What was found
CORROSION ON STRINGER 51, BETWEEN FRAME 36-37 LT, AFTER BLENDING IS THE REMAINING THICKNESS OUT OF LIMIT IAW SRM 53-10-00. STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-10-14/FIG 201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON STRINGER 51, BETWEEN FRAME 36-37 LT, AFTER BLENDING IS THE REMAINING THICKNESS OUT OF LIMIT IAW SRM 53-10-00. STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-10-14/FIG 201.