What was found
CORROSION BETWEEN FUSELAGE SKIN AND BARE STRAP AT BS 1139, BETWEEN LT STRINGER 46 AND 45. REPAIRED IAW SRM 53-20-00, FIG 18 AND FIG 6, VOLUME I, REV 99. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION BETWEEN FUSELAGE SKIN AND BARE STRAP AT BS 1139, BETWEEN LT STRINGER 46 AND 45. REPAIRED IAW SRM 53-20-00, FIG 18 AND FIG 6, VOLUME I, REV 99. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.