What was found
FOUND A .75 INCH CRACK ON FUSELAGE FRAME FS 640.00 AT STRINGER 9. DISCOVERED DURING B001 INSPECTION. COMPLIED WITH EA RJ208-53 IAW REO 601R-53-61-557.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND A .75 INCH CRACK ON FUSELAGE FRAME FS 640.00 AT STRINGER 9. DISCOVERED DURING B001 INSPECTION. COMPLIED WITH EA RJ208-53 IAW REO 601R-53-61-557.