacing them. It's a small price to pay for "peace of mind" don't you think?
Good luck.
__________________
Fred Magare
GySgt, USMC (Ret.)
PP-ASEL, A&P
Frederic.magare "at" gmail.com
 RV-9A Firewall Forward
[Engine purchased]
|
Posting Rules
|
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts
HTML code is Off
|
|
|
All times are GMT -6. The time now is 02:29 PM.
|