24th October 2010

Activation energy: drilled rear spars

Hours: 2.8 | Posted in Wing & Tail Joins

No work on the project for nearly a month, though it’s been near in thought.  Times have been busy at work pushing toward completion of a complete remodel of our audio production studios, and life has happened in other areas, as well.  In the meantime, Vertical Power shipped me the new blank box for the VP-X Pro (the other one is on the way back), and I bought some vise-grip clamps for drilling the rear spars.  That’s about the entire progress that was made on the project; the upside is that the credit card bill this month will be gloriously small.

Tonight I pushed over the next hurdle, hoping that things will mellow a bit for at least a few weeks and allow some work time…the engine and interior should be coming early next month, and the icy season is dead ahead, so I need to get the wings off and restore some garage parking.

After checking the fuselage for level fore-aft and laterally, I trimmed a block of hardwood to a bit larger than the spacer required for finding the wing incidence, and fine-tuned it’s length with the disc sander.  With the block of wood securely taped to a 4′ level at the correct distance from the end, and a bucking bar taped at the far end to hold it on the wing, I was ready.  Setting the wing incidence was easy; both were very close to start with, requiring only a small adjustment upward, and a push to be sure the rear spar was fully seated in the “hand” of the fuselage.  Clamped down and measured in several locations along the wing, then marked the infamous 5/8″ edge distance on the spar stubs (a piece of scrap filed to 5/8″ made marking easy…I actually cheated for extra safety margin and used a 21/32″ strip, and the width of the marker line made it more like 11/16″…).

Setting wing incidence Double levels for accuracy check

Satisfied with the rigging, I test-fit the flaps as suggested by Van’s in their incidence drilling guide.  Both flaps required filing off a small portion of the inboard nose skin to clear the spar stub for full retraction, but the bottom skin tucked nicely against the fuselage bottom.  Flaps off, I went in and re-read the drilling guide from Van’s.  A couple more measurements, and it’s time to get on with the drilling.  “Nothin’ to it but to do it,” as they say.

The actual deed was done easily.  A long #30 bit and a drill guide made from a block of oak set the pilot holes in the center of the edge-distance box.  Stepped up the holes with a series of drills to final size: #30, #20, #10, .250, .295, then the .3115 reamer for final fit on the AN5 bolt.  A touch of deburring and in went the bolts.  Done.

Left wing margin box Right wing margin box

Left wing drilled Right wing drilled

Left wing temporary bolted Right wing temporary bolted

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