What was found
CORROSION ON EXTERNAL FUSELAGE SKIN BS 1098 - 1112 BETWEEN LONGERONS 27 - 29L. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-04 FIG 57, 51-10-3 P. 21-14, 51-30-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON EXTERNAL FUSELAGE SKIN BS 1098 - 1112 BETWEEN LONGERONS 27 - 29L. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-04 FIG 57, 51-10-3 P. 21-14, 51-30-5.