1,2 The tailcome skins were indentified and prepared 11/13/18: 6.68Hrs 3,4 F-1210 was fluted on two locations until the curvature was met. Most of the fuselage frames were fluted in order for the holes to be as alligned as possible. 5. F-1208A was riveted to F-1208-R. 6,7 F-1208 L&R and F-1209 L&R were riveted together. 8. F-1210B and F-1210C were clecoed to F-1210L&R, this was used to match-drill two #30 holes onto F-1210A L&R. 9. Four holes were final-drilled #12 on F-1210B.
11/14/18: 8Hrs The tailcone skins were identified, deburred and the edges were broken as specified on the manual. 10. F-1210A L&R, F-1210B and F-1210C were riveted together
