01/14/20: 2Hrs 1. The upper hinge halves were reinstalled to the bottom ones using the pins. 2. The top cowl was placed on the fuselage and clecloed to the bottom one, the top pins were installed. 3. It was verified that both cowls were aligned properly. 4. The rivet hole locations from the bottom halves of the F-12115-1 were transferred to the top cowl.
01/15/20: 2Hrs 5.The top cowl was removed and the previously marked locations were drilled #40. 6. Repeat 2 and 3 7. The top cowl was reinstalled. The recently made holes on the top cowl were used to match-drill their upper hinge halves #40.
