What was found
INSPECTION FOUND A 2 INCH CRACK IN LT FUSELAGE SKIN BETWEEN WINDOWS NR 16 AND NR 17 AT STA 680. THE CRACKED AREA WAS REPAIRED IAW SRM 51-40-00, 51-10-6, AND 51-10-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2 INCH CRACK IN LT FUSELAGE SKIN BETWEEN WINDOWS NR 16 AND NR 17 AT STA 680. THE CRACKED AREA WAS REPAIRED IAW SRM 51-40-00, 51-10-6, AND 51-10-2.