What was found
CRACK EXTERNAL SKIN ACCESS PANEL 191CR AT LOWER FUSELAGE. REPAIRED ACCESS PANEL 191CR AT LOWER FUSELAGE IAW SRM 51-70-04-2R-2 REPAIR 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK EXTERNAL SKIN ACCESS PANEL 191CR AT LOWER FUSELAGE. REPAIRED ACCESS PANEL 191CR AT LOWER FUSELAGE IAW SRM 51-70-04-2R-2 REPAIR 2.