As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE SKIN CRACKED AT STRINGER 21R, BS 931-BS 934.0625. CRACK IS 3.0625" LONG. REPAIRED PER BOEING REPAIR SKETCH AND SERVICE REQUEST MESSAGE 1-79197357-1 THRU -21, FAA FORM 8100-9, DATED 21 MARCH 2008. 8100-9 STATES ALTERNATE REPAIR HAS BEEN APPROVED AS AN ALTERNATIVE METHOD OF COMPLIANCE (AMOC) TO PARAGRAPH (D) OF AD 2004-18-06.