What was found
FUSELAGE UPPER LOBE, STRINGER CLIP IS CRACKED, BS 660, STR 8R. REMOVED FABRICATED AND INSTALLED STR. CLIP AT BS 660 STR 8R IAW SRM 51-20-1 & 51-30- 02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE UPPER LOBE, STRINGER CLIP IS CRACKED, BS 660, STR 8R. REMOVED FABRICATED AND INSTALLED STR. CLIP AT BS 660 STR 8R IAW SRM 51-20-1 & 51-30- 02.