What was found
INSPECTION FOUND A 1.5 INCH CRACK IN FUSELAGE SKIN AT STA 500 STRINGER 28R. THE CRACKED AREA WAS CUT OUT, STRINGER SPLICE AND SKIN DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-30-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.5 INCH CRACK IN FUSELAGE SKIN AT STA 500 STRINGER 28R. THE CRACKED AREA WAS CUT OUT, STRINGER SPLICE AND SKIN DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-30-3.