What was found
FUSELAGE SKIN CORROSION BETWEEN SKIN LAYERS FROM BS 1140 TO 1183 STR 15 TO 20R. REMOVED CORROSION AND CUT OUT DAMAGED SKIN BS 1148 TO 1183 STR 14 TO 20R. INSTALLED DOUBLER PER EA 7-5310-28796A AND SRM 53-30-3 FIG 12.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN CORROSION BETWEEN SKIN LAYERS FROM BS 1140 TO 1183 STR 15 TO 20R. REMOVED CORROSION AND CUT OUT DAMAGED SKIN BS 1148 TO 1183 STR 14 TO 20R. INSTALLED DOUBLER PER EA 7-5310-28796A AND SRM 53-30-3 FIG 12.