What was found
INSPECTION FOUND A .25 INCH CRACK IN FUSELAGE FRAME AT STA 887 BETWEEN STRINGER 8R AND 9R. THE FRAME WAS REPAIRED IAW ECRA 5310-04636.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .25 INCH CRACK IN FUSELAGE FRAME AT STA 887 BETWEEN STRINGER 8R AND 9R. THE FRAME WAS REPAIRED IAW ECRA 5310-04636.