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Old 04-29-2017, 06:01 AM
Tom Martin Tom Martin is offline
Join Date: Jan 2005
Location: Ontario, Canada
Posts: 1,392
Default RV14 wing tips

Typically I only install the wing tips after the wings are on the airplane and the flaps and ailerons have been rigged. This insures that the tips will match the ailerons.
I am curious to know how the tip alignment has worked out for those that have done the tips before installing the wings, as is called out in the plans?
Tom Martin RV1 pilot 4.6hours!
CPL & IFR rated
EVO F1 Rocket 1000 hours,
2010 SARL Rocket 100 race, average speed of 238.6 knots/274.6mph
RV4, RV7, RV10, two HRIIs and five F1 Rockets
RV14 Tail dragger flying #153

Fairlea Field
St.Thomas, Ontario Canada, CYQS
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Old 04-29-2017, 08:30 AM
JDA_BTR JDA_BTR is offline
Join Date: Dec 2013
Location: Baton Rouge, LA
Posts: 604

Same question... I was thinking that if the aileron alignment jig were cleco'd in place the alignment of the tip is based on that jig.... so go for it! I'm planning a hinged installation.
N1463 seems a good number....
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Old 04-29-2017, 08:54 AM
Larco Larco is online now
Join Date: Mar 2005
Location: DVT Phoenix
Posts: 1,054

I did a set some time ago on sawhorses and with the 14 aileron fixture in place it worked as well or better than a few other models done the plane
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Old 04-29-2017, 10:08 AM
n982sx n982sx is offline
Join Date: Apr 2010
Location: Chicago, IL
Posts: 256

Originally Posted by Tom Martin View Post
Typically I only install the wing tips after the wings are on the airplane and the flaps and ailerons have been rigged.
I'm about to put the wings on the airplane but I have already fitted, installed and trimmed the wing tips. With the rigging tool supplied with the wing kit, I am very confident that the wings can be rigged off the plane with very good alignment of the tips.

We'll see in a few weeks.
Bob Meyers

Built and Flying RV-14A N626KM SN 140093
Built and Flying Sonex N982SX
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Old 04-29-2017, 03:43 PM
Aussieflyer Aussieflyer is offline
Join Date: Jan 2015
Location: Redcliffe, Queensland, Australia
Posts: 52
Default Wing tips misaligned

I installed wing tips as per the plan. It made sense following the plans and uniformity should have resulted. However it did not happen, when I finally mounted the wings to the fuselage and fitted flaps and ailerons I discovered the port wing tip did not align with the aileron as required and was out by about 3/16th of an inch. This was enough to make the plane fly out of balance. I had to cut the wing tip open and re-glass it to effect the repair.

In hindsight I think it would have been better to have waited to final assembly of the wing to ensure the wing tips aligned.

Food for thought.

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Old 04-29-2017, 04:07 PM
TimO TimO is offline
Join Date: Feb 2005
Location: Wisconsin
Posts: 420

You should be able to install the wingtips and use the jig and rig the ailerons with the flaps on the wing cradle. You will most likely want the ailerons and wingtips both aligned with the flaps with the flaps in reflex position, and that can be determined by just mounting the flaps while on the wing cradles.
I would not spend the time to completely rig them on the cradle though. Rig them to a close approximation but then do the final rigging with everything assembled on the plane. You will need to have the stick (elevator) neutral when you rig the ailerons for the final rigging because the ailerons will change position slightly with nose-up/down stick movement. But since everything should line up with the flaps (assuming you don't have twist in your flaps) you can rig them on the cradle.

One thing to check...with the flaps mounted on the wing in the cradle, look at your rivet lines against the top wing skin. You can tell then if you have twist in the flaps. The question then is, how bad is the twist? With a lot of twist, you won't necessarily want to rig your ailerons and wingtips to the flaps. Use the jig to see what the proper position should be. If you're all straight, you should have the jig in place and flaps in reflex and it'll all line up pretty well.
Tim Olson - CFI
RV-10 N104CD - Flying 2/2006 - 1300+ hours
RV-14 N14YT - Flying 6/2016 - 285+ hours
RV-10/14 Transition Training:
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Old 04-29-2017, 07:37 PM
Tom Martin Tom Martin is offline
Join Date: Jan 2005
Location: Ontario, Canada
Posts: 1,392

Thank you all for the input. My flaps and ailerons are very straight, no issue there. However there is no way to "see" if the wings themselves are perfectly straight.
A slight twist in one with the opposite in the other and it will show up with the wing tips maybe matching one wing but not both wing tips matching the ailerons/flaps at the same time. The wings should be perfect but if they are off even a small amount it will show if the tips are set using only the aileron jig. The jig just measures the aileron relative to the last rib of the wing and as such is an excellent place to start when doing the final rigging.

