|
-
POSTING RULES

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

02-18-2017, 06:57 AM
|
 |
|
|
Join Date: Jan 2005
Location: Charlottesville, Virginia
Posts: 1,227
|
|
Quote:
Originally Posted by tracy
Bob, I'm not that knowledgeable, but if you look at Vic's first picture, you will see that the end bolt either cuts or misses all together the longeron(where the #4 is) on the top side, which you can't see.
|
ok, I see it now.....took me awhile.
Plans call for 2 bolts each side, outermost bolt thru the longeron.
His top spar attach angle was not long enough so it had no edge distance for the bolt, so he removed top angle material to get a bolt into the longeron and thru bottom attach angle, then added a full piece spacer plate under the spar and an additional bolt.
So I can see the builder had a problem getting his parts to match the plans.
Then figured a way to compensate and carried on building.
I can see he had some logic to his plan. This logic may have been explained to his inspecting buddies to garner their approval or lack of intervention.
I am guessing the bottom line is there was most likely no engineering on this deviation from the plans and therefore unacceptable.
I am assuming the proper thing to have done was to somewhat disassemble the HS and remake the attach angle longer to get a proper fit. Then it would conform to plans and known engineering.
Knowing the build sequence and that this is a known close tolerance, seems like the plans would say to leave this part longer and maybe even notch the rib over it. Or maybe the plans do.....I need to check them today at the hangar. Thanks for posting this and making me continue to THINK.
__________________
Bob Martin
RV-6, 0-360 Hartzell C/S, Tip up, 1200+TT
James extended cowl/plenum, induction, -8VS and Rudder. TSFlightline hoses. Oregon Aero leather seats.
D100-KMD150-660-TT ADI2- AS air/oil seperator. Vetterman exhaust with turndown tips.
Louisa, Virginia KLKU N94TB
|

02-19-2017, 06:14 PM
|
|
|
|
Join Date: Nov 2014
Location: Plano, TX
Posts: 224
|
|
Quote:
Originally Posted by az_gila
Start with #40 holes and work up in several increments.
Measure and carefully mark the edge distances on both parts.
A needle file can adjust the location of the holes as you slowly increase the holes for the AN3 bolts.
That, and the rear spar wing bolts. were the two hardest critical holes to get correct on the -6.
|
To add to Gil's information if the edge distances between the angle bracket and the longeron do not line up (they don't overlap enough to give you sufficient edge distance on both) contact Van's. They have recommendations of how to build the area up based on the details.
Oliver
|

02-20-2017, 03:59 PM
|
 |
|
|
Join Date: May 2005
Location: Savannah, GA
Posts: 1,301
|
|
If it were me, I'd pass on it. Who knows how many other things are hidden, and fixing cracks could be a real hassle... and hopefully you'd find them in time.
As for resale value...
Ed
__________________
RV-9A at KSAV (Savannah, GA; dual G3X Touch with autopilot, GTN650, GTX330ES, GDL52 ADSB-In)
Previously RV-4, RV-8, RV-8A, AirCam, Cessna 175
ATP CFII PhD, so I have no excuses when I screw up
2020 dues slightly overpaid
Retired - "They used to pay me to be good, now I'm good for nothing."
|

02-20-2017, 06:02 PM
|
|
|
|
Join Date: Jan 2005
Location: Georgetown, TX
Posts: 396
|
|
Ed, exactly what we decided...
__________________
Deene Ogden.
N399AD RV-12...flying
N299AD RV8 QB, IO-390X, BA prop...SOLD
N199AD One Design...SOLD
N99AD BD4, flew for 22 years...SOLD
EAA Tech Counselor/Flight Advisor
CFII, MEI, CFIG
|

02-20-2017, 07:29 PM
|
|
|
|
Join Date: Feb 2012
Location: Trenton, SC
Posts: 173
|
|
Quote:
Originally Posted by vic syracuse
The pictures that Rob posted show a very common fix. It works and is approved by Van's. But don't hesitate to check with them for your particular situation.
Vic
|
Vic,
Just curious as to how YOU would fix this type of issue.
Would you:
A. drill out the top panel rivets and remake the attachment angles, redrill and
re-rivet the area or
B. perform the Vans approved fix.
Thanks for bringing this to light. I am facing this right now with my 6A.
__________________
Gene Mohr
Ret. US Army
RV6A (purchased), O360, Hartzell C/S prop
Trenton, SC (S17 homebase)
Happily Donated
|

