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Date:  11-28-2019
Number of Hours:  15.52
Manual Reference:  
Brief Description:  21iS/U-03

9/18/18: 8.66Hrs
1. F-12102AB was separated into 8 parts.
2. Holes were dimpled #30 and #40 on F-01221 L&R
3. F-01221 L&R, F-01221 L&R and F-01223 L&R were riveted to F-01204D and F-01224 L&R

STEP 4 POSTPONED UNTIL AIRCRAFT HAS BEEN PAINTED
5. Nutplates were riveted to F-01221 and F-01224 (L&R)
6. A total of four F-12102B were riveted to F-01223 L&R
7. F-1206B was separated into two parts.
8. Rear stub spars were filed to fit into the F-1206B curve.

9/19/18: 3.83Hrs

9. F-1206B L&R were riveted to F-1206C and F-01206A-1
10. A total of 16 holes were dimpled #40 and 6 holes were dimpled #30 on the flange of F-01206A-1.
11. Two nutplates were riveted onto F-01206A.
12. ES-00301 was riveted onto F-01206A-1.
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