Category Archives: Section 12, Empennage Fairings

Control System (2)

Previous posts described the rudder cables installation.  Here the final tabs were measured and installed.

Here are photos of the rudder pedal linkages and the rudder attachment.

 

 

 

 

Fairings were added to the cables outlet locations for added strength and a touch of streamlining.

 

 

 

 

EMPENNAGE FAIRINGS

Experience from other builders indicate the holes tapped in the longeron for the #6 screws holding the empennage fairings will eventually strip out from taking on and off.  While the tail section has not been completely sealed and the access was relatively easy, I added Click-Bond nutplates.

Empennage Attach (5) and Empennage Fairings (7)

Attachment of the horizontal stabilizer enabled the final configuration of the elevator control rods and elevator stops.

Match drilling the forward spar shims and aft bracket were performed to mount the horizontal stabilizer.  The UP position of 30 degrees exactly matches specification. The DOWN angle, even after considerable filing of the stop bracket, was finalized about a degree shy of the expected 25 degrees.

 

 

These pictures show the vertical stabilizer forward and aft attachments after the elevators were removed. Two mounting shims under each forward HS spar attach pad were also match drilled and bolted on before VS install.

 

 

The empennage gap cover under the HS was clecoed into place. The rear section overlaps the inspection port cover.  Both are match drilled together through the longeron.

 

 

 

The plans call for only three screws per side to hold the forward section of the empennage fairing.  Many pilots have suggested additional fasteners to prevent fiberglass bulging due to air stream pressure over the fuselage. Here intermediate points were drilled midway between the default points. Nutplates for #6 screws will later be added to the upper aft skin.

 

 

Front and rear photos of the match drill screw points on the empennage fairing. The aft points require special care when trimming to not interfere with either the elevator horn or the rudder motions.

 

 

With the main empennage components staged in place, the whole fuselage begins to look like an airplane.

 

 

 

 

OCTOBER 2020 UPDATE

Further trimming and edge preparation has been completed on the fiberglass empennage prior to priming.

Edges were measured against a scribe line formed into the part. Enough ‘meat’ needed to remain for the attachment screws to have sufficient structure to hold properly.

 

 

 

Because of the extra holes added, smooth curves based on circular patterns were applied.  Since fiberglass always seems to have numerous pinholes from the manufacturing process, a coat of Smooth Prime helps with initial underlayment.

 

 

 

MISCELLANEOUS

The forward and aft NACA air vents were fastened with ProSeal and #4 stainless screws into position.  Later SuperFil will be applied to smooth out the backing plate rivets.

Empennage Fairings (6)

The tedious work of sanding, fitting, aligning, and build-up continue on the fiberglass tips for the elevator and horizontal stabilizer.  The nice part about fiberglass is you can add or subtract material as desired.  The down side is having to wait at least 24 hours between operations.

Here is a case of trying to level the HS tips, then fill as needed with resin/glass beads (white) or Awl Grip fairing compound (pink).  The same operations apply to the elevatore tips.  Sand, fit, fill, rinse, repeat…

 

 

 

The left shows backing washers clecoed for superglue attachment to the elevator tips. These are not required, as these holes are supposed to be countersunk, then pop riveted onto the elevator.  However, experience has shown the fiberglass gets very thin after the countersink operation, so this attempt should reinforce the connection.

 

 

… and while waiting for the next round 0f build-up to cure, I started adding the nutplates to the horizontal stabilizer.  Eventually these will fasten a custom fairing which sits between the horizontal and vertical stabilizers.

Empennage Fairings (5)

Work on the vertical stabilizer and rudder fairings was recently completed – at least for the time being and until final preparations for paint are underway.

My overall satisfaction level is good with the overall fit, gaps and blending of skins to fairings.

 

 

 

 

The upper and lower elements are clecoed in position to check the final rudder angles, gap tolerance on the upper rudder swing and rudder/vs skin clearance.  All within tolerance and acceptable for now.

