What was found
UPON REMOVAL OF TRANSITION PANEL STRINGER CLIP AT BS 500G, STR 26R, FOUND TO BE CRACKED. ACFT GROUNDED. R & R STRINGER CLIP IAW SRM 51-40-02-0G-0.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
UPON REMOVAL OF TRANSITION PANEL STRINGER CLIP AT BS 500G, STR 26R, FOUND TO BE CRACKED. ACFT GROUNDED. R & R STRINGER CLIP IAW SRM 51-40-02-0G-0.