What was found
LEFT FWD FUSELAGE SKIN IS CRACKED AT AFT LATCH FOR PANEL 212AL. R & R SKIN WITH NEW SKIN IAW SRM 51-42-06.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT FWD FUSELAGE SKIN IS CRACKED AT AFT LATCH FOR PANEL 212AL. R & R SKIN WITH NEW SKIN IAW SRM 51-42-06.