What was found
INSPECTION FOUND A 1.5 INCH CRACK IN RIGHT FUSELAGE SKIN LAP AT STA 880, S25R. THE SKIN WAS REPAIRED IAW SRM 53-00-01, REPAIR 31.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.5 INCH CRACK IN RIGHT FUSELAGE SKIN LAP AT STA 880, S25R. THE SKIN WAS REPAIRED IAW SRM 53-00-01, REPAIR 31.