As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFT END OF DOGHOUSE 6 O''CLOCK POSITION DOUBLER PEELED BACK ON BOTH SIDES OF INLET SKIN BUTT JOINT. REMOVED DAMAGE PER SRM 54-10-3D FIG 801D. DYE PENETRANT INSP AREA, NO CRACKS FOUND SRM 54-10-10-3D. CHEMICAL TREATED PER 900-2-4 NR 02. APPLIED EPOXY PRIMER AS PER PS 900-3-6 NR 3. OK TO INSTALL. REPAIRED STRAP AS PER SRM 54-10-3D FIG 801D. REPAIRED SKIN AS PER SRM 51-40-2.