As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SURFACE CORROSION ON L/H TRANSITION ANGLE LBL 21 STA. 767 - 787 (MARKED)<[01] REMOVED CORROSION ON LH TRANSITION ANGLE STA 767-787 REMAINING THICKNESS IS 0.029. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] C/W INSP; REMOVED CORROSION ON LH TRANSITION ANGLE STA 767-787 REMAINING THICKNESS IS 0.029. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[03] ALL WORK ACCOMPLISHED ON TTG8Q00P693X.;[04] CW