What was found
FOUND FUSELAGE SKIN CRACKED DURING HFEC INSPECTION IAW PRI 519950-14 REV O STEP 4 AT BS 1700 BETWEEN STRINGERS 29 & 30R APPROXIMATELY LENGTH 1 INCH. REMOVED SKIN AND REPAIRED IAW PRI 519950-14AD REV 4 C/W ERA 519950-14 AD.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND FUSELAGE SKIN CRACKED DURING HFEC INSPECTION IAW PRI 519950-14 REV O STEP 4 AT BS 1700 BETWEEN STRINGERS 29 & 30R APPROXIMATELY LENGTH 1 INCH. REMOVED SKIN AND REPAIRED IAW PRI 519950-14AD REV 4 C/W ERA 519950-14 AD.