What was found
INSPECTION FOUND AN 8 INCH CRACK IN LT FUSELAGE SKIN AT STA 262-274, STRINGER 9L. THE CRACKED AREA OF SKIN WAS CUT OUT. REPAIR DOUBLERS AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-21-31.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND AN 8 INCH CRACK IN LT FUSELAGE SKIN AT STA 262-274, STRINGER 9L. THE CRACKED AREA OF SKIN WAS CUT OUT. REPAIR DOUBLERS AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-21-31.