What was found
FUSELAGE SKIN CRACK INDICATED WITH NDT AT BS 414-418 AT STR 4R SKIN LAP AREA UPPER SKIN PANEL. *S/D* MAJOR REPAIR: REMOVED DAMAGE. FABRICATED AND INSTALLED EXTERNAL DOUBLER AND FILLER REPAIR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN CRACK INDICATED WITH NDT AT BS 414-418 AT STR 4R SKIN LAP AREA UPPER SKIN PANEL. *S/D* MAJOR REPAIR: REMOVED DAMAGE. FABRICATED AND INSTALLED EXTERNAL DOUBLER AND FILLER REPAIR.