02-21-2017, 04:58 AM
|
|
Super Moderator
|
|
Join Date: May 2005
Location: Locust Grove, GA
Posts: 2,624
|
|
Quote:
Originally Posted by gmohr
Vic,
Just curious as to how YOU would fix this type of issue.
Would you:
A. drill out the top panel rivets and remake the attachment angles, redrill and
re-rivet the area or
B. perform the Vans approved fix.
Thanks for bringing this to light. I am facing this right now with my 6A.
|
Either way works if you are carfeul. The problem with drilling out the rivets is that unless you are very careful and experienced, the holes could get wallowed out and may require the next size rivet. I certainly wouldn't hesitate to remove the tail and put it on a workbench to accomplish the task. It will make access much easier.
The trick to cleanly drilling out the rivets, especially in thicker material is to just drill off the head very carefully, and then use a punch ( a heavy duty center punch works real nicely) to "pound" out the shaft of the rivet. It will leave the hole intact, assuming it is a nice hole to begin with. Sometimes you will find that the reason for the crooked rivets is that the holes aren't drilled 90 degrees to the material or are already wallowed out.
Vic
__________________
 Vic Syracuse
Built RV-4, RV-6, 2-RV-10's, RV-7A, RV-8, Prescott Pusher, Kitfox Model II, Kitfox Speedster, Kitfox 7 Super Sport, Just Superstol, DAR, A&P/IA, EAA Tech Counselor/Flight Advisor, CFII-ASMEL/ASES
Kitplanes "Unairworthy" monthly feature
EAA Sport Aviation "Checkpoints" column
EAA Homebuilt Council Chair/member EAA BOD
Author "Pre-Buy Guide for Amateur-Built Aircraft"
www.Baselegaviation.com
|

02-23-2017, 12:29 PM
|
|
|
|
Join Date: Jun 2011
Location: Hope Valley, Rhode Island
Posts: 133
|
|
Quote:
Originally Posted by wirejock
I will be doing this soon. Any tips for getting it perfect?
|
Larry;
I just did mine recently and it came out good.
The key was carefully marking the edge distance limits for all pieces right there clearly on top-most surface where you can see them when you drill. That takes some ingenuity because the edges of the underlying longerons are hidden.
I used several measuring schemes to make sure that I had lines drawn that reflected both inboard and outboard edges of the longeron and checked them several times before center punching and drilling a small pilot hole.
It helped to use a 12 inch bit for that first hole, too. Better able to precisely locate it.
I also have an inexpensive endoscope that lets me see on my ipad the view from underneath-- Much more handy that just using an inspection mirror.
Hope this helps.
-Ivan
__________________
Ivan Luke
Hope Valley, RI
RV-7 SB
Just hung the engine!
2020 dues paid
|

02-26-2017, 08:28 PM
|
|
|
|
Join Date: Apr 2012
Location: Warrensburg, MO
Posts: 58
|
|
Checked mine today!
http://imgur.com/a/dVejP
I checked mine today, everything looks good to my untrained eye. Anybody see anything note worthy?
|

02-27-2017, 12:32 AM
|
|
|
|
Join Date: Apr 2008
Location: Lake Havasu City AZ
Posts: 2,390
|
|
Tail
Quote:
Originally Posted by TeamFAS
http://imgur.com/a/dVejP
I checked mine today, everything looks good to my untrained eye. Anybody see anything note worthy?
|
I'll take a pot shot at this: picture #1- notch for rivet in top of angle, likely not a problem.
#2 Right side angle at lower bolt MAY have a slight notch in angle. Left angle lower bolt edge distance appears to be less than others.
#3 Multiple mangled rivet heads but probably not unsafe. Some one didn't know how to hold the rivet gun OR did not have the proper gun.
Overall I give it a 7.0 as opposed to some zeros for some of the earlier posts.
|

02-27-2017, 09:10 AM
|
|
|
|
Join Date: Oct 2007
Location: Sacramento, CA
Posts: 3,343
|
|
The rivets on the elevator push rod is not what I have seen in the past. In a RV7, there are (I believe 8) that goes around and not in one row.
__________________
Mehrdad
N825SM RV7A - IO360M1B - SOLD
N825MS RV14A - IO390 - Flying
Dues paid
|
| Thread Tools |
Search this Thread |
|
|
|
| Display Modes |
Linear Mode
|
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 02:11 PM.
|