02/12/19: 1Hr 1. The F-01203F-L & -R were dimpled and countersunk. 2. The F-01298-L was dimpled.
02/14/19: 1.16Hrs 3. The hex-hole was file as necessary for the head of the bolt. 4. The nutplates were riveted along the aft edge of the F-01203F-L & -R 5. The F-01203F-L & -R were riveted to the fuselage. the forward inboard nutplates
06/19/19: 0.41Hrs Step 6 The F-12100 was riveted to the F-01298-L &-R
12/03/19 6.5Hrs 7. The F-12100 and F-01298-L & -R were riveted to the F-01203A-1. 8. Two F-1264 were fabricated from AT6-058X5/16 as required. 9. Two Control Sick Pushrod Assemblies were fabricated as required.
