What was found
CORROSION DAMAGE ON CENTER FUSELAGE RH TOP SKIN PANEL ASSEMBLY PN 85320282 BETWEEN X291.40 -X312.35 AND STR. 1-2S. REF. 008.53-22.07
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION DAMAGE ON CENTER FUSELAGE RH TOP SKIN PANEL ASSEMBLY PN 85320282 BETWEEN X291.40 -X312.35 AND STR. 1-2S. REF. 008.53-22.07