Saturday, October 17, 2015

24 SEP 15: Page 31-8 steps 7 (top skin), 12-3 1-4:  5 hours
Dimpled forward fuse top skin.  Jumped back to the empennage and fit the rudder fairings.  I wanted to make the lower fairing removable because of the aft position light, so I installed nutplates.  I used an aluminum backing strip in hopes that the nutplates do nut loosen in the future:
Took longer than expected, but I’m glad I did it.  Turned out nicely:

25 SEP 15: Page 12-3 1-4, 12-2 6-9:  5.5 hours
Finished the rudder fairings. Added the backing strip to the top fairing even though it isn’t removable.  Don’t think it was really necessary.  Both fairings installed:

26 SEP 15: Page 30-4 1-2, 9-15 8-9, 12-2 1-5, 29-18 2, 29-20 1:  11.25 hours
Bolted the steps into the fuselage.  Inside:
Outside:
Continued finishing the empanage control surfaces.  Installed the elevator counterweights:
Installed the elevator fairings:
Finished riveting the fuse side skins:
Installed the left cabin floor panel.  This took way longer and was more difficult than I had expected.  A huge hand workout pulling all those pop rivets!

27 SEP 15: Page 29-20 step 1, 29-21 step 2:  5.5 hours
Installed the right cabin floor panel.  Began to install the WD-1021-L/R-PC landing gear mounts – no pics.

28 SEP 15: Page 29-21 step 2:  3 hours
Finished installing the landing gear mounts.  Boy was this fun installing all the bolts in between the spars!  Nothing like leaving you mark – that’s some blood:

29 SEP 15: Page 29-22 step 1, 31-8 step 15:  3.5 hours
Riveted the F-1088-L/R forward fuselage ribs to the side skins.  I am SO glad to say that section 29 is now complete!!!!!!!!!!!!!!!!!  Riveted the F-1044B, D, E, and F angles and F-1044C spacer to the F-1044A forward fuse rib:

1 OCT 15: Page 38-2 step 1-5:  3.5 hours
Deburred the F-1052 brake pedals, cut four F-1097 spacers, match-drilled and deburred the pedals – no pics.

2 OCT 15: Page 38-4 steps 1-4, drill out tail cone rivets/prime:  4 hours
Cut and fit the F-6115 pedal bearing blocks to the F-1039B bearing block mount plates.  Bolted the blocks to the fuselage to test fit the pedals:
Everything lined up nicely:
So keeping the theme of going back to previous steps…I brought the tailcone back home from the hangar in prep for attaching to the fuse.  First I had to correct a little issue… Back when I was riveting the tail cone, I was only priming the interior of the skins.  After it was riveted together I primed the outside.  While priming, I noticed some plastic in the overlap of the top/side skin that I did not remove completely.  Not wanting to have the plastic in there, I had to drill out all of the rivets attaching the top skins to the longerons.  Didn’t take long:
You can see the unprimed seam.  In actuality, there was very little plastic stuck in the seam.  But any was too much, so I’m glad I fixed this issue:
Seam primed and ready to put back together:
 

3 OCT 15: Page 32-2 steps 1-4, rivet tailcone, VOR ant doubler, static ports:  6.75 hours
Final drilled the F-1006A/B/C bulkheads. Made a doubler for the VOR antenna under the tail.  Positioned the antenna over my dropped bucking bar ding (you can see a smaller one just forward of the antenna):
Placing the rivet holes in the doubler:
Test fit – looks good:
Outside placement looks good:
Scuffed the inside of the tailcone for the static ports:
Prosealed up:
Inserted and taped until cured:
 Outside:

4 OCT 15: Page 32-2 steps 5-8, 32-3 steps 1-4, 32-4 1-8:  9 hours
Dimpled the F-1006 A/B/C bulkheads.  Clecoed and match-drilled the tailcone to the fuse.  Fuse is now just about the length of the garage.  Probably will have to go diagonally when it comes time to hang the engine:
Match-drilling the bottom of the tailcone to the fuse:

5 OCT 15: Page 32-5 steps 1-9:  3.75 hours
Dimpled the holes in the tailcone, bulkhead, fuse skin joints.  Riveted nutplates to the flange on the F-1006B bulkhead.  Riveted the F-1006 A/B/C bulkheads together – no pics.

6 OCT 15: Wire run tabs:  1.25 hours
Made some tabs to eventually install inside the fuse/for wire runs.  Will probably proseal them in place:

7 OCT 15: Page 32-5 steps 10-11, re-rivet tailcone:  3 hours
Riveted the F-1006B bulkhead to the F-1029 bell crank ribs, re-riveted the tailcone top skin, and clecoed the tailcone to the fuselage – no pics.

12 OCT 15: Page 32-5 steps 12-16, 34-3 steps 1-4, 34-4 1-2:  4 hours
Started riveting the tailcone to the fuse:
Marked and cut the hinge for the baggage door, deburred the door parts, and countersunk the holes in the door hinge.  Marking the rivet holes in the door hinge:

14 OCT 15: Page 33-2 steps 1-10, 33-3 steps 2-9:  4 hours
Match-drilled rear seat floors and baggage floors.  Floors installed:
Drilling the F-1027 close out panel into the baggage floor:

15 OCT 15: Page 33-4 steps 2&6, drilled holes for conduit through bulkheads:  1 hour
Removed floor panels and final-drilled #40 the holes in the aft flange of the baggage floors – no pics.

16 OCT 15: Page 33-4 steps 3-5:  1 hour
Final-drilled the stiffeners to the baggage floors – no pics.

17 OCT 15: Page 33-4 step 6, step access panels:  3.5 hours
Cut access panel holes in each baggage floor over the steps:

Finished deburring all the parts.  Finally have a pile ready for priming – means I’ll soon be riveting structure together again!

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