What was found
DURING SCHEDULED C-8 CHECK PER JOB CARD HC5321, FOUND FUSELAGE EXTERIOR UPPER SKIN STIFFENER CRACKED AT FS 1039, WL286, BL0.0. REPAIR ACCOMPLISHED BY FABRICATING AND REPLACING STIFFENER IAW SMP583 CHAP 51-60 AND 51-70.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED C-8 CHECK PER JOB CARD HC5321, FOUND FUSELAGE EXTERIOR UPPER SKIN STIFFENER CRACKED AT FS 1039, WL286, BL0.0. REPAIR ACCOMPLISHED BY FABRICATING AND REPLACING STIFFENER IAW SMP583 CHAP 51-60 AND 51-70.