As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ELONGATED HOLE G4 LOC. AT LEVEL STRGR 5 AND BTW FR53.6 AND FR53.7 LH SIDE UPPER FUSELAGE. ACCOMPLISHED PERMANENT REPAIR ON HOLE G4 LOCATED BTW FR 53.6 TO FR 53.7 AT LEVEL STR 5L AS PER ER/A 603846-14AD MATCHES WITH ALL STEPS ON PRI # 603846-14AD REV. 0 IT IS BEEN VALIDATED. PERFORMED REPAIR INSTRUCCION ON FUSELAGE SKIN CIRCUMFERENTIAL JOINT MOD BETWEEN FR 53.6-FR 53.7 AT STGR 5 LH.