As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
L/H I/B FLAP, LEADING EDGE, AT RIB 16, 2 GOUGES WITH SEPARATION OF 1.5 INCH EACH OTHER. ACCOMPLISHED STEP # 1 OF E.A. 300-5752-27-A4487 PRELIMINARY 1. (BLEND GOUGE DAMAGE MINIMALLY TO REMOVE DAMAGE IAW A300-600 SRM 57-50-00-101 AND SRM 51-73-10. SKIN INSERT AND BUTTSTRAPS WAS WORKED (FABRICATION AND INSTALLATION). VERIFIED 1 INSERT AND 2EA BUTTSTRAPS INSTALLATION PER A300/600 SRM 51-40-21-001 AND SRM 57-50-00-200.