What was found
DURING A SCHEDULED ROUTINE INSPECTION FOUND THE SKIN CRACKED IN THE UPPER CABIN FUSELAGE AT FS 273.25, BETWEEN STRINGER 1 AND 2R, CRACK IS ALONG A ROW OF FASTENERS, 3.65" IN LENGTH. REPAIRED THE AFFECTED AREA IAW EO12-1900-53-037.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING A SCHEDULED ROUTINE INSPECTION FOUND THE SKIN CRACKED IN THE UPPER CABIN FUSELAGE AT FS 273.25, BETWEEN STRINGER 1 AND 2R, CRACK IS ALONG A ROW OF FASTENERS, 3.65" IN LENGTH. REPAIRED THE AFFECTED AREA IAW EO12-1900-53-037.