02/05/19: 1.5Hrs Step 1. The VS-1213 was placed onto the V-Stab assembly. step 2 was worked on.
02/06/19: 1.75Hrs 2. Match-drilled #30 the holes from the VS-1201 into the V-stab tip fairing and clecoed. 3. The V-stab tip fairing was removed and the surface sanded. 4. The Vs-1213 was trimmed. 5. The rudder assembly was temporally attached to the V-stab assembly.
02/08/19: 1Hr Worked on 6.
02/13/19: 1Hr step 6. The VS-1213 V-stab tip fairing was placed in its correct position. The aft edge of the V -stab was marked in order to indicate any material that was within 1/8 of the rudder assembly. The fairing was removed and triom to the marked areas. The process was repeated untill 1/8 inn of clearence was reached.