 

 

 

The next fairings to be addressed are on the horizontal stabilizer.  To properly fit these, Section 11 Tailcone Attach elements must first be completed.  The elevators are fastened to the rod end bearings of the HS, then angles and clearances checked for free movement.

adfa

 

Here the HS cradles in the jig built many moons ago with the original construction.  The elevators are in position to begin work on the fairing alignment.

 

 

 

Close-ups of the gap between elevator tips and horizontal stabilizer, then the rod end bearding and the hinges.

 

 

 

 

Initial fiberglass filling of the HS end caps after rough trimming to shape with the elevator tips.  These are not straight – bending backwards at an 8degree angle. This is enough to  prevent the fiberglass molding from being simple.

 

Empennage Fairings (4)

More sanding, fitting and filler on the fiberglass parts. Plus the addition of nut plates at various locations to complete some of the parts.

This photo shows the lower rudder fairing with #6 nut plates soft riveted into place. I made this fairing removable, as the AeroLED Suntail nav/strobe light wiring and electonics still needs to be added. A machined spacer from Cleaveland Tools provides a stable surface for fastening the Suntail afterwards.

 

 

 

Final filler and smoothing on the bottom rudder skins.  These parts hold the bottom fairing.

 

 

 

 

Nut plates for #6 screws are also install on the vertical stabilizer top.  These will allow removal of the top to access the VOR bracket made earlier.

 

 

 

The bottom of the vertical stabilizer skins also takes #6 nut plates.  These holes will later be used to fasten the fairing which bridges  between the vertical and horizontal stabilizers.

 

 

 

Empennage Fairings (3)

This week was about sanding and fitting the rudder top and bottom fairings.

This shows the top fairing pop-riveted into position on the rudder.  The end cap with the lead counter-weight needed some additional material to match well with the VS top.

 

 

 

 

Plastic electrical tape is applied to keep the resin off unwanted parts.  Then the end cap is sanded and cleaned for fiberglass layers.  These are probably not necessary, but I wanted to ensure the overlapping metal parts are held rigidly in place (should help prevent cracking along the seam)

 

 

 

Multiple layers of fiberglass and resin are applied. Because the resin is quite fluid at the start, some droops down the lower face.  This will later be sanded smooth and covered with Awl Grip D8200 for the final finish.

 

 

 

The basement shop was also enhanced with a new single stage, 12.8cfm air compressor made in USA by Quincy. Next steps are get the electrician to wire a dedicated circuit, then fire up for plane building usage.

Empennage Fairings (2)

Further fitting the VS top and rudder bottom fairing were the activity for this week.

 

The VS top fairing did not fit properly in the metal opening.  Throughout this build I have found all the fiberglass parts to only be approximations, much work on proper alignment and sizing has been needed.   Here the rear profile is being sanded to shape and the back panel straightened to match the rudder top fairing.

 

 

The AeroLED Suntail NAV/strobe will be attached to the lower rudder fairing via a machined aluminum spacer purchased from Cleaveland Tool.  The fiberglass from the fairing at this point is fairly thin, so fabricating a backing plate for the six pull rivets was chosen. This photo shows interim progress.

Empennage Fairings (1)

After months of inactivity due to the new house move I am finally back to working on plane parts.

Moving day!  Here are photos for relocating many plane parts from the rented storage unit to my new basement workshop.  Outside temperatures this time of year are in the mid-90’s.  The basement has a dehumidifier with temperatures in the low-70s, humidity around 40% – perfect working conditions.

 

 

First action in the new shop was build a jig for the vertical stabilizer and bolt down to the workbenches.

 

 

 

The fiberglass part needs to cover the NAV antenna holder with enough space for easy assembly. These show the initial fitting, plus the bend antenna rods in position.  Nice.

 

 

 

Eric helps install the rudder linkages, then rough fit to the vertical stabilizer.  This was a provisional attachment to check fit/finish. Adjustments to the flex angles and VS skins are needed.

 

 

 

Fiberglass caps on the rudder top and bottom are next on the TO_DO list, plus finish filling the VS cap piece.