What was found
SKIN HAS A .5" LONG CRACK, LATERAL AXIS, AT BS 1436.5. OTBD END OF CRACK IS 1.25" INBD OF L4R RIVET ROW. INSTALLED REPAIR IAW SRM 53-01, FIG 4, SHT 4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
SKIN HAS A .5" LONG CRACK, LATERAL AXIS, AT BS 1436.5. OTBD END OF CRACK IS 1.25" INBD OF L4R RIVET ROW. INSTALLED REPAIR IAW SRM 53-01, FIG 4, SHT 4.