11/01/18: 2.5Hrs 1. F-01202B-1 was clecoed to the fuselage. Worked on step 2.
11/02/18: 4.32Hrs 2. All of the holes on F-01202B-1 common to the longerons were match-drilled into it. The fuselage was vacuumed to remove burr.
01/05/19: 10Hrs 3. The canopy rib assemblies were clecoed to to F-01202B-1 and two holes were match-drilled into F-1202Y. 4. The four most-forward holes on both edges of F-01202B-1 were riveted. 5. The canopy rib assemblies were riveted to the fuselage, the two rivets that attach the F-12132 to the fuselage will be riveted after the aircraft is pending. 6. F-01202B-1 was riveted to the longerons. 7. F-01202B-1 and the canopy rib assemblies were riveted to F-01201A-1 along with the nutplates called out. 8. The canopy rib assemblies were sealed using tank sealant.
7/9/20 .55Hrs
The F-12132s were riveted to F-01202B-1,the installation of these parts was delayed until the interior was painted.
