1. 28 holes were dimpled #40 on each F-01213. 2. 9 holes were dimpled #30 on each F-01213. 3. 14 nutplates were installed on each F-01213. 4. F-01213 was installed onto the fuselage. 5. 2 nutplates were riveted onto F-01202F and F-01213 L & R. 6. F-01286A was separated. 7. F-01268B was separated.
