What was found
FUSELAGE SKIN FRAME 85 TO FRAME 86, BETWEEN STRINGER 13-15R. REPAIRED IAW SRM 53-10-12, FIG 208 AND 51-40-44, REV 23. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116. EO 6-5100-7-5000D PART 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN FRAME 85 TO FRAME 86, BETWEEN STRINGER 13-15R. REPAIRED IAW SRM 53-10-12, FIG 208 AND 51-40-44, REV 23. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116. EO 6-5100-7-5000D PART 1.