What was found
L/H FUSELAGE SKIN AT #1 PACK EXHAUST DOOR UPPER AFT CORNER HAS A .200 IN. CRACK PROPAGATING OUT OF FASTENER HOLE. (MARKED) INSTALLED FILLER, DOUBLER, AND TRIPLER REF MD11 SRM 53-20-15-2R REPAIR 3. MAJOR REPAIR
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
L/H FUSELAGE SKIN AT #1 PACK EXHAUST DOOR UPPER AFT CORNER HAS A .200 IN. CRACK PROPAGATING OUT OF FASTENER HOLE. (MARKED) INSTALLED FILLER, DOUBLER, AND TRIPLER REF MD11 SRM 53-20-15-2R REPAIR 3. MAJOR REPAIR