11/01/18: 6.85Hrs Step 1: Borh L-1 & R-1 F-01201Q were riveted to both L-1 & R-1 F-01201E.
Step 2: Both upper and lower F-01201F-1 were riveted to the F-01201A-1.
01/11/19: 1.43Hrs Step 3: Both L-1 & R-1 F-01201E were riveted to the F-01201A-1 and F-01201B-1.
Step 4: The lower F-01201F-1 was riveted to both L-1 & R-2 F-01201E.
Step 5: The head of each rivet on F-01201A-1 and F-01201B-1 was covered with a thin layer of fuel tank sealant.
Step 6: The lower F-01201G-1 was riveted to the FF-00088A.
Step 7: Both upper and lower F-01201G-1 were riveted to both L-1 & R-1 F-01201E.
01/05/19: 1Hr Step 8: The F-1240C was fabricated from the provided AS3-025 material.
01/07/19: 2.16 Hrs Step 9: Match drill #40 was made from F-1240C to F-1240B. Step 10: Fitting between F-1240B and the fuselage was tested. All the holes in both pieces were deburred and dimpled. Step11: The F-1240C was riveted to the F-1240B. Worked on other several steps, but rivets had to be removed.
