What was found
DURING DETAIL NR 1 WING INSPECTION, FOUND RIGHT OUTBOARD FLAP SKIN HAS A .25 INCH CRACK. STOP-DRILLED CRACK. PATCHED OVER CRACK USING FLAP STOCK, THREE ORIGINAL RIVETS, AND FOUR ADDITIONAL RIVETS IAW T.O. 1900-27-00-0001. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING DETAIL NR 1 WING INSPECTION, FOUND RIGHT OUTBOARD FLAP SKIN HAS A .25 INCH CRACK. STOP-DRILLED CRACK. PATCHED OVER CRACK USING FLAP STOCK, THREE ORIGINAL RIVETS, AND FOUR ADDITIONAL RIVETS IAW T.O. 1900-27-00-0001. (X)