What was found
INSPECTION FOUND A 1.75 INCH CRACK IN FUSELAGE SKIN AT BS 775, STRINGER 19R. THE CRACKED AREA WAS CUT OUT, A REPAIR DOUBLER WAS 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 1.75 INCH CRACK IN FUSELAGE SKIN AT BS 775, STRINGER 19R. THE CRACKED AREA WAS CUT OUT, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3.