What was found
CRACK OUTBOARD SUPPORT ANGLE OF INBOARD AUXILIARY TRACK SLAT 1 AT LT WING. REPLACED ANGLE LOCATED OF INBOARD AUXILIARY TRACK SLAT 1 AT LT WING AND IAW SRM 51-40-02;[03] TOOK MEASURE OF CRACK IS: L= 1.350 LOCATED SUPPORT ANGLE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK OUTBOARD SUPPORT ANGLE OF INBOARD AUXILIARY TRACK SLAT 1 AT LT WING. REPLACED ANGLE LOCATED OF INBOARD AUXILIARY TRACK SLAT 1 AT LT WING AND IAW SRM 51-40-02;[03] TOOK MEASURE OF CRACK IS: L= 1.350 LOCATED SUPPORT ANGLE.