As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING H CHK AT STAG, CORROSION WAS NOTED ON THE FUSELAGE SKIN BETWEEN BS 1197+165 AND 1197+187. A REPAIR WAS INSTALLED IAW ER/A 631872-14, SECT I. FOLLOW ON ACTION IS REQUIRED FOR SECT. II REPEAT INSPECTIONS. ACCOMPLISH ER/A 631872-14 SECT. II REPEAT INSPECTIONS PRIOR TO 30,000 TOTAL A/C CYCLES, THEN REPEAT AT 9000 FLIGHT CYCLE INTERVALS THEREAFTER. (1429833)