What was found
FUSELAGE HAS 3" SUB-SURFACE SKIN CRACK AT BS 827 + 12" ABOVE STR 4R. REPAIR COMPLETED PER EA 1-353-21707 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.
FUSELAGE HAS 3" SUB-SURFACE SKIN CRACK AT BS 827 + 12" ABOVE STR 4R. REPAIR COMPLETED PER EA 1-353-21707 FACT AS A RESULT OF POST REPAIR INSPECTION.