What was found
FRAME OUTER CHORD CRACKED IN RADIUS ON AFT SIDE AT BS 188, WL 208. INSTALLED ANGLE DOUBLERS, SHIMS AND FILLERS TO FRAME OUTER CHORD. REPAIRED FUSELAGE SKIN ACCESS CUT-OUT WITH SKIN DOUBLER. MAJOR REPAIR ACCOMPLISHED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FRAME OUTER CHORD CRACKED IN RADIUS ON AFT SIDE AT BS 188, WL 208. INSTALLED ANGLE DOUBLERS, SHIMS AND FILLERS TO FRAME OUTER CHORD. REPAIRED FUSELAGE SKIN ACCESS CUT-OUT WITH SKIN DOUBLER. MAJOR REPAIR ACCOMPLISHED.