10/04/18: 6.2Hrs (All of the following steps were mirrored to the left side) 1. F-1202E-R was riveted to F-01202F-1 and F-1203G-R was riveted to F-01203A-1. 2. two holes were match-drilled for each of the F-01248 onto the F-01202E and F-1204H. 3. F-01248B was riveted to F-01248. 4. F-01248 was riveted to F-1202E, F-1204C and F-1203H.
10/08/18: 0.66Hrs 5. F-01255 were inserted into the fuselage and F-01234 were cleco to F-1203G.
