What was found
INSPECTION FOUND A .25 INCH CRACK IN RIGHT FUSELAGE SKIN ABOVE SKIN LAP S25R APPROXIMATELY 6 INCHES FORWARD OF STA 887. THE SKIN WAS REPAIRED IAW SRM 53-00-01, PRODECURE 5, PAGE 203, REPAIR 31.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .25 INCH CRACK IN RIGHT FUSELAGE SKIN ABOVE SKIN LAP S25R APPROXIMATELY 6 INCHES FORWARD OF STA 887. THE SKIN WAS REPAIRED IAW SRM 53-00-01, PRODECURE 5, PAGE 203, REPAIR 31.