What was found
FOUND CORROSION AT UPPER FWD CORNER ON SKIN PANEL A538-12189-201 AT C39-40, P'28-29, RHS. REPAIR PERFORMED BY REWORK AND INSTALLING INTERNAL REPAIR DOUBLER IAW EA 6-5315-112437 AND RAS: 052738/008/2007 ISSUE "A".
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND CORROSION AT UPPER FWD CORNER ON SKIN PANEL A538-12189-201 AT C39-40, P'28-29, RHS. REPAIR PERFORMED BY REWORK AND INSTALLING INTERNAL REPAIR DOUBLER IAW EA 6-5315-112437 AND RAS: 052738/008/2007 ISSUE "A".