Labels

Monday, February 2, 2015

More forward upper fuselage: 6.4 hours


  • Bent tab on center rib reinforcing angle to 25 degrees and checked fit
  • Drilled rivet holes through firewall and center rib
  • Deburred and dimpled above
  • Match drilled left and right ribs to firewall
  • Drilled left rib and firewall for mounting engine sensor manifold (fuel, oil and manifold pressure)
  • Match drilled and deburred sub panel and left and right ribs
  • Clecoed forward skin on
Using top skin to help align center rib:

Using rivet fan to layout holes in firewall:

Center rib drilled:

Top skin clecoed on: