Log Entries - October 2003

DateChapterDescriptionHours
Wed 1 13 Fiddled with resevoir installtion - ready to be floxed into place. Cleaned up cylinder mount - ready to flox. Figured out pitot placement. 1
Wed 1 19 Cleaned up edges of top layup. 1
Thu 2 19 Sanding foam in wing ribs. 3
Tue 7 19 Finished shaping inboard wing root. Bonded level board to wing top. Sanded trailing edge straight. Removed wing from jigs. Removed jigs from table. 3
Thu 9 19 Fitting left wing cores into jigs. 3
Sun 12 19 Glued traling edge cores of left wing. 2
Sun 12 16 Began cutting parts for control system. 2
Wed 15 16 Cut all the non-Brock schedule B parts. 2
Sat 18 16 Layed out all the parts and hardware, figuring out where everything went and what was missing. 3
Sun 19 16 Began assembly of pushrod parts. 2
Mon 20 16 Drilled and assembled CS105, CS106, CS107, universal, CS115, CS116, and CS117 4
Tue 21 19 Cut attach depressions. Made both LWA4s and the LWA6. Cut rescesses for these. 2
Thu 23 19 Sanded shear web foam. Made LWA2 and LWA3 and W18s. 2
Thu 23 16 Press fit CS112 into CZSA. Attached to push rod. 1
Fri 24 16 Drilling more holes for rivets. 1
Fri 24 19 Cleaned up floor and foam for layup. 1
Sat 25 19 Glassed 2 BID in bolt access area 1
Sun 26 19 Cut all glass for shear web. Mounted LWA4s and LWA6. Did shear web layup. Added LWA2 and LWA3. Peel plied. Added leading edge cores. 11
Mon 27 16 Finished drilling parts of control rods inside fuselage. Measured locations of CS108 and CS119 inside fuselage. Drilled hole in seatback. Test fit control in fuselage. 2
Wed 29 19 Test fit parts in wing root. Drilled more holes in push rods for wing root. 2
Fri 31 19 Squeezed all the rivets for the push rods. Opened all the 3/16" holes to 1/4" where needed. Drilled 1/4" holes in AN970-3 washers where needed. Cut A10s and A13s. 4
Monthly Total 53