What was found
INSPECTION FOUND A 2 INCH CRACK IN FUSELAGE SKIN AT BS 720C, RBL 2 WITH A HOLE CHAFED THROUGH AT LBL 6. THE CRACKED AND CHAFED AREAS WERE CUT OUT. A REPAIR WAS INSTALLED IAW SRM 51-10-2 AND BOEING DRAWING 7275331041.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2 INCH CRACK IN FUSELAGE SKIN AT BS 720C, RBL 2 WITH A HOLE CHAFED THROUGH AT LBL 6. THE CRACKED AND CHAFED AREAS WERE CUT OUT. A REPAIR WAS INSTALLED IAW SRM 51-10-2 AND BOEING DRAWING 7275331041.