Showing posts with label Section 41-Wing Attachment. Show all posts
Showing posts with label Section 41-Wing Attachment. Show all posts

Monday, June 21, 2021

Finishing, Wing Attachment (Part 4)

In Part 3, all 18 of the F-14122 Root Fairing Stiffeners were prepared.  Today, we prepared the two Upper and two Lower Wing Root Fairings.  The work on these fairings was pretty straight forward, so I didn’t included any pictures of the preparation…..just the finished product.

The Fairings themselves had the edges cleaned, holes final-drilled #17, appropriate holes dimpled for #6 screws, treated with Alumiprep, treated with Alodine and sprayed with Akzo primer.  The nine Stiffeners for each Fairing were of various lengths, so they only fit in one location.  I could have back riveted the Stiffeners to the Fairings, but I decided to squeeze them with the pneumatic squeezer.  Either method would have worked fine.  Here are the completed F-14188A-L (top) & -R (bottom) Upper Wing Root Fairings.  You can see all 18 Stiffeners have been riveted into place and the appropriate holes have been dimpled.

These are the F-14118A-L (top) & -R (bottom) Lower Wing Root Fairings.  For preparation purposes, these two Fairings were prepared the same way as the Upper Fairings with one additional step.  You can see the forward portion of the Fairings are bent upward.  The plans tell you to mark two tangent lines onto the top side of the Fairings.  One line was 6 3/8” and the other was 8 7/8” from the forward edge of the Fairing.  The Fairings now had to be bent around a piece of tubing.  (I used a spare piece of tubing from an Aileron counterweight that I secured in a bench vice …..worked perfectly).  You place the rear tangent line on the top center of the tubing and bend the Fairing downward around the tubing until the forward tangent line touches the tubing on the bottom side.  Sound complicated?  It wasn’t!  We had to tweak the bend a few times to match the airplane, but it work out pretty nicely.  The plans do a very good job of explaining the process.  Here are the two completed Fairings.  The hole in the center of each fairing will be for the fuel vent line to go through.

Here is a little closer look at the bends we made on the Fairings.  Very happy with how they came out.


Backing up just a little bit…..prior to dimpling the holes in the Lower Root Fairings, they had to be used to mark the installation locations of the K1100-08 nutplates (circled in the two pictures below).  The first picture is the right side installation and the second picture is the left side.  The two Root Fairing Attach Angles (angles the nutplates are riveted on) did not have any prepunched holes in the bottom portion of the angle.  These holes were made by match-drilling the corresponding hole locations in the Lower Root Fairings.  After these holes were drilled (which will be where the screw passes through to the nutplate) you can use one of the nutplates to match-drill the nutplate attach holes.  Pretty easy process that was been used throughout the airplane on several occasions.



Lastly, the two F-1099C Wing Walk Spacers were installed as shown in the two pictures below.  The plans instruct you to scuff the lower surface of the Spacer and its bonding location on the upper surface of the Main Spar Assembly.  I initially used grey Scotchbrite and finished up with 80 grit sandpaper.  The plans tell you to use proseal to bond the Spacer, but I didn’t have any available.  So, I used RTV adhesive for the bonding.  I applied the adhesive to the Spacer, used a popsicle stick to smooth the adhesive evenly on the surface, pressed the Spacer into position, and wiped away the excess that oozed out the sides…..done!  Looks pretty good to me.


Tuesday, June 15, 2021

Finishing, Wing Attachment (Part 3)

This work session was completed on June 3, 2021.

Attaching the Wings is a BIG deal.....and a heavy one!  So, my Uncle from Atlanta came down to help.  He has said since he started helping that he wanted to be here for this milestone.....and he was!  Thanks Uncle Jim!

We installed the left Wing first and I forgot to start the camera (remembered for the right Wing install.....see below).  We initially used the two work tables to support the Wing next to the Fuselage.  The tables turned out to be about 4 inches to high.  So we ended up putting both tables together near the outboard end of the Wing and a plastic trash can near the inboard end.  As the plans instructed, we lubricated the mating surfaces of the Main Spar Assembly and Bulkhead Assemblies with Boelube to ease installation.  Once the Main Spar Assembly was inside the Bulkhead Assemblies, we lined up the holes and inserted two drift pins (previously fabricated) in the lower inboard hole and upper outboard hole.  With the drift pins inserted, the Wing was “stable” enough to remove the trash can.  Then, my Uncle inserted all nine bolts as I gently rocked the Wing up/down/fore/aft to aid in the installation of the bolts.

The four larger NAS1309-58 bolts (two on top and two on bottom) were installed first.
The four smaller NAS1306-58 (two on top and two on bottom) were installed second.
The single AN6-11 was installed last to secure the Rear Spar Assembly to the Bulkhead Bars

All the shanks of the bolts were lightly lubricated with LPS #1 (but not the threads.....the plans state doing so can result in incorrect torque values) prior to installation.  Each of the bolts had to be lightly tapped into place using a hard plastic hammer.  After all the bolts and associated hardware was installed, they all got fully torqued in the order they were installed.  The picture below shows the left Wing fully installed to the Fuselage.

In this view, you can see the heads of the eight bolts installed between the Main Spar Assembly and the Bulkhead Assemblies.

Not the best picture, but you can see a couple of the nuts attached here to the bolts.

Just another view of the attached left Wing.

The right Wing was installed in the same manner as the left Wing.  Although this is a time lapse video, you can still see how we used the tables and trash can to aid in the Wing installation.  Using the trash can was money!

Here is the completed right Wing installation.

Such a big milestone, I took several additional pictures.




Saturday, June 12, 2021

Finishing, Wing Attachment (Part 2)

This work session was completed on November 25, 2020.

These are the F-14122A Root Fairing Stiffeners (left column for the left side and right column for the right side).  They came from Van’s in two long strip and each Stiffener had to be separated and “shaped”.  These are the completed Stiffeners after being separated, “shaped” and dimpled.....

.....and after being treated with Alumiprep, Alodine and Akzo Primer.  They are now ready for installation.

Finishing, Wing Attachment (Part 1)


This work session was completed June 2, 2021.

The first step in this section is to fabricate some two Flap Pushrods Assemblies.  To start, the VA-256 Flap Pushrod had to be trimmed to 3 1/2” (88.9 mm).  The center section below is the part that will be used for the actual Pushrod.

These are the parts that’s will make up the assembly:  
VA-256 Flap Pushrod (x2)
CM-4M Rod End Bearings (x2)
AN316-4R Jam Nuts (x4)

The Pushrods were then treated with Alumiprep, Alodine, sprayed with Akzo primer, assembled and installed on/in the Flaps.  Here is the final product: