What was found
SKIN BELOW AFT LATCH FOR PANEL 211AL IS CRACKED. R & R PANEL IAW SRM 51-42-06 PAR 6, 51-42 -10 PAR 8 & 51-42-21 PAR 6.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
SKIN BELOW AFT LATCH FOR PANEL 211AL IS CRACKED. R & R PANEL IAW SRM 51-42-06 PAR 6, 51-42 -10 PAR 8 & 51-42-21 PAR 6.