What was found
DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS FOUND IN THE EXTERNAL PLATING A FUSELAGE STATION 225 BETWEEN LONGERONS 29 AND 30 LEFT. THE CRACK WAS REPAIRED IAW THE STRUCTURAL REPAIR MANUAL. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS FOUND IN THE EXTERNAL PLATING A FUSELAGE STATION 225 BETWEEN LONGERONS 29 AND 30 LEFT. THE CRACK WAS REPAIRED IAW THE STRUCTURAL REPAIR MANUAL. (M)