As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DOT A24-1 NOSE W/W PANEL 113BW HAS FRETTING CORROSION AROUND ALL FASTENER HOLES.<[01] REMOVED CORROSION IAW SRM 51-10-02-0G-0. ORIGINAL 'T'= .192'; REMAINING 'T'= .188'; LOSS OF .004'. MAX ALLOWED IS .005'; DAMAGE WITHIN LIMITS IAW SRM 53-10-14-1A-2. RECEIVED NEW PANEL; P/N 141A7900-4; DUE TO REPAIR REQUIRING REINSPECT. PANEL INSTALLED ON TASK CARD TTG8Q00S5NC3.<BR><BR>A-TAG# WN43993;[02] VERIFIED ITEM 1.