10 MAY 14: Page 10-2 steps 2-6, page 10-3 steps 1-5: 5.5 hours

Deburred the F-1012A&B fuselage bulkheads, clecoed together, and matchdrilled the 3/32 holes of the bulkhead and the tie down bar:

Made the F-1011E ruder cable angle, match-drilled the nutplate rivet holes into the F-1011E , machine countersunk the rivet holes in the angle:

Straightened the two F-1011C horizontal stabilizer attachment bars:

Final drilled holes in common to the attachment bars and bulkhead, match-drilled the holes of the bulkhead and the F-1011A bulkhead stiffener, match-drilled the holes of the bulkhead and the F-1011E rudder cable angle:

11 MAY 14: Page 10-4 steps 1-5, page 10-5 steps 1-4: 8 hours

Made the F-1010A horizontal stabilizer attachment angle.  Separated the F-1010C bulkhead doublers into left and right parts.  Deburred the F-1010 bulkhead and cleacoed the F-1010C-L/R bulkhead doublers.  Match-drilled the holes in the bulkhead and the bulkhead doublers into the F-1010A angle.  Final-drilled the remaining holes common between the F-1010 bulkhead and the F-1010C-L/R doublers:

Deburred and final-drilled the F-1008, F-1007, and F1006 frames:

Spent the rest of the session finishing all the F-1047 fuselage stiffeners – 12 in all:

Between all the stiffeners and all the bulkhead parts, it was a boring, but productive day.  Not too many pics, just a bunch of parts: