What was found
INSPECTION FOUND FUSELAGE SKIN CORRODED AT BS 2240, STRINGER 49R TO 50R. THE SKIN WAS REPAIRED IAW SRM 53-30-03, FIGURE 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND FUSELAGE SKIN CORRODED AT BS 2240, STRINGER 49R TO 50R. THE SKIN WAS REPAIRED IAW SRM 53-30-03, FIGURE 1.