What was found
DRILL START IN EXTERIOR FUSE SKIN AT STA 886, 2 INCH BELOW L10L. INSTALLED FUSELAGE SKIN DOUBLER, STA 886 LT LONGERON 10, PER EA MD80-53-006187.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DRILL START IN EXTERIOR FUSE SKIN AT STA 886, 2 INCH BELOW L10L. INSTALLED FUSELAGE SKIN DOUBLER, STA 886 LT LONGERON 10, PER EA MD80-53-006187.