What was found
CORROSION ON EXTERNAL FUSELAGE SKIN BETWEEN BS 520 AND 540, STRINGER 28L AND 28R. REWORKED AREA ON THE SKIN AND FOUND WITHIN LIMITS IAW SRM 53-00-01, ALLOWABLE DAMAGE 1, DETAIL II, FIG 101, SHEET 4 OF 6.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON EXTERNAL FUSELAGE SKIN BETWEEN BS 520 AND 540, STRINGER 28L AND 28R. REWORKED AREA ON THE SKIN AND FOUND WITHIN LIMITS IAW SRM 53-00-01, ALLOWABLE DAMAGE 1, DETAIL II, FIG 101, SHEET 4 OF 6.