I think I will trial fit the wings in my shop and set the system before moving to the hangar.

Thanks again, I will report back in a few weeks and let you know how it works out.
Tom Martin RV1 pilot 4.6hours!
CPL & IFR rated
EVO F1 Rocket 1000 hours,
2010 SARL Rocket 100 race, average speed of 238.6 knots/274.6mph
RV4, RV7, RV10, two HRIIs and five F1 Rockets
RV14 Tail dragger flying #153

Fairlea Field
St.Thomas, Ontario Canada, CYQS

Last edited by Tom Martin : 04-30-2017 at 01:49 AM.
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Old 04-30-2017, 11:55 AM
czechsix's Avatar
czechsix czechsix is offline
Join Date: Mar 2006
Location: Spring Hill, KS
Posts: 322
Default Careful with the jig...

I've just been through the wingtip fitting process in the past couple weeks. A while back I was told by Vans that the aileron jig in the early wing kits (I have s/n 140017) was wrong and has been corrected in later kits (don't know which s/n the change occurred in). Page 41-07 says:

"Step 6: With the control stick base in the "fully neutral" position, verify that the ailerons are approximately 1/16 [1.6 mm] above the trail position with respect to the wingtip trailing edges. NOTE: Newer revisions of the W-00026 Alignment Template will have a reflex ID hole as shown on Page 23-10, Figure 2. If the template does not have the reflex ID hole, use shims to rig the trailing edge of the Aileron to protrude approximately 1/16 [1.6 mm] to ABOVE the trailing edge of the template. The Ailerons must be in this slightly reflexed position to compensate for aerodynamic loads during flight."

It was not clear to me how to identify the "reflex ID hole" but I sent a picture of my template and was told I had the older version and I should therefore rig the TE of the aileron 1/16" above the template. So, with both wings in the cradle that's how I rigged the ailerons (by adjusting the pushrods such that the bellcrank and wing root torque tubes were all in the specified neutral positions).

After making all the adjustments I decided to install the flaps just to see how everything looked and it became obvious that the aileron alignment could not possibly be correct...the TE of the ailerons was about 3/16 to 1/4" higher than the flap TE, and the flaps cannot go any higher (the LE of the flaps hits the rear spar in the fully reflexed position). I started thinking that the instructions must be wrong and actually the TE of the aileron should be rigged 1/16" below the template as this would provide better alignment with the flaps. So I emailed Vans to ask and received this response:

"This is because of the new tool to align the 14 ailerons, which takes no account of the flap position, and makes no allowance for any variations in the flaps/ailerons. See attached RV-10 section 23-9 that achieved the same task with no tool, simply by aligning the aileron with the flap. Probably a simpler way to go, if you want the ailerons and flaps to align. Either way, a 1/8 up/down is no problem."

So, I tossed the template in the scrap bin and went about alignment in the following manner:

1) First I used my digital level to verify that with both flaps in the full up position, they both have the same relative angle between the top surface of the flap and the top surface of the wing (as measured along the straight section of the ribs that extends a dozen inches forward of the rear spar). I recall this being about 3 deg reflex angle, but the important part is that they are identical on both wings. One flap was about 0.2 deg different from the other, so I placed a shim between the rear spar and flap LE to make them the same.

2) Then I adjusted both ailerons (bellcrank-to-aileron pushrod) to align the aileron TE with the flap TE. I double checked the aileron-to-wing rib angles just like I did for the flaps to verify they are identical on both wings.

3) I then fit the wingtips with the wingtip TE in alignment with the aileron TE. On the left wing the tip aligned perfectly. The alignment of the right tip wasn't quite correct, so I fixed it by cutting the inboard half of the wingtip with my dremel tool and re-bonded it with a couple pieces of fiberglass inserted to fill in the gap created by the cut. Clamped the TE between two pieces of alum angle that were also clamped to the aileron to hold everything in alignment until it dried.

I'm pretty confident my TE surfaces are now well aligned with the basic wing structure. Hopefully the wing incidence will come out equal on both wings using the plans procedure for drilling the rear spar holes (I would have preferred the approach used on earlier RVs where you install the wings, carefully align everything, and then drill the rear spar attach holes to the fuselage with everything assembled as I have a higher degree of confidence in getting both wings exactly the same with that process).
Mark Navratil
Spring Hill, KS
RV-8A N2D #80583 - built/flew/sold
RV-14A #140017 - wings complete, empacone in progress...
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