er to allow for a flush skin repair. The existing nut plate holes were filled with 4 screws P/N. AN525-10R7. See Attached FAA Form 8110.3 signed by DERT-410115-CE Paul Hedding dated August 15, 2012 using Nextant Aerospace Engineering Order 139.12 Rev C Dated August 03, 2012 for details. ICA Weight and Balance change is N