What was found
A 2.5 INCH CRACK ON FUSELAGE SKIN FWD OF BS 344 FRAME AND 4 INCHES BELOW STR 21R (HFEC VERIFIED). REPAIRED SKIN AS PER SRM 53-00-01-2R-31 DETAIL X1. FACT AS A RESULT OF POST REPAIR INSPECTION.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
A 2.5 INCH CRACK ON FUSELAGE SKIN FWD OF BS 344 FRAME AND 4 INCHES BELOW STR 21R (HFEC VERIFIED). REPAIRED SKIN AS PER SRM 53-00-01-2R-31 DETAIL X1. FACT AS A RESULT OF POST REPAIR INSPECTION.