What was found
DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FUSELAGE SKIN FS 389 TO 406, LONGERONS 27R TO 28R. REPAIRED PANEL ASSEMBLY (P/N 5911412) PER EA 99-108803.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FUSELAGE SKIN FS 389 TO 406, LONGERONS 27R TO 28R. REPAIRED PANEL ASSEMBLY (P/N 5911412) PER EA 99-108803.