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Date:  1-21-2020
Number of Hours:  8.50
Manual Reference:  
Brief Description:  37iS/U-16

01/16/20: 4.83Hrs
1. The bottom cowl was installed.
2,3 RTV was applied to the areas where the bent ends of the F-12116 pins contact the firewall.
4.The nutplate rivet holes on F-01285B-2 were countersunk and the nutplate was riveted to it.
5. F-01285B-2 was attached to the fuselage.
6.F-01285-1 was bent to match the cowl contour.
7,8. F-01285-1 was attached to F-01285B-2, it was aligned to F-01285 and clamped to it.
9.The nutplate screw holes on F-01285-1 were match-drilled #19 onto the bottom cowl.

01/20/20: 1.5Hrs
One of the nutplate screw holes that were match-drilled on step 9 was expanded so this hole was filled with epoxy and drilled again.

01/21/20: 1.66Hrs
11.The nutplate screw holes on F-12130A L&R were match-drilled #19 onto the bottom cowl.
12. The nutplate rivet holes were expanded to #40 and they were countersunk. The nutplates were riveted on both sides

01/22/20: 0.5Hrs
Aft side of F-01285 was trimmed until flush with the aft side of the bottom cowl. The cutout for the nose gear leg to go through on F-01285 was also expanded to avoid interference.
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