What was found
DURING INSPECTION, TWO GOUGES WERE FOUND ON NR 2 ENGINE STRUT RIGHT SKIN PANEL NEAR ACCESS DOOR CUT OUT. MAXIMUM DEPTH OF BLENDED OUT REQUIRED TO COMPLETELY REMOVE DAMAGE, 0.025 INCH. REPAIRED AREA IAW REA .
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION, TWO GOUGES WERE FOUND ON NR 2 ENGINE STRUT RIGHT SKIN PANEL NEAR ACCESS DOOR CUT OUT. MAXIMUM DEPTH OF BLENDED OUT REQUIRED TO COMPLETELY REMOVE DAMAGE, 0.025 INCH. REPAIRED AREA IAW REA .