Continued assembly of center fuselage frame and test fit of side skins as follows:
1. Fabricated rear spar bulkead support angles from angle stock. Cleco'd bottom end hole and transfer drilled remaining holes to #40. Enlarged these holes to #30.
2. Installed remaining sidewall ribs, stiffeners, and other parts with cleco's.
3. Rolled a conical bend in side skins per Rans manual.
4. Cleco'd side skins in place for test fit to notate proper placement of frame components and need for joggling of frame parts.
